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1
+ arXiv:2301.08418v1 [math.CT] 20 Jan 2023
2
+ Measurings of Hopf algebroids and morphisms in cyclic (co)homology
3
+ theories
4
+ Abhishek Banerjee *
5
+ Surjeet Kour †
6
+ Abstract
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+ In this paper, we consider measurings between Hopf algebroids and show that they induce morphisms on cyclic homology
8
+ and cyclic cohomology. We also consider comodule measurings between SAYD modules over Hopf algebroids. These measur-
9
+ ings induce morphisms on cyclic (co)homology of Hopf algebroids with SAYD coefficients. Finally, we obtain morphisms on
10
+ cyclic homology induced by measurings of cyclic comp modules over operads with multiplication.
11
+ MSC(2020) Subject Classification: 16T15, 16E40, 18D50
12
+ Keywords: Hopf algebroids, cyclic (co)homology, SAYD modules, comp modules
13
+ 1
14
+ Introduction
15
+ Let k be a field, C be a k-coalgebra and A, B be k-algebras. In [20], Sweedler introduced the notion of a coalgebra measuring
16
+ as a kind of generalized morphism between algebras. More precisely, a C-measuring from A to B consists of a k-linear map
17
+ φ : C −→ Vectk(A, B) satisfying
18
+ φ(c)(aa′) =
19
+
20
+ φ(c(1)(a)φ(c(2))(a′)
21
+ φ(c)(1) = ǫ(c)1
22
+ (1.1)
23
+ for any a, a′ ∈ A. Here, ∆(c) = � c(1) ⊗ c(2) denotes the coproduct on C and ǫ : C −→ k denotes the counit. Since then, the
24
+ notion of a measuring has been widely studied in the literature by several authors (see, for instance, [1], [3], [4], [9], [10], [11],
25
+ [12],[22], [23], [24]).
26
+ In [2], we studied how coalgebra measurings induce morphisms between Hochschild homology groups of algebras. The purpose
27
+ of this paper is to take this idea one step further. Our aim is to consider cocommutative coalgebra morphisms between Hopf
28
+ algebroids and show that they induce morphisms in cyclic homology and cyclic cohomology. We begin by showing that there are
29
+ universal measurings which give an enrichment of the category HAlgk of Hopf algebroids over the category of cocommutative
30
+ coalgebras. If U is a Hopf algebroid, the cyclic module C•(U) defining its cyclic homology groups as well as the cocyclic
31
+ module C•(U) defining its cyclic cohomology groups are defined in [13]. We show that a cocommutative coalgebra measuring
32
+ between two Hopf algebroids induces morphisms on their corresponding cyclic homology and cyclic cohomology groups. If a
33
+ Hopf algebroid is commutative, we know from [15] that there is a shuffle product on its Hochschild homology groups. We show
34
+ that a measuring between commutative Hopf algebroids induces an algebra measuring between the corresponding Hochschild
35
+ homology rings with respct to this shuffle product. This also gives us an enrichment of commutative Hopf algebroids over
36
+ cocommutative coalgebras.
37
+ Thereafter, we consider comodule measurings of SAYD modules over Hopf algebroids. Accordingly, we obtain an enrichment
38
+ of the “global category” of SAYD modules (see Theorem 5.9) over the “global category” of comodules. The cyclic homology
39
+ *Department of Mathematics, Indian Institute of Science, Bangalore. Email: [email protected]
40
+ †Department of Mathematics, Indian Institute of Technology, Delhi. Email: [email protected]
41
+ 1
42
+
43
+ and the cyclic cohomology of a Hopf algebroid with coefficients in an SAYD module was defined in [14]. We show that a
44
+ comodule measuring induces morphisms between cyclic (co)homology with SAYD coefficients. In the final part of the paper,
45
+ we work with pairs of the form (O, M), where M is a cyclic unital comp module over a non-Σ operad O with multiplication
46
+ in the sense of [16]. The cyclic homology groups of such a comp module were also defined in [16]. We consider comodule
47
+ measurings between such pairs and show that they induce morphisms in cyclic homology.
48
+ 2
49
+ Measurings of Hopf algebroids
50
+ Throughout, k is a field and let Vectk be the category of k-vector spaces. Let A be a unital k-algebra. In order to define left
51
+ and right bialgebroids, as well as Hopf algebroids in later sections, we will frequently need both the algebra A and its opposite
52
+ algebra Aop. For this, we will often write the algebra A as AL, while Aop will often be written as AR.
53
+ An (s, t)-ring over A consists of a unital k-algebra U along with two k-algebra morphisms s : A −→ U and t : Aop −→ U whose
54
+ images commute in U, i.e., s(a1)t(a2) = t(a2)s(a1) for any a1, a2 ∈ U. The morphisms s and t are often referred to as source
55
+ and target maps respectively. These morphisms introduce an (A, A)-bimodule structure on U given by left multiplication
56
+ a1 · h · a2 := s(a1)t(a2)h
57
+ a1, a2 ∈ A, h ∈ H
58
+ (2.1)
59
+ The left and right A-module structures on U in (2.1) allow us to consider the tensor product U ⊗A U. The following subspace
60
+ of U ⊗A U is known as the Takeuchi product
61
+ U ×A U := {� ui ⊗A u′
62
+ i ∈ U ⊗A U | � uit(a) ⊗A u′
63
+ i = � ui ⊗A u′
64
+ is(a), ∀ a ∈ A}
65
+ (2.2)
66
+ It is well known (see, for instance, [13, § 2]) that the Takeuchi product U ×A U is a unital subalgebra of U ⊗A U.
67
+ From now onwards, we also fix a unital k-algebra U. The multiplication on U will be denoted by µU. Since the category of
68
+ (A, A)-bimodules is monoidal, we can consider coalgebra objects in this category. We now recall the notion of a left Hopf
69
+ algebroid (see, for instance, [5], [13], [21]). For several closely related notions, see [18], [19].
70
+ Definition 2.1. A left bialgebroid UL := (U, AL, sL, tL, ∆L, ǫL) over k consists of the following data:
71
+ (1) A unital k-algebra AL
72
+ (2) A unital k-algebra U which carries the structure of an (sL, tL) ring over AL.
73
+ (3) A coalgebra object (U, ∆L : U −→ U ⊗AL U, ǫL : U −→ AL) in the category of (AL, AL)-bimodules satisfying the following
74
+ conditions:
75
+ (i) ∆L : U −→ U ⊗AL U factors through U ×A U ⊆ U ⊗AL U.
76
+ (ii) ǫL(usL(ǫL(u′))) = ǫL(uu′) = ǫL(utL(ǫL(u′))) for all u, u′ ∈ H.
77
+ A morphism (F, f) : (U, AL, sL, tL, ∆L, ǫL) = UL −→ U′
78
+ L = (U′, A′
79
+ L, s′
80
+ L, t′
81
+ L, ∆′
82
+ L, ǫ′
83
+ L) of left bialgebroids consists of a pair of
84
+ k-algebra morphisms F : U −→ U′ and f : AL −→ A′
85
+ L such that
86
+ F ◦ sL = s′
87
+ L ◦ f
88
+ F ◦ tL = t′
89
+ L ◦ f
90
+ ∆′
91
+ L ◦ F = (F ⊗φ F) ◦ ∆L
92
+ f ◦ ǫL = ǫ′
93
+ L ◦ F
94
+ (2.3)
95
+ We will denote the category of left bialgebroids over k by LBialgk.
96
+ If UL = (H, AL, sL, tL, ∆L, ǫL) is a left bialgebroid, we employ standard Sweedler notation to write ∆L(u) = � u(1) ⊗ u(2) for any
97
+ u ∈ H and suppress the summation sign throughout. We now recall the notion of Hopf algebroid from [5, Definition 4.1].
98
+ Definition 2.2. A Hopf algebroid U = (UL, S ) over k consists of the following data:
99
+ (1) A left bialgebroid UL = (U, AL, sL, tL, ∆L, ǫL) over k.
100
+ (2) An involutive anti-automorphism S : U −→ U of the k-algebra U which satisfies S ◦ tL = sL as well as
101
+ S (u(1))(1)u(2) ⊗ S (u(1))(2) = 1H ⊗ S (u)
102
+ S (u2)1 ⊗ S (u(2))(2)u(1) = S (u) ⊗ 1U
103
+ (2.4)
104
+ 2
105
+
106
+ as elements of U ⊗AL U, for all u ∈ U.
107
+ A morphism (F, f) : U = (UL, S ) −→ (U′
108
+ L, S ′) = U′ of Hopf algebroids is a morphism in LBialgk that also satisfies S ′◦F = f ◦S .
109
+ We will denote the category of Hopf bialgebroids over k by HAlgk.
110
+ We remark here that in this paper we will always assume the antipode on a Hopf algebroid U = (UL, S ) is involutive, i.e.,
111
+ S 2 = id. However, this condition is not part of the original definition due to B¨ohm and Szlach´anyi in [5]. Further, it is shown in
112
+ [5, Proposition 4.2] that a Hopf algebroid (UL, S ) is equivalent to a datum consisting of a left bialgebroid and a right bialgebroid
113
+ connected by an antipode.
114
+ We now recall the classical notion of a coalgebra measuring due to Sweedler [20]. Let R, R′ be k-algebras and C be a k-
115
+ coalgebra. Then, a C-measuring from R to R′ consists of a morphism ψ : C −→ Vectk(R, R′) such that
116
+ ψ(x)(ab) =
117
+
118
+ ψ(x(1))(a)ψ(x(2))
119
+ ψ(x)(1R) = ǫC(x)1R′
120
+ ∀ a, b ∈ R
121
+ (2.5)
122
+ where the coproduct ∆C : C −→ C ⊗ C is given by ∆C(x) = � x(1) ⊗ x(2) for any x ∈ C and ǫC : C −→ k is the counit. The
123
+ measuring as in (2.5) is said to be cocommutative if the coalgebra C is cocommutative. In this paper, we will only consider
124
+ cocommutative measurings. By abuse of notation, if ψ : C −→ Vectk(R, R′) is a coalgebra measuring, we will often write the
125
+ morphism ψ(x) ∈ Vectk(R, R′) simply as c : R −→ R′ for any x ∈ C.
126
+ We are now ready to introduce the notion of measuring between Hopf algebroids.
127
+ Definition 2.3. Let U = (U, S ) = (U, AL, sL, tL, ∆L, ǫL, S ) and U′ = (U′, S ′) = (U′, AL, s′
128
+ L, t′
129
+ L, ∆′
130
+ L, ǫ′
131
+ L, S ′) be Hopf algebroids
132
+ over k. Let C be a cocommutative k-coalgebra. A C-measuring (Ψ, ψ) from U to U′ consists of a pair of measurings
133
+ Ψ : C −→ Vectk(U, U′)
134
+ ψ : C −→ Vectk(AL, A′
135
+ L)
136
+ (2.6)
137
+ such that the following diagrams commute for any x ∈ C
138
+ AL
139
+ sL
140
+ −−−−−−→ U
141
+ c
142
+ �
143
+ �c
144
+ A′
145
+ L
146
+ s′
147
+ L
148
+ −−−−−−→ U′
149
+ AL
150
+ tL
151
+ −−−−−−→ U
152
+ c
153
+ �
154
+ �c
155
+ A′
156
+ L
157
+ t′
158
+ L
159
+ −−−−−−→ U′
160
+ U
161
+ S
162
+ −−−−−−→ U
163
+ c
164
+ �
165
+ �c
166
+ U′
167
+ S ′
168
+ −−−−−−→ U′
169
+ (2.7)
170
+ U
171
+ ǫL
172
+ −−−−−−→ AL
173
+ c
174
+ �
175
+ �c
176
+ U′
177
+ ǫ′
178
+ L
179
+ −−−−−−→ A′
180
+ L
181
+ U
182
+ ∆L
183
+ −−−−−−→ U ⊗AL U
184
+ c
185
+ �
186
+ �c
187
+ U′
188
+ ∆′
189
+ L
190
+ −−−−−−→ U′ ⊗A′
191
+ L U′
192
+ (2.8)
193
+ where the arrow c : U ⊗AL U −→ U′ ⊗A′
194
+ L U′ is defined by setting c(u1 ⊗ u2) := x(1)(h) ⊗ x(2)(u2) for u1 ⊗ u2 ∈ U ⊗AL U.
195
+ Before proceeding further, we need to verify the following fact.
196
+ Lemma 2.4. For any x ∈ C, the morphism c : H ⊗AL U −→ U′ ⊗A′
197
+ L U′ defined by setting c(u1 ⊗ u2) := x(1)(h) ⊗ x(2)(u2) for
198
+ u1 ⊗ u2 ∈ U ⊗AL U is well-defined.
199
+ Proof. We consider u1, u2 ∈ uL and a ∈ AL. Using the fact that Ψ : C −→ Vectk(U, U′) is a measuring and applying the
200
+ conditions in (2.7) and (2.8), we see that
201
+ c((u1 · a) ⊗ u2) = c(tL(a)u1 ⊗ u2)
202
+ = x(1)(tL(a)u1) ⊗ x(2)(u2) = x(1)(tL(a))x(2)(u1) ��� x(3)(u2)
203
+ = t′
204
+ L(x(1)(a))x(2)(u1) ⊗ x(3)(u2)
205
+ = t′
206
+ L(x(2)(a))x(1)(u1) ⊗ x(3)(u2)
207
+ (because C is cocommutative)
208
+ = x(1)(u1) · x(2)(a) ⊗ x(3)(u2) = x(1)(u1) ⊗ x(2)(a) · x(3)(u2)
209
+ = x(1)(u1) ⊗ s′
210
+ L(x(2)(a))x(3)(u2) = x(1)(u1) ⊗ x(2)(sL(a))x(3)(u2)
211
+ = x(1)(u1) ⊗ x(2)(sL(a)u2) = x(1)(u1) ⊗ x(2)(a · u2)
212
+ = c(u1 ⊗ (a · u2))
213
+ (2.9)
214
+
215
+ 3
216
+
217
+ If U = (UL, S ) and U′ = (U′
218
+ L, S ′) are Hopf algebroids over k, we now consider the subspace
219
+ V(U, U′) ⊆ Vectk(U, U′) × Vectk(AL, A′
220
+ L)
221
+ (2.10)
222
+ given by setting
223
+ V(U, U′) := {(F, f) | FsL = s′
224
+ L f, FtL = t′
225
+ L f, FS = S ′F and fǫL = ǫ′
226
+ LF }
227
+ (2.11)
228
+ We note that a measuring from U to U′ by means of a cocommutative coalgebra C has an underlying morphism (Ψ, ψ) : C −→
229
+ V(U, U′).
230
+ Let Coalgk denote the category of k-coalgebras. We know that the forgetful functor Coalgk −→ Vectk has a right adjoint
231
+ C : Vectk −→ Coalgk. In other words, we have natural isomorphisms
232
+ Vectk(C, V) � Coalgk(C, C(V))
233
+ (2.12)
234
+ for any k-coalgebra C and any k-vector space V.
235
+ Proposition 2.5. Let U = (UL, S ) and U′ = (U′
236
+ L, S ′) be Hopf algebroids over k. Then, there exists a cocommutative coalgebra
237
+ Mc(U, U′) and a measuring (Φ, φ) from U to U′ satisfying the following universal property: given any measuring (Ψ, ψ) : C −→
238
+ V(U, U′) with a cocommutative coalgebra C, there exists a unique morphism ξ : C −→ Mc(U, U′) of coalgebras making the
239
+ following diagram commutative
240
+ Mc(U, U′)
241
+ (Φ,φ)
242
+ � V(U, U′)
243
+ C
244
+ ξ
245
+ �■■■■■■■■■■
246
+ (Ψ,ψ)
247
+ �✇
248
+
249
+
250
+
251
+
252
+
253
+
254
+
255
+
256
+ (2.13)
257
+ Proof. We set V := V(U, U′) and consider the canonical morphism π(V) : C(V) −→ V ⊆ Vectk(uL, u′
258
+ L) × Vectk(AL, A′
259
+ L) from
260
+ the cofree coalgebra C(V) induced by the adjunction in (2.12). We now set Mc(U, U′) := � D, where the sum is taken over all
261
+ cocommutative subcoalgebras of C(V) such that the restriction π(V)|D : D −→ V = V(U, U′) is a measuring. It is clear that this
262
+ sum is still a cocommutative coalgebra, and that the restriction (Φ, φ) := π(V)|Mc(U,U′) gives a measuring from U to U′.
263
+ In general, if (Ψ, ψ) : C −→ V = V(U, U′) is a cocommutative measuring, the adjunction in (2.12) shows that it factors through
264
+ ξ : C −→ C(V). Then, ξ(C) ⊆ C(V) is a cocommutative coalgebra such that the restriction π(V)|ξ(C) is a measuring. By
265
+ definition, it follows that ξ(C) ⊆ Mc(U, U′). This proves the result.
266
+
267
+ From (2.10) and (2.11) it is clear that given Hopf algebroids U = (UL, S ), U′ = (U′
268
+ L, S ′) and U′′ = (U′′
269
+ L, S ′′), the composition
270
+ of morphisms induces a canonical map
271
+ V(U, U′) ⊗ V(U′, U′′)
272
+
273
+ −→ V(U, U′′)
274
+ (2.14)
275
+ We denote by CoCoalgk the category of cocommutative coalgebras over k. We know that this category is symmetric monoidal
276
+ and our objective is to show that the category HAlgk of Hopf algebroids is enriched over CoCoalgk. For this we need the
277
+ following result.
278
+ Proposition 2.6. Let U = (UL, S ), U′ = (U′
279
+ L, S ′) and U′′ = (U′′
280
+ L, S ′′) be Hopf algebroids over k. Suppose that we have a
281
+ measuring (Ψ, ψ) : C −→ V(U, U′) from U to U′ and a measuring (Ψ′, ψ′) : C′ −→ V(U′, U′′) from U′ to U′′. Then, the
282
+ following
283
+ (Ψ′, ψ′) ◦ (Ψ, ψ) : C ⊗ C′ (Ψ,ψ)⊗(Ψ′,ψ′)
284
+ −−−−−−−−−−→ V(U, U′) ⊗ V(U′, U′′)
285
+
286
+ −→ V(U, U′′)
287
+ (2.15)
288
+ determines a measuring from U to U′′.
289
+ Proof. It is easy to verify that the compositions
290
+ C ⊗ C′ Ψ⊗Ψ′
291
+ −−−−→ Vectk(U, U′) ⊗ Vectk(U′, U′′)
292
+
293
+ −−−−−−→ Vectk(U, U′′)
294
+ C ⊗ C′ ψ⊗ψ′
295
+ −−−−→ Vectk(AL, A′
296
+ L) ⊗ Vectk(A′
297
+ L, A′′
298
+ L)
299
+
300
+ −−−−−−→ Vectk(AL, A′′
301
+ L)
302
+ (2.16)
303
+ 4
304
+
305
+ give coalgebra measurings from U to U′′ and from AL to A′′
306
+ L respectively. For c ⊗ c′ ∈ C ⊗ C′ and u ∈ U, we also see that
307
+ ∆′′
308
+ L((c ⊗ c′)(u)) = ∆′′
309
+ L(c′(c(u)))
310
+ = c′
311
+ (1)(c(u)(1)) ⊗ c′
312
+ (2)(c(u)(2))
313
+ = c′
314
+ (1)(x(1)(u(1))) ⊗ c′
315
+ (2)(x(2)(u(2)))
316
+ = (c′ ⊗ c)(1)(u(1)) ⊗ (c′ ⊗ c)(2)(u(2))
317
+ (2.17)
318
+ It is also clear that the morphism in (2.15) satisfies all the other conditions in Definition 2.3. This proves the result.
319
+
320
+ Theorem 2.7. The category HAlgk of Hopf algebroids is enriched over the category CoCoalgk of cocommutative k-coalgebras.
321
+ Proof. Given Hopf algebroids U = (UL, S ) and U′ = (U′
322
+ L, S ′), we consider the “hom object” Mc(U, U′) which lies in CoCoalgk.
323
+ The composition of these hom objects is obtained as follows: if U, U′ and U′′ are Hopf algebroids, we obtain as in Proposition
324
+ 2.6 a measuring
325
+ Mc(U, U′) ⊗ Mc(U′, U′′) −→ V(U, U′′)
326
+ (2.18)
327
+ Applying the universal property in Proposition 2.5, we now have a morphism of coalgebras Mc(U, U′) ⊗ Mc(U′, U′′) −→
328
+ Mc(U, U′′). The unit object in CoCoalgk is k treated as a coalgebra over itself. Then, we have a unit map
329
+ k ��→ V(U, U) ⊆ Vectk(U, U) × Vectk(AL, AL)
330
+ t �→ (t · iduL, t · idAL)
331
+ (2.19)
332
+ which induces a morphism k −→ Mc(U, U) of cocommutative coalgebras. Together with the composition of hom objects in
333
+ (2.18), we see that HAlgk is enriched over CoCoalgk.
334
+
335
+ From now onwards, we will denote by HALGk the category of Hopf algebroids enriched over the symmetric monoidal category
336
+ CoCoalgk of cocommutative k-algebras.
337
+ 3
338
+ Morphisms on cyclic (co)homology and Hopf-Galois maps
339
+ Let U = (UL, S ) = (U, AL, sL, tL, ∆L, ǫL) be a Hopf algebroid over k. We now recall from [13, § 2] the cocyclic module C•(U)
340
+ that computes the cyclic cohomology of the Hopf algebroid U. For n ≥ 1, we put
341
+ Cn(U) := U ⊗AL ⊗ · · · ⊗AL U
342
+ ��������������������������������������
343
+ n-times
344
+ (3.1)
345
+ and set C0(U) := AL. For n ≥ 1, the face maps δi : Cn(U) −→ Cn+1(U) are defined by
346
+ δi(u1 ⊗ ... ⊗ un) :=
347
+ 
348
+ 1 ⊗ u1 ⊗ ... ⊗ un
349
+ if i = 0
350
+ u1 ⊗ .... ⊗ ∆Lui ⊗ ... ⊗ un
351
+ if 1 ≤ i ≤ n
352
+ u1 ⊗ .... ⊗ un ⊗ 1
353
+ if i = n + 1
354
+ (3.2)
355
+ For n = 0, there are two maps δ0 := tL : C0(U) = AL −→ C1(U) = U and δ1 := sL : C0(U) = AL −→ C1(U) = U. The
356
+ degeneracy maps σi : Cn(U) −→ Cn−1(U) are given by
357
+ σi(u1 ⊗ ... ⊗ un) := u1 ⊗ ... ⊗ ǫL(ui+1) · ui+2 ⊗ ... ⊗ un
358
+ 0 ≤ i ≤ n − 1
359
+ (3.3)
360
+ The cyclic operator τn : Cn(U) −→ Cn(U) is defined by setting
361
+ τn(u1 ⊗ ... ⊗ un) := (S (u1)(1) · u2) ⊗ .... ⊗ (S (u1)(n−1) · un) ⊗ S (u1)(n)
362
+ (3.4)
363
+ Since we have assumed that the antipode S is involutive, it follows from [13, Theorem 2.1] that C•(U) is indeed a cocyclic
364
+ module. We will denote by HC•(U) the cyclic cohomology groups of the Hopf algebroid U by U. The Hochschild cohomology
365
+ groups of the Hopf algebroid U will then be denoted by HH•(U).
366
+ 5
367
+
368
+ Let U, U′ be Hopf algebroids and let (Ψ, ψ) : C −→ V(U, U′) be a measuring from U to U′. For each x ∈ C, we now define a
369
+ family of morphisms
370
+ Ψ
371
+ n(x) : Cn(U) −→ Cn(U′)
372
+ Ψ
373
+ n(x)(u1 ⊗ ... ⊗ un) := x(u1 ⊗ ... ⊗ un) = x(1)(u1) ⊗ ... ⊗ x(n)(un)
374
+ ∀ n ≥ 0
375
+ (3.5)
376
+ We now prove the first main result of this section.
377
+ Proposition 3.1. Let C be a cocommutative coalgebra and let (Ψ, ψ) : C −→ V(U, U′) be a measuring of Hopf algebroids.
378
+ For each x ∈ C, the family {Ψ
379
+ n(x) : Cn(U) −→ Cn(U′)}n≥0 gives a morphism of cyclic modules. In particular, we have induced
380
+ morphisms
381
+ Ψ
382
+
383
+ hoc(x) : HH•(U) −→ HH•(U)
384
+ Ψ
385
+
386
+ cy(x) : HC•(U) −→ HC•(U)
387
+ (3.6)
388
+ on Hochschild and cyclic cohomologies for each x ∈ C.
389
+ Proof. For each x ∈ C, we start by showing that Ψ
390
+ n+1(x) ◦ δi = δ′
391
+ i ◦ Ψ
392
+ n(x) : Cn(U) −→ Cn+1(H ′), where δi and δ′
393
+ i are the face
394
+ maps on the respective cocyclic modules C•(U) and C•(U′). If i = 0 or i = n + 1, this is immediately clear from the definition
395
+ in (3.2) and the action in (3.5). For 1 ≤ i ≤ n, we see that
396
+ Ψ
397
+ n+1(x) ◦ δi(u1 ⊗ ... ⊗ un)
398
+ = Ψ
399
+ n+1(x)(u1 ⊗ .... ⊗ ∆Lui ⊗ ... ⊗ un)
400
+ = x(1)(u1) ⊗ ... ⊗ x(i)(ui
401
+ (1)) ⊗ x(i+1)(ui
402
+ (2)) ⊗ .... ⊗ x(n+1)(un)
403
+ = x(1)(u1) ⊗ ∆L(x(i)(ui)) ⊗ ... ⊗ x(n)(un) = δ′
404
+ i ◦ Ψ
405
+ n(x)(u1 ⊗ ... ⊗ un)
406
+ Next, we verify that Ψ
407
+ n−1(x) ◦ σi = σ′
408
+ i ◦ Ψ
409
+ n(x), where σi and σ′
410
+ i are the degeneracies on the respective cocyclic modules C•(U)
411
+ and C•(U′).
412
+ Ψ
413
+ n−1(x) ◦ σi(u1 ⊗ ... ⊗ un)
414
+ = Ψ
415
+ n−1(x)(u1 ⊗ ... ⊗ ǫL(ui+1) · ui+2 ⊗ ... ⊗ un)
416
+ = x(1)(u1) ⊗ ... ⊗ x(i+1)(ǫL(ui+1) · ui+2) ⊗ ... ⊗ x(n−1)(un)
417
+ = x(1)(u1) ⊗ ... ⊗ x(i+1)(ǫL(ui+1)) · x(i+2)(ui+2) ⊗ ... ⊗ x(n)(un)
418
+ = x(1)(u1) ⊗ ... ⊗ ǫL(x(i+1)(ui+1)) · x(i+2)(ui+2) ⊗ ... ⊗ x(n)(un)
419
+ = σ′
420
+ i ◦ Ψ
421
+ n(x)(u1 ⊗ ... ⊗ un)
422
+ Finally, we show that Ψ
423
+ n(x)◦τn = τ′
424
+ n ◦Ψ
425
+ n(x), where τn and τ′
426
+ n are the cyclic operators on the respective cocyclic modules C•(U)
427
+ and C•(U′).
428
+ Ψ
429
+ n(x) ◦ τn(u1 ⊗ ... ⊗ un)
430
+ = Ψ
431
+ n(x)((S (u1)(1) · u2) ⊗ .... ⊗ (S (u1)(n−1) · un) ⊗ S (u1)(n))
432
+ = x(1)((S (u1)(1) · u2)) ⊗ .... ⊗ x(n−1)((S (u1)(n−1) · un) ⊗ x(n)(S (u1)(n))
433
+ = x(1)(S (u1)(1)) · x(2)(u2) ⊗ .... ⊗ x(2n−3)(S (u1)(n−1)) · x(2n−2)(un) ⊗ x(2n−1)(S (u1)(n))
434
+ = x(1)(S (u1)(1)) · x(n+1)(u2) ⊗ .... ⊗ x(n−1)(S (u1)(n−1)) · x(2n−1)(un) ⊗ x(n)(S (u1)(n))
435
+ = (x(1)(S (u1)))(1) · x(2)(u2) ⊗ .... ⊗ (x(1)(S (u1)))(n−1) · x(n)(un) ⊗ (x(1)(S (u1)))(n)
436
+ = (S (x(1)(u1)))(1) · x(2)(u2) ⊗ .... ⊗ (S (x(1)(u1)))(n−1) · x(n)(un) ⊗ (S (x(1)(u1)))(n)
437
+ = τ′
438
+ n ◦ Ψ
439
+ n(x)(u1 ⊗ ... ⊗ un)
440
+
441
+ We continue with a Hopf algebroid U = (UL, S ) = (U, AL, sL, tL, ∆L, ǫL). As mentioned in Section 2, we set AR := Aop
442
+ L = Aop.
443
+ Following [5, § 4], we also set
444
+ sR := tL
445
+ tR := S ◦ tL = sL
446
+ (3.7)
447
+ Then, U becomes an (AR, AR)-bimodule by right multiplication as follows
448
+ a1 · h · a2 := hsR(a2)tR(a1) = htL(a2)sL(a1)
449
+ h ∈ H, a1, a2 ∈ AR
450
+ (3.8)
451
+ We now consider
452
+ S rl : H ⊗AR H −→ H ⊗AL H
453
+ u1 ⊗ u2 �→ S (u2) ⊗ S (u1)
454
+ S lr := S −1
455
+ rl : H ⊗AL H −→ H ⊗AR H
456
+ u1 ⊗ u2 �→ S (u2) ⊗ S (u1)
457
+ (3.9)
458
+ 6
459
+
460
+ as well as
461
+ ∆R := S lr ◦ ∆L ◦ S : U −→ U ⊗AR U
462
+ ǫR := ǫL ◦ S : U −→ AR
463
+ (3.10)
464
+ We know from [5, § 4] that the datum UR := (U, AR, sR, tR, ∆R, ǫR) defines a right bialgebroid over k. We now adopt the Sweedler
465
+ notation ∆R(u) := u[1] ⊗ u[2] for any u ∈ U in order to distinguish it from the left coproduct ∆L(u) = u(1) ⊗ u(2). More explicitly,
466
+ we have
467
+ ∆R(u) = u[1] ⊗ u[2] = S (S (u)(2)) ⊗ S (S (u)(1))
468
+ ∀ u ∈ U
469
+ (3.11)
470
+ Now let U, U′ be Hopf algebroids and consider (F, f) ∈ V(U, U′). From the conditions in (2.11) and the definitions in (3.7) and
471
+ (3.10), we already have
472
+ FsR = s′
473
+ R f
474
+ FtR = t′
475
+ R f
476
+ FS = S ′F
477
+ fǫR = ǫ′
478
+ RF
479
+ (3.12)
480
+ We now need the following result.
481
+ Lemma 3.2. Let C be a cocommutative coalgebra and (Ψ, ψ) : C −→ V(U, U′) a measuring of Hopf algebroids. Then, for
482
+ each x ∈ C, there is a well defined morphism
483
+ x : U −→ U ⊗AR U
484
+ u1 ⊗ u2 �→ x(1)(u1) ⊗ x(2)(u2)
485
+ (3.13)
486
+ which fits into the following commutative diagram
487
+ U
488
+ ∆R
489
+ −−−−−−→ U ⊗AR U
490
+ x
491
+ �
492
+ �x
493
+ U′
494
+ ∆′
495
+ R
496
+ −−−−−−→ U′ ⊗A′
497
+ R U′
498
+ (3.14)
499
+ Proof. We consider u1, u2 ∈ uL and a ∈ AR. Using the fact that Ψ : C −→ Vectk(U, U′) is a measuring and applying the
500
+ conditions in (3.12), we see that
501
+ c((u1 · a) ⊗ u2) = c(u1sR(a) ⊗ u2)
502
+ = x(1)(u1sR(a)) ⊗ x(2)(u2) = x(1)(u1)x(2)(sR(a)) ⊗ x(3)(u2)
503
+ = x(1)(u1)s′
504
+ R(x(2)(a)) ⊗ x(3)(u2)
505
+ = x(1)(u1) · x(2)(a) ⊗ x(3)(u2)
506
+ = x(1)(u1) ⊗ x(2)(a) · x(3)(u2) = x(1)(u1) ⊗ x(3)(u2)t′
507
+ R(x(2)(a))
508
+ = x(1)(u1) ⊗ x(3)(u2)x(2)(tR(a))
509
+ = x(1)(u1) ⊗ x(2)(u2)x(3)(tR(a))
510
+ (as C is cocommutative)
511
+ = x(1)(u1) ⊗ x(2)(u2tR(a)) = x(1)(u1) ⊗ x(2)(a · u2) = c(u1 ⊗ (a · u2))
512
+ It follows that the morphism in (3.13) is well defined. It remains to verify the condition in (3.14). For u ∈ U and x ∈ C, we
513
+ have
514
+ c(∆R(u)) = c(S (S (u)(2)) ⊗ S (S (u)(1)))
515
+ = x(1)(S (S (u)(2))) ⊗ x(2)(S (S (u)(1)))
516
+ = S ′(x(1)(S (u)(2))) ⊗ S ′(x(2)(S (u)(1)))
517
+ = S ′(x(2)(S (u)(2))) ⊗ S ′(x(1)(S (u)(1)))
518
+ (as C is cocommutative)
519
+ = S ′(c(S (u))(2)) ⊗ S ′(c(S (u))(1))
520
+ = S ′(S ′(c(u))(2)) ⊗ S ′(S ′(c(u))(1)) = ∆′
521
+ R(c(u))
522
+
523
+ We now recall from [13, § 2.3.1] the cyclic module C•(U) defining the cyclic homology of a Hopf algebroid U. For n ≥ 0, we
524
+ set
525
+ Cn(U) := U ⊗AR ⊗ · · · ⊗AR U
526
+ ��������������������������������������
527
+ n-times
528
+ (3.15)
529
+ 7
530
+
531
+ and C0(U) := AR. The face maps di : Cn(U) −→ Cn−1(U) are defined by setting
532
+ di(u1 ⊗ ... ⊗ un) :=
533
+ 
534
+ ǫR(u1)u2 ⊗ ... ⊗ un
535
+ if i = 0
536
+ u1 ⊗ ... ⊗ uiui+1 ⊗ ... ⊗ un
537
+ if i ≤ i ≤ n − 1
538
+ u1 ⊗ ... ⊗ un−1ǫR(S (un))
539
+ if i = n
540
+ (3.16)
541
+ The degeneracies si : Cn(U) −→ Cn+1(U) are defined as
542
+ si(u1 ⊗ ... ⊗ un) :=
543
+ � 1 ⊗ u1 ⊗ ... ⊗ un
544
+ if i = 0
545
+ u1 ⊗ ... ⊗ ui ⊗ 1 ⊗ ui+1 ⊗ .... ⊗ un
546
+ if 1 ≤ i ≤ n
547
+ (3.17)
548
+ The cyclic operators tn : Cn(U) −→ Cn(U) are given by
549
+ tn(u1 ⊗ ... ⊗ un) := S (u1
550
+ (2)...un−1
551
+ (2) un) ⊗ u1
552
+ (1) ⊗ u2
553
+ (1) ⊗ ... ⊗ un−1
554
+ (1)
555
+ (3.18)
556
+ The Hochschild homology groups of the Hopf algebroid U will then be denoted by HH•(U) and the cyclic homology groups
557
+ by HC•(U). We will now prove the homological counterpart for Proposition 3.1.
558
+ Proposition 3.3. Let C be a cocommutative coalgebra and let (Ψ, ψ) : C −→ V(U, U′) be a measuring of Hopf algebroids. For
559
+ each x ∈ C, the family
560
+ Ψn(x) : Cn(U) −→ Cn(U′)
561
+ u1 ⊗ ... ⊗ un �→ x(u1 ⊗ ... ⊗ un) = x(1)(u1) ⊗ ... ⊗ x(n)(un)
562
+ (3.19)
563
+ for n ≥ 0 gives a morphism of cyclic modules. In particular, we have induced morphisms
564
+ Ψhoc
565
+ • (x) : HH•(U) −→ HH•(U′)
566
+ Ψcy
567
+ • (x) : HC•(U) −→ HC•(U′)
568
+ (3.20)
569
+ on Hochschild and cyclic homologies for each x ∈ C.
570
+ Proof. Using the properties in (3.12) and the fact that Ψ : C −→ Vectk(U, U′) is a measuring, it may easily be verified that the
571
+ maps Ψ•(x) commute with the respective face maps and degeneracy maps on the cyclic modules C•(U) and C•(U′). Moreover,
572
+ if tn and t′
573
+ n are the respective cyclic operators on C•(U) and C•(U′), we have for each x ∈ C
574
+ c(tn(u1 ⊗ ... ⊗ un))
575
+ = c(S (u1
576
+ (2)...un−1
577
+ (2) un) ⊗ u1
578
+ (1) ⊗ u2
579
+ (1) ⊗ ... ⊗ un−1
580
+ (1) )
581
+ = x(1)(S (u1
582
+ (2)...un−1
583
+ (2) un)) ⊗ x(2)(u1
584
+ (1)) ⊗ x(3)(u2
585
+ (1)) ⊗ ... ⊗ x(n)(un−1
586
+ (1) )
587
+ = S ′(x(1)(u1
588
+ (2))...x(n−1)(un−1
589
+ (2) )x(n)(un)) ⊗ x(n+1)(u1
590
+ (1)) ⊗ ... ⊗ x(2n−1)(un−1
591
+ (1) )
592
+ = S ′(x(2)(u1
593
+ (2))...x(2n−2)(un−1
594
+ (2) )x(2n−1)(un)) ⊗ x(1)(u1
595
+ (1)) ⊗ ... ⊗ x(2n−3)(un−1
596
+ (1) )
597
+ = S ′(x(1)(u1)(2)...x(n−1)(un−1)(2)x(n)(un)) ⊗ x(1)(u1)(1) ⊗ ... ⊗ x(n−1)(un−1)(1)
598
+ = t′
599
+ n(x(1)(u1) ⊗ ... ⊗ x(n)(un))
600
+
601
+ Our final aim in this section is to show that the morphisms induced by a measuring of Hopf algebroids are well behaved with
602
+ respect to cyclic duality. More precisely, we know from [13, § 2.3.3] that there are Hopf-Galois maps
603
+ ξn(U) : Cn(U)
604
+
605
+ −→ Cn(U)
606
+ u1 ⊗ ... ⊗ un �→ u1
607
+ (1) ⊗ u1
608
+ (2)u2
609
+ (1) ⊗ u1
610
+ (3)u2
611
+ (2)u3
612
+ (1) ⊗ ... ⊗ u1
613
+ (n)u2
614
+ (n−1)....un−1
615
+ (2) un
616
+ (3.21)
617
+ inducing isomorphisms between C•(U) and C•(U). We now have the following result.
618
+ Proposition 3.4. Let C be a cocommutative coalgebra and let (Ψ, ψ) : C −→ V(U, U′) be a measuring of Hopf algebroids.
619
+ Then for each x ∈ C, the following diagram commutes
620
+ Cn(U)
621
+ ξn(U)
622
+ −−−−−−→ Cn(U)
623
+ Ψn(x)
624
+ �
625
+ �Ψ
626
+ n(x)
627
+ Cn(U)
628
+ ξn(U)
629
+ −−−−−−→ Cn(U)
630
+ (3.22)
631
+ 8
632
+
633
+ Proof. We put N := n(n + 1)/2. Using the fact that Ψ : C −→ Vectk(U, U′) is a measuring and that C is cocommutative we
634
+ have
635
+ c(ξn(U)(u1 ⊗ ... ⊗ un))
636
+ = c(u1
637
+ (1) ⊗ u1
638
+ (2)u2
639
+ (1) ⊗ u1
640
+ (3)u2
641
+ (2)u3
642
+ (1) ⊗ ... ⊗ u1
643
+ (n)u2
644
+ (n−1)....un−1
645
+ (2) un)
646
+ = x(1)(u1
647
+ (1)) ⊗ x(2)(u1
648
+ (2))x(3)(u2
649
+ (1)) ⊗ ... ⊗ x(N+1−n)(u1
650
+ (n))....x(N−1)(un−1
651
+ (2) )x(N)(un)
652
+ = x(1)(u1
653
+ (1)) ⊗ x(2)(u1
654
+ (2))x(n+1)(u2
655
+ (1)) ⊗ ... ⊗ x(n)(u1
656
+ (n))....x(N−1)(un−1
657
+ (2) )x(N)(un)
658
+ = ξn(U′)(x(1)(u1) ⊗ ... ⊗ x(n)(un))
659
+ This proves the result.
660
+
661
+ 4
662
+ Shuffle products and the enrichment of the category of commutative Hopf alge-
663
+ broids
664
+ We recall from Section 2 the category HALGk of Hopf algebroids over k, enriched over the symmetric monoidal category
665
+ of CoCoalgk of cocommutative k-coalgebras.
666
+ By a commutative Hopf algebroid, we will mean a Hopf algebroid U =
667
+ (U, AL, sL, tL, ∆L, ǫL) such that H and AL = A = AR are commutative rings.
668
+ Let cHALGk denote the full subcategory of HALGk consisting of commutative Hopf algebroids. Then, cHALGk is also en-
669
+ riched over CoCoalgk. In this section, we will obtain a second enrichment of commutative Hopf algebroids in cocommutative
670
+ coalgebras, by using the shuffle product in Hochschild homology.
671
+ We know from [17, § 4.2] that the Hochschild homology of a commutative algebra is equipped with a shuffle product structure.
672
+ For a commutative Hopf algebroid U = (U, AL, sL, tL, ∆L, ǫL), we now recall from [15, § 4.4.1] the (p, q)-shuffle product
673
+ shpq(U) : Cp(U) ⊗ Cq(U) −→ Cp+q(U)
674
+ (4.1)
675
+ which is given by the formula (for p, q ≥ 1)
676
+ shpq(U)((u1 ⊗ ... ⊗ up) ⊗ (up+1 ⊗ ... ⊗ up+q)) :=
677
+
678
+ σ∈S h(p,q)
679
+ sgn(σ)(uσ−1(1) ⊗ ... ⊗ uσ−1(p+q))
680
+ (4.2)
681
+ Here S h(p, q) is the set of (p, q)-shuffles, i.e.,
682
+ S h(p, q) := {σ ∈ S p+q | σ(1) < ... < σ(p); σ(p + 1) < ... < σ(p + q)}
683
+ (4.3)
684
+ For p = q = 0, the shuffle product is given by setting sh00(U) to be the multiplication on A. Further, one has (see [15, § 4.4.1])
685
+ shp0(U) : Cp(U) ⊗ C0(U) −→ Cp(U)
686
+ (u1 ⊗ ... ⊗ up) ⊗ a �→ (tL(a)u1 ⊗ ... ⊗ up)
687
+ sh0q(U) : C0(U) ⊗ Cq(U) −→ Cq(U)
688
+ a ⊗ (u1 ⊗ ... ⊗ up) �→ (u1 ⊗ ... ⊗ uqtL(a))
689
+ (4.4)
690
+ for p ≥ 1 and q ≥ 1. There is now an induced product structure shpq(U) : HHp(U) ⊗ HHq(U) −→ HHp+q(U) which makes the
691
+ the Hochschild homology HH•(U) :=
692
+
693
+ n≥0
694
+ HHp(U) of a commutative Hopf algebroid U into a graded algebra (see [15, § 4.4.1])
695
+ that we denote by (HH•(U), sh(U)).
696
+ Proposition 4.1. Let U, U′ be commutative Hopf algebroids. Let C be a cocommutative coalgebra and let (Ψ, ψ) : C −→
697
+ V(U, U′) be a measuring of Hopf algebroids. Then, the induced K-linear map
698
+ Ψhoc : C −→ HomK(HH•(U), HH•(U′))
699
+ x �→ (Ψhoc
700
+ • (x) : HH•(U) −→ HH•(U′))
701
+ (4.5)
702
+ gives a measuring of algebras from (HH•(U), sh(U)) to (HH•(U′), sh(U′)).
703
+ 9
704
+
705
+ Proof. The unit in (HH•(U), sh(U)) is given by the class of the unit 1A ∈ A = C0(U). Since ψ : C −→ HomK(A, A′) gives in
706
+ particular a measuring from A to A′, we have Ψhoc
707
+ • (x)(1A) = 1A′. We now note that for any x ∈ C and p, q ≥ 1, we have
708
+ Ψp+q(x)(shpq(U)((u1 ⊗ ... ⊗ up) ⊗ (up+1 ⊗ ... ⊗ up+q)))
709
+ = Ψp+q(x)
710
+
711
+
712
+ σ∈S h(p,q)
713
+ sgn(σ)(uσ−1(1) ⊗ ... ⊗ uσ−1(p+q))
714
+
715
+ =
716
+
717
+ σ∈S h(p,q)
718
+ sgn(σ)(x(1)(uσ−1(1)) ⊗ ... ⊗ x(p+q)(uσ−1(p+q)))
719
+ =
720
+
721
+ σ∈S h(p,q)
722
+ sgn(σ)(xσ−1(1)(uσ−1(1)) ⊗ ... ⊗ xσ−1(p+q)(uσ−1(p+q)))
723
+ (because C is cocommutative)
724
+ = shpq(U)((x(1)(u1) ⊗ ... ⊗ x(p)(up)) ⊗ (x(p+1)(up+1) ⊗ ... ⊗ x(p+q)(up+q)))
725
+ (4.6)
726
+ For p ≥ 1, we have
727
+ Ψp(x)(shp0(U)((u1 ⊗ ... ⊗ up) ⊗ a)
728
+ = Ψp(x)((tL(a)u1 ⊗ ... ⊗ up))
729
+ = (x(1)(tL(a)u1) ⊗ ... ⊗ x(p)(up))
730
+ = (x(1)(tL(a))x(2)(u1) ⊗ ... ⊗ x(p+1)(up))
731
+ = (tL(x(p+1)(a)))x(1)(u1) ⊗ ... ⊗ x(p)(up))
732
+ = shp0(U)((x(1)(u1) ⊗ ... ⊗ x(p)(up)) ⊗ x(p+1)(a))
733
+ (4.7)
734
+ We can similarly verify the case for sh0q with q ≥ 1 and for sh00. This proves the result.
735
+
736
+ Our next objective is to use Proposition 4.1 to obtain an enrichment of commutative Hopf algebroids over the category of
737
+ cocommutative coalgebras. For that we recall the following fact: if R, R′ are k-algebras, the category of coalgebra measurings
738
+ from R to R′ contains a final object ϕ(R, R′) : M(R, R′) −→ Vectk(R, R′) (see Sweedler [20]). Then, M(R, R′) is known as the
739
+ universal measuring coalgebra. We let Mc(R, R′) be the cocommutative part of the coalgebra M(R, R′). Then, the restriction
740
+ ϕc(R, R′) : Mc(R, R′) ֒→ M(R, R′) −→ Vectk(R, R′) becomes the final object in the category of cocommutative coalgebra
741
+ measurings from R to R′ (see [9, Proposition 1.4], [10]). Further, the objects Mc(R, R′) give an enrichment of k-algebras over
742
+ cocommutative k-coalgebras.
743
+ We now define the enriched category
744
+
745
+ cHALGk whose objects are commutative Hopf algebroids over k and whose hom-objects
746
+ are defined by setting
747
+
748
+ cHALGk(U, U′) := Mc((HH•(U), sh(U)), (HH•(U′), sh(U′))) ∈ CoCoalgk
749
+ (4.8)
750
+ for commutative Hopf algebroids U, U′. Since each (HH•(U), sh(U)) is an algebra, we also have a canonical morphism k −→
751
+ Mc((HH•(U), sh(U)), (HH•(U), sh(U))) of cocommutative coalgebras.
752
+ Lemma 4.2. Let U, U′ be commutative Hopf algebroids. Then, there is a canonical morphism of cocommutative coalgebras
753
+ τ(U, U′) : Mc(U, U′) −→ Mc((HH•(U), sh(U)), (HH•(U′), sh(U′)))
754
+ (4.9)
755
+ Proof. By definition, (Φ, φ) : Mc(U, U′) −→ V(U, U′) is a cocommutative measuring from U to U′. By Proposition 4.1,
756
+ this induces a measuring of algebras from (HH•(U), sh(U)) to (HH•(U′), sh(U′)). By the universal property of the universal
757
+ cocommutative measuring coalgebra Mc((HH•(U), sh(U)), (HH•(U′), sh(U′))), we now obtain an induced morphism τ(U, U′)
758
+ as in (4.9).
759
+
760
+ Theorem 4.3. There is a CoCoalgk enriched functor cHALGk −→
761
+
762
+ cHALGk which is identity on objects and whose mapping
763
+ on hom-objects is given by
764
+ τ(U, U′) : cHALGk(U, U′) = Mc(U, U′) −→ Mc((HH•(U), sh(U)), (HH•(U′), sh(U′))) =
765
+
766
+ cHALGk(U, U′)
767
+ (4.10)
768
+ for commutative Hopf algebroids U, U′ over k.
769
+ 10
770
+
771
+ Proof. Let U, U′, U′′ be commutative Hopf algebroids. We show that the following diagram commutes
772
+ Mc(U, U′) ⊗ Mc(U′, U′′)
773
+
774
+ −−−−−−→
775
+ Mc(U, U′′)
776
+ τ(U,U′)⊗τ(U′,U′′)
777
+ �
778
+ �τ(U,U′′)
779
+ Mc(HH•(U), HH•(U′)) ⊗ Mc(HH•(U′), HH•(U′′))
780
+
781
+ −−−−−−→ Mc(HH•(U), HH•(U′′))
782
+ (4.11)
783
+ The top horizontal composition ◦ : Mc(U, U′) ⊗ Mc(U′, U′′) −→ Mc(U, U′′) in (4.11) is obtained from Theorem 2.7, while the
784
+ bottom horizontal composition ◦ : Mc(HH•(U), HH•(U′)) ⊗ Mc(HH•(U′), HH•(U′′)) −→ Mc(HH•(U), HH•(U′′)) is obtained
785
+ from the enrichment of algebras in cocommutative coalgebras.
786
+ From Lemma 4.2 and Theorem 2.7, we note that all the maps in (4.11) are morphisms of cocommutative coalgebras. It follows
787
+ from the property of the universal cocommutative measuring coalgebra Mc(HH•(U), HH•(U′′)) that in order to show that (4.11)
788
+ commutes, it suffices to verify that the following two compositions are equal
789
+ Mc(U, U′) ⊗ Mc(U′, U′′)
790
+ τ(U,U′)⊗τ(U′,U′′)
791
+ �
792
+ Mc(HH•(U), HH•(U′)) ⊗ Mc(HH•(U′), HH•(U′′))
793
+
794
+ �
795
+ Mc(HH•(U), HH•(U′′))
796
+ �ϕc(HH•(U),HH•(U′′))
797
+ Vectk(HH•(U), HH•(U′′))
798
+ Mc(U, U′) ⊗ Mc(U′, U′′)
799
+ �◦
800
+ Mc(U, U′′)
801
+ �τ(U,U′′)
802
+ Mc(HH•(U), HH•(U′′))
803
+ �ϕc(HH•(U),HH•(U′′))
804
+ Vectk(HH•(U), HH•(U′′))
805
+ (4.12)
806
+ For the sake of convenience, we denote the left vertical composition in (4.12) by ψ1 and the right vertical composition by ψ2.
807
+ We now consider x ∈ Mc(U, U′), y ∈ Mc(U′, U′′) and (u1 ⊗ ... ⊗ up) ∈ Cp(U). We see that
808
+ ψ2(x ⊗ y)(u1 ⊗ ... ⊗ up)
809
+ = (y ◦ x)(u1 ⊗ ... ⊗ up)
810
+ = (y ◦ x)(1)(u1) ⊗ ... ⊗ (y ◦ x)(p)(up)
811
+ (4.13)
812
+ Since ◦ : Mc(U, U′) ⊗ Mc(U′, U′′) −→ Mc(U, U′′) is a morphism of coalgebras, we note that (y ◦ x)(1) ⊗ ... ⊗ (y ◦ x)(p) =
813
+ (y(1) ◦ x(1)) ⊗ ... ⊗ (y(p) ◦ x(p)). Combining with (4.13), we see that the right vertical composition in (4.12) may be described
814
+ explicitly as
815
+ ψ2(x ⊗ y)(u1 ⊗ ... ⊗ up) = (y(1) ◦ x(1))(u1) ⊗ ... ⊗ (y(p) ◦ x(p))(up) = y(1)(x(1)(u1)) ⊗ ... ⊗ y(p)(x(p)(up))
816
+ (4.14)
817
+ On the other hand, we note that the following diagram is commutative
818
+ Mc(U, U′) ⊗ Mc(U′, U′′)
819
+ ◦(τ(U,U′)⊗τ(U′,U′′))
820
+ −−−−−−−−−−−−−−−−→
821
+ Mc(HH•(U), HH•(U′′))
822
+ (ϕc(HH•(U),HH•(U′))◦τ(U,U′))⊗
823
+ �(ϕc(HH•(U′),HH•(U′′))◦τ(U′,U′′))
824
+ ϕc(HH•(U),HH•(U′′))
825
+ �
826
+ Vectk(HH•(U), HH•(U′)) ⊗ Vectk(HH•(U′), HH•(U′′))
827
+
828
+ −−−−−−→
829
+ Vectk(HH•(U), HH•(U′′))
830
+ (4.15)
831
+ From (4.15), it follows that the left vertical composition in (4.12) may be described explicitly as
832
+ ψ1(x ⊗ y)(u1 ⊗ ... ⊗ up)
833
+ = y(x(u1 ⊗ ... ⊗ up))
834
+ = y(1)(x(1)(u1)) ⊗ ... ⊗ y(p)(x(p)(up))
835
+ (4.16)
836
+ From (4.14) and (4.16), we see that ψ1 = ψ2 and hence the diagram (4.11) commutes. Similarly by considering the coalgebra k
837
+ and using the fact that the p-th iterated coproduct ∆p(1) = 1 ⊗ ... ⊗ 1(p-times), we see that the following compositions are equal
838
+ k −→ Mc(HH•(U), HH•(U))
839
+ ϕc(HH•(U),HH•(U))
840
+ −−−−−−−−−−−−−−−→ Vectk(HH•(U), HH•(U))
841
+ k −→ Mc(U, U)
842
+ τ(U,U)
843
+ −−−−−→ Mc(HH•(U), HH•(U))
844
+ ϕc(HH•(U),HH•(U))
845
+ −−−−−−−−−−−−−−−→ Vectk(HH•(U), HH•(U))
846
+ (4.17)
847
+ 11
848
+
849
+ It follows from (4.17) that the following diagram commutes
850
+ k
851
+
852
+ �●
853
+
854
+
855
+
856
+
857
+
858
+
859
+
860
+
861
+
862
+ Mc(HH•(U), HH•(U))
863
+ Mc(U, U)
864
+ τ(U,U)
865
+ �❧
866
+
867
+
868
+
869
+
870
+
871
+
872
+
873
+
874
+
875
+
876
+
877
+
878
+ (4.18)
879
+ This proves the result.
880
+
881
+ 5
882
+ Comodule measurings for SAYD modules
883
+ Let U = (U, AL, sL, tL, ∆L, ǫL, S ) be a Hopf algebroid. From now onwards, we set Ae := A ⊗k Aop and define
884
+ ηL : Ae = A ⊗k Aop
885
+ sL⊗tL
886
+ −−−−→ U ⊗ U −→ U
887
+ (5.1)
888
+ where the second arrow in (5.1) is the multilplication on U. Following [14, § 2], we note that there are now four commuting
889
+ actions of A on U which are denoted as follows
890
+ a ⊲ u ⊳ b := sL(a)tL(b)u
891
+ a ◮ u ◭ b := usL(b)tL(a)
892
+ a, b ∈ A, u ∈ U
893
+ (5.2)
894
+ By Definition 2.1, we then have an A-coring
895
+ ∆L : U −→ U⊳ ⊗A ⊲U
896
+ ǫL : U −→ A
897
+ (5.3)
898
+ The left action ◮ of A on U may be treated as a right action of Aop on U. Similarly, the right action ⊳ of A on U may be treated
899
+ as a left action by Aop. Accordingly, we may consider the tensor product
900
+ ◮U ⊗Aop U⊳ := U ⊗k U/span{a ◮ u ⊗ v − u ⊗ v ⊳ a | u, v ∈ U, a ∈ A}
901
+ (5.4)
902
+ There is now a Hopf-Galois map (see [5], [14], [19])
903
+ β(U) : ◮U ⊗Aop U⊳ −→ U⊳ ⊗A ⊲U
904
+ u ⊗Aop v �→ u(1) ⊗A u(2)v
905
+ (5.5)
906
+ Since U is a Hopf algebroid, it follows (see [5, Proposition 4.2]) that the morphism β(U) in (5.5) is a bijection. Accordingly, in
907
+ the notation of [14], [19], we write
908
+ u+ ⊗Aop u− := β(U)−1(u ⊗A 1)
909
+ u ∈ U
910
+ (5.6)
911
+ In this section, we will consider comodule measurings between stable anti-Yetter Drinfeld modules over Hopf algebroids. For
912
+ this, we first recall the notion of comodule measuring between ordinary modules. Let R, R′ be rings and let P, P′ be modules
913
+ over R and R′ respectively. Then, a comodule measuring from P to P′ consists of a pair of maps (see [4], [12])
914
+ ψ : C −→ Vectk(R, R′)
915
+ ω : D −→ Vectk(P, P′)
916
+ (5.7)
917
+ where C is a k-coalgebra, D is a right C-comodule, ψ : C −→ Vectk(R, R′) is a coalgebra measuring and
918
+ ω(y)(pr) = y(pr) = y(0)(p)y(1)(r) = ω(y(0))(p)ψ(y(1))(r)
919
+ (5.8)
920
+ for y ∈ D, p ∈ P and r ∈ R. For U = (U, AL, sL, tL, ∆L, ǫL, S ), we will now recall the notions of U-modules, U-comodules and
921
+ stable anti-Yetter Drinfeld modules.
922
+ Definition 5.1. (see [14, § 2.4]) Let U = (U, AL, sL, tL, ∆L, ǫL, S ) be a Hopf algebroid. A right U-module P is a right module
923
+ over the k-algebra U. Because of the ring homomorphism ηL : Ae −→ U, any right U-module P is also equipped with a right
924
+ Ae-module structure (or (A, A)-bimodule structure) given by
925
+ b ◮ p ◭ a = p(a ⊗ b) = pηL((a ⊗ 1)(1 ⊗ b)) = psL(a)tL(b)
926
+ (5.9)
927
+ for (a ⊗ b) ∈ Ae = A ⊗k Aop and p ∈ P.
928
+ 12
929
+
930
+ Definition 5.2. (see [6], [8], [14], [18]) Let U = (U, AL, sL, tL, ∆L, ǫL, S ) be a Hopf algebroid. A left U-comodule P is a left
931
+ comodule over the A-coring (U, ∆L : U −→ U ⊗AL U, ǫL : U −→ AL). In particular, a left U-comodule P is equipped with a left
932
+ A-module structure (a, p) �→ ap as well as a left A-module map
933
+ ∆P : P −→ U⊳ ⊗A P
934
+ p �→ p(−1) ⊗ p(0)
935
+ (5.10)
936
+ Following [14, § 2.5], we note that any left U-comodule P also carries a right A-module structure given by setting
937
+ pa := ǫL(p(−1)sL(a))p(0)
938
+ (5.11)
939
+ for p ∈ P, a ∈ A. This makes any left U-comodule P into a right Ae = A ⊗k Aop-module by setting
940
+ p(a ⊗ b) = bpa = bǫL(p(−1)sL(a))p(0)
941
+ (5.12)
942
+ for p ∈ P and (a ⊗ b) ∈ Ae.
943
+ Definition 5.3. (see [14, Definition 2.7]) Let U = (U, AL, sL, tL, ∆L, ǫL, S ) be a Hopf algebroid. A stable anti-Yetter Drinfeld
944
+ module (or SAYD module) P over U consists of the following
945
+ (1) A right U-module structure on P denoted by (p, u) �→ pu for p ∈ P and u ∈ U.
946
+ (2) A left U-comodule structure on P given by ∆P : P −→ U⊳ ⊗A P.
947
+ (3) The right Ae-module structure on P induced by (5.9) coincides with the right Ae-module structure on P as in (5.12):
948
+ psL(a)tL(b) = b ◮ p ◭ a = bǫL(p(−1)sL(a))p(0)
949
+ (5.13)
950
+ (4) For u ∈ U and p ∈ P, one has
951
+ ∆P(pu) = u−p(−1)u+(1) ⊗A p(0)u+(2)
952
+ (5.14)
953
+ (5) Stability condition: for any p ∈ P, one has p(0)p(−1) = p.
954
+ Lemma 5.4. Let R, R′ be k-algebras and let Re = R ⊗k Rop, R′e = R′ ⊗k R′op be their respective enveloping algebras. Let C be
955
+ a cocommutative k-coalgebra and let ψ : C −→ Vectk(R, R′) be a measuring. Then,
956
+ ψe : C −→ Vectk(Re, R′e)
957
+ ψe(c)(r ⊗ r′) = c(r1 ⊗ r2) = c(1)(r1) ⊗ c(2)(r2) = ψ(c(1))(r1) ⊗ ψ(c(2))(r2)
958
+ (5.15)
959
+ is a measuring of algebras.
960
+ Proof. From (5.15), it is immediate that c(1 ⊗ 1) = ǫC(c)(1 ⊗ 1), where ǫC is the counit on C. Since C is cocommutative, we
961
+ have for (r1 ⊗ r2), (r3 ⊗ r4) ∈ Re
962
+ c((r1 ⊗ r2)(r3 ⊗ r4)) = c(r1r3 ⊗ r4r2)
963
+ = c(1)(r1r3) ⊗ c(2)(r4r2)
964
+ = c(1)(r1)c(2)(r3) ⊗ c(3)(r4)c(4)(r2)
965
+ = c(1)(r1)c(3)(r3) ⊗ c(4)(r4)c(2)(r2)
966
+ = (c(1)(r1) ⊗ c(2)(r2))(c(3)(r3) ⊗ c(4)(r4))
967
+ = c(1)(r1 ⊗ r2)c(2)(r3 ⊗ r4)
968
+ (5.16)
969
+
970
+ Lemma 5.5. Let U = (U, S ) = (U, AL, sL, tL, ∆L, ǫL, S ) and U′ = (U′, S ′) = (U′, AL, s′
971
+ L, t′
972
+ L, ∆′
973
+ L, ǫ′
974
+ L, S ′) be Hopf algebroids over
975
+ k. Let P (resp. P′) be an SAYD-module over U (resp. U′). Let C be a cocommutative k-coalgebra and D be a right C-comodule.
976
+ Suppose that we are given the following data
977
+ Ψ : C −→ Vectk(U, U′)
978
+ ψ : C −→ Vectk(A, A′)
979
+ Ω : D −→ Vectk(P, P′)
980
+ (5.17)
981
+ such that
982
+ 13
983
+
984
+ (1) (Ψ, ψ) is a measuring of Hopf algebroids from U to U′.
985
+ (2) (Ψ, Ω) is a comodule measuring from the right U-module P to the right U′ module P′.
986
+ Then, we have:
987
+ (a) (ψe, Ω) is a comodule measuring from the right Ae-module P to the right A′e-module P′.
988
+ (b) For each d ∈ D, the following morphism is well-defined
989
+ d : U⊳ ⊗A P −→ U′
990
+ ⊳ ⊗A′ P′
991
+ d(u ⊗A p) := Ψ(d(1))(u) ⊗A′ Ω(d(0))(p)
992
+ (5.18)
993
+ Proof. (a) Since C is cocommutative, we already know from Lemma 5.4 that ψe : C −→ Vectk(Ae, A′e) is a coalgebra measuring
994
+ from Ae to A′e. We now consider (a ⊗ b) ∈ Ae = A ⊗k Aop. By (5.9), we know that p(a ⊗ b) = psL(a)tL(b). For any d ∈ D, we
995
+ now have
996
+ Ω(d)(p(a ⊗ b)) = Ω(d)(psL(a)tL(b))
997
+ = Ω(d(0))(p)Ψ(d(1))(sL(a)tL(b))
998
+ = Ω(d(0))(p)Ψ(d(1))(sL(a))Ψ(d(2))(tL(b))
999
+ = Ω(d(0))(p)s′
1000
+ L(ψ(d(1))(a))t′
1001
+ L(ψ(d(2))(b))
1002
+ = Ω(d(0))(p)(ψ(d(1)(a)) ⊗ ψ(d(2)(b)))
1003
+ = Ω(d(0))(p)(ψe(d(1))(a ⊗ b))
1004
+ (5.19)
1005
+ (b) Since P and P′ are SAYD modules, it follows from the definition in (5.9) and the condition in (5.13) that
1006
+ ap = ptL(a)
1007
+ a′p′ = p′t′
1008
+ L(a′)
1009
+ a ∈ A, a′ ∈ A′, p ∈ P, p′ ∈ P′
1010
+ (5.20)
1011
+ where the left hand side of the equalities in (5.20) comes from the left A-module action on P (resp. the left A′-module action
1012
+ on P′) appearing in the structure map ∆P : P −→ U⊳ ⊗A P (resp. the structure map ∆′
1013
+ P′ : P′ −→ U′
1014
+ ⊳ ⊗A′ P′). For a ∈ A, u ∈ U
1015
+ and p ∈ P, we now see that
1016
+ d(u ⊗A ap)
1017
+ = Ψ(d(1))(u) ⊗A′ Ω(d(0))(ap)
1018
+ = Ψ(d(1))(u) ⊗A′ Ω(d(0))(ptL(a))
1019
+ (using (5.20))
1020
+ = Ψ(d(2))(u) ⊗A′ Ω(d(0))(p)Ψ(d(1))(tL(a))
1021
+ = Ψ(d(2))(u) ⊗A′ Ω(d(0))(p)t′
1022
+ L(ψ(d(1))(a))
1023
+ = Ψ(d(2))(u) ⊗A′ ψ(d(1))(a)Ω(d(0))(p)
1024
+ (using (5.20))
1025
+ = Ψ(d(2))(u) ⊳ ψ(d(1))(a) ⊗A′ Ω(d(0))(p)
1026
+ = t′
1027
+ L(ψ(d(1))(a))Ψ(d(2))(u) ⊗A′ Ω(d(0))(p)
1028
+ (using (5.2))
1029
+ (5.21)
1030
+ On the other hand, we also have
1031
+ d(u ⊳ a ⊗A p)
1032
+ = d(tL(a)u ⊗A p)
1033
+ (using (5.2))
1034
+ = Ψ(d(1))(tL(a)u) ⊗A′ Ω(d(0))(p)
1035
+ = Ψ(d(1))(tL(a))Ψ(d(2))(u) ⊗A′ Ω(d(0))(p)
1036
+ = t′
1037
+ L(ψ(d(1))(a))Ψ(d(2))(u) ⊗A′ Ω(d(0))(p)
1038
+ (5.22)
1039
+ This proves the result.
1040
+
1041
+ We are now ready to introduce the notion of a comodule measuring between SAYD modules.
1042
+ Definition 5.6. Let U = (U, S ) = (U, AL, sL, tL, ∆L, ǫL, S ) and U′ = (U′, S ′) = (U′, AL, s′
1043
+ L, t′
1044
+ L, ∆′
1045
+ L, ǫ′
1046
+ L, S ′) be Hopf algebroids
1047
+ over k. Let P (resp. P′) be an SAYD-module over U (resp. U′). Let C be a cocommutative coalgebra. Then, a (right) measuring
1048
+ comodule over (C, Ψ, ψ) from P to P′ consists of the following data
1049
+ Ψ : C −→ Vectk(U, U′)
1050
+ ψ : C −→ Vectk(A, A′)
1051
+ Ω : D −→ Vectk(P, P′)
1052
+ (5.23)
1053
+ such that
1054
+ (1) (Ψ, ψ) is a measuring of Hopf algebroids from U to U′.
1055
+ 14
1056
+
1057
+ (2) (Ψ, Ω) is a comodule measuring from the right U-module P to the right U′ module P′.
1058
+ (3) For any d ∈ D, the following diagram commutes
1059
+ P
1060
+ ∆P
1061
+ −−−−−−→ U⊳ ⊗A P
1062
+ d:=Ω(d)
1063
+ �
1064
+ d
1065
+ �
1066
+ P′
1067
+ ∆′
1068
+ P′
1069
+ −−−−−−→ U′
1070
+ ⊳ ⊗A′ P′
1071
+ (5.24)
1072
+ where the right vertical morphism is as defined in (5.18)
1073
+ We will now construct universal measuring comodules. By definition, the right comodules over a k-coalgebra C are coalgebras
1074
+ over the comonad
1075
+ ⊗k C : Vectk −→ Vectk. Accordingly, the forgetful functor Comod − C −→ Vectk from the category of
1076
+ right C-comodules has a right adjoint (see, for instance, [7, § 2.4]) that we denote by RC, i.e., we have natural isomorphisms
1077
+ Vectk(D, V) � Comod − C(D, RC(V))
1078
+ (5.25)
1079
+ for any D ∈ Comod − C and V ∈ Vectk.
1080
+ Theorem 5.7. Let U = (U, AL, sL, tL, ∆L, ǫL, S ) and U′ = (U′, AL, s′
1081
+ L, t′
1082
+ L, ∆′
1083
+ L, ǫ′
1084
+ L, S ′) be Hopf algebroids over k. Let P (resp. P′)
1085
+ be an SAYD-module over U (resp. U′). Let C be a cocommutative coalgebra and (Ψ, ψ) : C −→ V(U, U′) be a measuring of
1086
+ Hopf algebroids.
1087
+ Then, there exists a measuring (C, Ψ, ψ)-comodule (QC(P, P′), Θ : QC(P, P′) −→ Vectk(P, P′)) satisfying the following property:
1088
+ given any measuring (C, Ψ, ψ)-comodule (D, Ω : D −→ Vectk(P, P′)) from P to P′, there exists a morphism χ : D −→ QC(P, P′)
1089
+ of right C-comodules such that the following diagram is commutative
1090
+ QC(P, P′)
1091
+ Θ
1092
+ � Vectk(P, P′)
1093
+ D
1094
+ χ
1095
+ �❍❍❍❍❍❍❍❍❍
1096
+
1097
+ �t
1098
+ t
1099
+ t
1100
+ t
1101
+ t
1102
+ t
1103
+ t
1104
+ t
1105
+ t
1106
+ t
1107
+ (5.26)
1108
+ Proof. We put V := Vectk(P, P′). By the adjunction in (5.25), there is a canonical morphism ρ(V) : RC(V) −→ V of vector
1109
+ spaces. We set QC(P, P′) := � Q, where the sum is taken over all right C-subcomodules over RC(V) such that the restriction
1110
+ ρ(V)|Q : Q −→ V = Vectk(P, P′) is a (C, Ψ, ψ)-comodule measuring from P to P′ in the sense of Definition 5.6. It is clear that
1111
+ Θ : ρ(V)|QC(P, P′) : QC(P, P′) −→ V = Vectk(P, P′) is a (C, Ψ, ψ)-measuring comodule.
1112
+ Additionally, given a measuring (C, Ψ, ψ)-comodule (D, Ω : D −→ Vectk(P, P′)) from P to P′, the adjunction in (5.25) gives a
1113
+ morphism χ : D −→ RC(V). But then we notice that ρ(V)|χ(D) : χ(D) −→ V is a measuring (C, Ψ, ψ)-comodule, whence it
1114
+ follows that the image χ(D) ⊆ QC(P, P′). The result is now clear.
1115
+
1116
+ Lemma 5.8. Let U = (U, AL, sL, tL, ∆L, ǫL, S ), U′ = (U′, AL, s′
1117
+ L, t′
1118
+ L, ∆′
1119
+ L, ǫ′
1120
+ L, S ′) and U′′ = (U′′, A′′
1121
+ L, s′′
1122
+ L, t′′
1123
+ L , ∆′′
1124
+ L, ǫ′′
1125
+ L , S ′′) be Hopf
1126
+ algebroids over k. Let P, P′ and P′′ be SAYD modules over U, U′ and U′′ respectively. Suppose that we have:
1127
+ (1) Ψ : C −→ Vectk(U, U′), ψ : C −→ Vectk(A, A′) and Ω : D −→ Vectk(P, P′) giving the data of a measuring comodule from
1128
+ P to P′.
1129
+ (2) Ψ′ : C′ −→ Vectk(U′, U′′), ψ′ : C′ −→ Vectk(A′, A′′) and Ω : D′ −→ Vectk(P′, P′′) giving the data of a measuring
1130
+ comodule from P′ to P′′.
1131
+ Then, the following
1132
+ (Ψ′, ψ′) ◦ (Ψ, ψ) : C ⊗ C′ (Ψ,ψ)⊗(Ψ′,ψ′)
1133
+ −−−−−−−−−−→ V(U, U′) ⊗ V(U′, U′′)
1134
+
1135
+ −→ V(U, U′′)
1136
+ Ω′ ◦ Ω : D ⊗ D′ Ω⊗Ω′
1137
+ −−−−→ Vectk(P, P′) ⊗ Vectk(P′, P′′)
1138
+ ◦−→ Vectk(P, P′′)
1139
+ (5.27)
1140
+ gives the data of a measuring comodule from P to P′′. There is also a canonical morphism of right (C ⊗ C′)-comodules
1141
+ QC(P, P′) ⊗ QC′(P′, P′′) −→ QC⊗C′(P, P′′)
1142
+ (5.28)
1143
+ 15
1144
+
1145
+ Proof. We know from Proposition 2.6 that (Ψ′, ψ′) ◦ (Ψ, ψ) : C ⊗ C′ −→ V(U, U′′) is a measuring of Hopf algebroids. It
1146
+ may also be directly verified that ((Ψ′, ψ′) ◦ (Ψ, ψ), Ω′ ◦ Ω) is a comodule measuring from the right U-module P to the right
1147
+ U′′-module P′′. To check the condition (5.24) in Definition 5.6, we observe that for any d ⊗ d′ ∈ D ⊗ D′, u ∈ U and p ∈ P:
1148
+ (d ⊗ d′)(u ⊗A p) = (d ⊗ d′)(1)(u) ⊗A′′ (d ⊗ d′)(0)(p) = d′
1149
+ (1)(d(1)(u)) ⊗A′′ d′
1150
+ (0)(d(0)(p)) = d′(d(u ⊗A p)))
1151
+ (5.29)
1152
+ Since the measurings (Ψ, ψ, Ω) and (Ψ′, ψ′, Ω′) both satisfy the condition in (5.24), it is clear that so does (Ψ′◦Ψ, ψ′ ◦ψ, Ω′ ◦Ω).
1153
+ Hence, (5.27) gives the data of a measuring comodule from P to P′′. By definition, QC(P, P′) (resp. QC′(P′, P′′)) is a measuring
1154
+ comodule from P to P′ (resp. from P′ to P′′). From (5.27) it now follows that QC(P, P′) ⊗ QC′(P′, P′′) is a measuring comodule
1155
+ from P to P′′. The morphism in (5.28) is now obtained by the universal property of QC⊗C′(P, P′′).
1156
+
1157
+ We now consider the “global category of comodules” Comodk whose objects are pairs (C, D), where C is a cocommutative k-
1158
+ coalgebra and D is a right C-comodule. A morphism (f, g) : (C, D) −→ (C′, D′) in Comodk consists of a k-coalgebra morphism
1159
+ f : C −→ C′ and a morphism g : D −→ D′ of C′-comodules, where D is treated as a C′-comodule by corestriction of scalars.
1160
+ It is clear that putting (C, D) ⊗ (C′, D′) := (C ⊗ C′, D ⊗ D′) makes Comodk into a symmetric monoidal category.
1161
+ Theorem 5.9. Let S AYDk be the category given by:
1162
+ (a) Objects: pairs (U, P), where U is a Hopf-algebroid and P is an S AYD-module over U
1163
+ (b) Hom-objects: for pairs (U, P), (U′, P′) ∈ S AYDk, we set
1164
+ S AYDk((U, P), (U′, P′)) := (Mc(U, U′), QMc(U,U′)(P, P′)) ∈ Comodk
1165
+ (5.30)
1166
+ Then, S AYDk is enriched over the symmetric monoidal category Comodk.
1167
+ Proof. For any (U, P) ∈ S AYDk, the scalar multiples of the identity map give a morphism k −→ Mc(U, U) of k-coalgebras,
1168
+ and along with the universal property in Theorem 5.7 give a morphism k −→ QMc(U,U)(P, P). We now consider (U, P), (U′, P′),
1169
+ (U′′, P′′) ∈ S AYDk. Applying Lemma 5.8 with C = Mc(U, U′) and C′ = Mc(U′, U′′), we obtain a morphism QMc(U,U′)(P, P′) ⊗
1170
+ QMc(U′,U′′)(P, P′) −→ QMc(U,U′)⊗Mc(U′,U′′)(P, P′′) of (Mc(U, U′) ⊗ Mc(U′, U′′))-comodules. From the proof of Theorem 2.7, we
1171
+ already have a morphism Mc(U, U′) ⊗ Mc(U′, U′′) −→ Mc(U, U′′) of k-coalgebras. Combining, we have a morphism
1172
+ S AYDk((U, P), (U′, P′)) ⊗ S AYDk((U′, P′), (U′′, P′′)) −→ (Mc(U, U′′), QMc(U,U′)⊗Mc(U′,U′′)(P, P′′))
1173
+ (5.31)
1174
+ in Comodk. In (5.31), QMc(U,U′)⊗Mc(U′,U′′)(P, P′′) is treated as a Mc(U, U′′)-module via the morphism Mc(U, U′)⊗Mc(U′, U′′) −→
1175
+ Mc(U, U′′) of k-coalgebras. From the proof of Theorem 2.7, we also know that the morphism Mc(U, U′) ⊗ Mc(U′, U′′) −→
1176
+ Mc(U, U′′) arises from the universal property of Mc(U, U′′) applied to the measuring Mc(U, U′) ⊗ Mc(U′, U′′) −→ V(U, U′) ⊗
1177
+ V(U′, U′′)
1178
+ ◦−→ V(U, U′′). Hence, the canonical map QMc(U,U′)⊗Mc(U′,U′′)(P, P′′) −→ Vectk(P, P′′) gives a measuring when treated
1179
+ as a Mc(U, U′′)-comodule. The universal property of QMc(U,U′′)(P, P′′) as in Theorem 5.7 now yields a morphism
1180
+ (Mc(U, U′′), QMc(U,U′)⊗Mc(U′,U′′)(P, P′′)) −→ (Mc(U, U′′), QMc(U,U′′)(P, P′′))
1181
+ (5.32)
1182
+ in Comodk. Composing (5.32) with (5.31), we obtain the required composition of Hom-objects S AYDk((U, P), (U′, P′)) ⊗
1183
+ S AYDk((U′, P′), (U′′, P′′)) −→ S AYDk((U, P), (U′′, P′′)). This proves the result.
1184
+
1185
+ 6
1186
+ Comodule measurings and morphisms on cyclic (co)homology
1187
+ Throughout this section, we fix the following: let U = (U, AL, sL, tL, ∆L, ǫL, S ), and U′ = (U′, A′
1188
+ L, s′
1189
+ L, t′
1190
+ L, ∆′
1191
+ L, ǫ′
1192
+ L, S ′) be Hopf
1193
+ algebroids over k. Let P and P′ be SAYD modules over U and U′ respectively. Let (Ψ, ψ) : C −→ V(U, U′) be a cocommutative
1194
+ measuring and let Ω : D −→ Vectk(P, P′) be a (C, Ψ, ψ)-measuring comodule from P to P′.
1195
+ Since U, U′ are Hopf algebroids, we have recalled in Section 5 that the morphisms β(U) : ◮U ⊗Aop U⊳ −→ U⊳ ⊗A ⊲U and
1196
+ β(U′) : ◮U′ ⊗A′op U′
1197
+ ⊳ −→ U′
1198
+ ⊳ ⊗A′ ⊲U′ in the notation of (5.5) are bijections. We now need the following result.
1199
+ 16
1200
+
1201
+ Lemma 6.1. For each x ∈ C, the following diagram commutes:
1202
+ U⊳ ⊗A ⊲U
1203
+ β(U)−1
1204
+ −−−−−−→
1205
+ ◮U ⊗Aop U⊳
1206
+ x
1207
+ �
1208
+ x
1209
+ �
1210
+ U′
1211
+ ⊳ ⊗A′ ⊲U′
1212
+ β(U′)−1
1213
+ −−−−−−→ ◮U′ ⊗A′op U′
1214
+
1215
+ (6.1)
1216
+ Here, the left vertical map is given by u1 ⊗A u2 �→ x(1)(u1) ⊗A′ x(2)(u2) and the right vertical map by u1 ⊗Aop u2 �→ x(1)(u1) ⊗A′op
1217
+ x(2)(u2).
1218
+ Proof. It is easy to see that the vertical morphisms in (6.1) are well-defined. Further, since β(U) and β(U′) are invertible, it
1219
+ suffices to check that the following diagram commutes
1220
+ ◮U ⊗Aop U⊳
1221
+ β(U)
1222
+ −−−−−−→ U⊳ ⊗A ⊲U
1223
+ x
1224
+ �
1225
+ �x
1226
+ ◮U′ ⊗A′op U′
1227
+
1228
+ β(U′)
1229
+ −−−−−−→ U′
1230
+ ⊳ ⊗A′ ⊲U′
1231
+ (6.2)
1232
+ We now see that for u ⊗Aop v ∈ ◮U ⊗Aop U⊳ and x ∈ C, we have
1233
+ x(β(U)(u ⊗Aop v)) = x(u(1) ⊗A u(2)v) = x(1)(u(1)) ⊗A x(2)(u(2))x(3)(v) = (x(1)(u))(1) ⊗A (x(1)(u))(2)x(2)(v) = β(U′)(x(1)(u) ⊗ x(2)(v))
1234
+ This proves the result.
1235
+
1236
+ From Lemma 6.1, it follows in the notation of (5.6) that we have
1237
+ x(1)(u+) ⊗A′op x(2)(u−) = x(u+ ⊗Aop u−) = β(U′)−1(x(u ⊗A 1)) = x(u)+ ⊗A′op x(u)−
1238
+ (6.3)
1239
+ for each u ∈ U. We now recall from [14, Theorem 4.1] that the Hochschild homology groups HH•(U; P) (resp. the cyclic
1240
+ homology groups HC•(U; P)) of U with coefficients in the SAYD module P are obtained from the cyclic module C•(U; P) :=
1241
+ P ⊗Aop (◮U⊳)⊗Aop• with operators as follows (where ¯u := u1 ⊗Aop ⊗... ⊗Aop un, p ∈ P)
1242
+ di(p ⊗Aop ¯u) :=
1243
+ 
1244
+ p ⊗Aop u1 ⊗Aop · · · ⊗Aop un−1tL(ǫL(un))
1245
+ if i = 0
1246
+ p ⊗Aop u1 ⊗Aop · · · ⊗Aop un−iun−i+1 ⊗Aop . . .
1247
+ if 1 ≤ i ≤ n − 1
1248
+ pu1 ⊗Aop u2 ⊗Aop · · · ⊗Aop un
1249
+ if i = n
1250
+ si(p ⊗Aop ¯u) :=
1251
+ 
1252
+ p ⊗Aop u1 ⊗Aop · · · ⊗Aop un ⊗Aop 1
1253
+ if i = 0
1254
+ p ⊗Aop · · · ⊗Aop un−i ⊗Aop 1 ⊗Aop un−i+1 ⊗Aop . . .
1255
+ if 1 ≤ i ≤ n − 1
1256
+ p ⊗Aop 1 ⊗Aop u1 ⊗Aop · · · ⊗Aop un
1257
+ if i = n
1258
+ tn(p ⊗Aop ¯u) := p(0)u1
1259
+ + ⊗Aop u2
1260
+ + ⊗Aop · · · ⊗Aop un
1261
+ + ⊗Aop un
1262
+ − . . .u1
1263
+ −p(−1)
1264
+ (6.4)
1265
+ We now have the following result.
1266
+ Proposition 6.2. For each y ∈ D, the family
1267
+ Ωn(y) : Cn(U; P) −→ Cn(U′; P′)
1268
+ p ⊗ u1 ⊗ ... ⊗ un �→ y(p ⊗ u1 ⊗ ... ⊗ un) = y(0)(p) ⊗ y(1)(u1) ⊗ ... ⊗ y(n)(un)
1269
+ (6.5)
1270
+ for n ≥ 0 gives a morphism of cyclic modules. In particular, we have induced morphisms
1271
+ Ωhoc
1272
+ • (y) : HH•(U; P) −→ HH•(U′; P′)
1273
+ Ωcy
1274
+ • (y) : HC•(U; P) −→ HC•(U′; P′)
1275
+ (6.6)
1276
+ on Hochschild and cyclic homologies for each y ∈ D.
1277
+ 17
1278
+
1279
+ Proof. From the fact that C is cocommutative and the conditions in Definition 5.6, it is clear that the morphisms Ωn(y) are well
1280
+ defined, as well as the fact that they commute with the face maps and degeneracies appearing in the cyclic modules C•(U; P)
1281
+ and C•(U′; P′) as in (6.4). To verify that the morphisms in (6.5) also commute with the cyclic operators, we note that for
1282
+ p ⊗Aop u1 ⊗Aop ⊗... ⊗Aop un ∈ Cn(U; P)
1283
+ y(tn(p ⊗ u1 ⊗ ... ⊗ un)) = y(p(0)u1
1284
+ + ⊗ u2
1285
+ + ⊗ · · · ⊗ un
1286
+ + ⊗ un
1287
+ − . . . u1
1288
+ −p(−1))
1289
+ = y(0)(p(0))y(1)(u1
1290
+ +) ⊗ y(2)(u2
1291
+ +) ⊗ · · · ⊗ y(n)(un
1292
+ +) ⊗ y(n+1)(un
1293
+ −) . . .y(2n)(u1
1294
+ −)y(2n+1)(p(−1))
1295
+ = y(0)(p(0))y(2)(u1
1296
+ +) ⊗ y(4)(u2
1297
+ +) ⊗ · · · ⊗ y(2n)(un
1298
+ +) ⊗ y(2n+1)(un
1299
+ −) . . . y(3)(u1
1300
+ −)y(1)(p(−1))
1301
+ (since C is cocommutative)
1302
+ = y(0)(p)(0)y(1)(u1
1303
+ +) ⊗ y(3)(u2
1304
+ +) ⊗ · · · ⊗ y(2n−1)(un
1305
+ +) ⊗ y(2n)(un
1306
+ −) . . . y(2)(u1
1307
+ −)y(0)(p)(−1)
1308
+ (using (5.24))
1309
+ = y(0)(p)(0)y(1)(u1)+ ⊗ y(2)(u2)+ ⊗ · · · ⊗ y(n)(un)+ ⊗ y(n)(un)− . . . y(1)(u1)−y(0)(p)(−1)
1310
+ (using (6.3))
1311
+ This proves the result.
1312
+
1313
+ We now come to cyclic cohomology. For this, we recall that from [14, Theorem 1.1] that the Hochschild cohomology groups
1314
+ HH•(U; P) (resp. the cyclic cohomology groups HC•(U; P)) of U with coefficients in the SAYD module P are obtained from
1315
+ the cocyclic module C•(U; P) := (⊲U⊳)⊗A• ⊗A P with operators as follows (where ¯u := u1 ⊗A ⊗... ⊗A un, p ∈ P)
1316
+ δi(¯u ⊗A p)
1317
+ =
1318
+ 
1319
+ 1 ⊗A u1 ⊗A · · · ⊗A un ⊗A p
1320
+ if i = 0
1321
+ u1 ⊗A · · · ⊗A ∆L(ui) ⊗A · · · ⊗A un ⊗A p
1322
+ if 1 ≤ i ≤ n
1323
+ u1 ⊗A · · · ⊗A un ⊗A p(−1) ⊗A p(0)
1324
+ if i = n + 1
1325
+ δi(p)
1326
+ =
1327
+ � 1 ⊗A p
1328
+ if j = 0
1329
+ p(−1) ⊗A p(0)
1330
+ if j = 1
1331
+ σi(¯u ⊗A p)
1332
+ = u1 ⊗A · · · ⊗A ǫL(ui+1) ⊗A · · · ⊗A un ⊗A p
1333
+ 0 ≤ i ≤ n − 1
1334
+ τn(¯u ⊗A p)
1335
+ = u1
1336
+ −(1)u2 ⊗A · · · ⊗A u1
1337
+ −(n−1)un ⊗A u1
1338
+ −(n)p(−1) ⊗A p(0)u1
1339
+ +
1340
+ (6.7)
1341
+ We now have the following result.
1342
+ Proposition 6.3. For each y ∈ D, the family
1343
+
1344
+ n(y) : Cn(U; P) −→ Cn(U′; P′)
1345
+ u1 ⊗ ... ⊗ un ⊗ p �→ y(u1 ⊗ ... ⊗ un ⊗ p) = y(1)(u1) ⊗ ... ⊗ y(n)(un) ⊗ y(0)(p)
1346
+ (6.8)
1347
+ for n ≥ 0 gives a morphism of cocyclic modules. In particular, we have induced morphisms
1348
+
1349
+
1350
+ hoc(y) : HH•(U; P) −→ HH•(U′; P′)
1351
+
1352
+
1353
+ cy(y) : HC•(U; P) −→ HC•(U′; P′)
1354
+ (6.9)
1355
+ on Hochschild and cyclic cohomologies for each y ∈ D.
1356
+ Proof. It is clear that the morphisms in (6.8) are well-defined. For y ∈ D and i = n + 1 in (6.7), we note that
1357
+ y(δn+1(u1 ⊗ · · · ⊗ un ⊗ p))
1358
+ = y(1)(u1) ⊗ . . . y(n)(un) ⊗ y(n+1)(p(−1)) ⊗ y(0)(p(0))
1359
+ = y(2)(u1) ⊗ . . . y(n+1)(un) ⊗ y(1)(p(−1)) ⊗ y(0)(p(0))
1360
+ (since C is cocommutative)
1361
+ = y(1)(u1) ⊗ . . . y(n)(un) ⊗ (y(0)(p))(−1) ⊗ y(0)(p)(0)
1362
+ (using (5.24))
1363
+ (6.10)
1364
+ Similarly, we may verify that the morphisms in (6.8) commute with the face and degeneracy maps appearing in (6.7). To show
1365
+ that they also commute with the cyclic operators appearing in (6.7), we note that for u1 ⊗ ... ⊗ un ⊗ p ∈ Cn(U; P) and y ∈ D, we
1366
+ have
1367
+ y(τn(u1 ⊗ ... ⊗ un ⊗ p)) = y(u1
1368
+ −(1)u2 ⊗A · · · ⊗A u1
1369
+ −(n−1)un ⊗A u1
1370
+ −(n)p(−1) ⊗A p(0)u1
1371
+ +)
1372
+ = y(1)(u1
1373
+ −(1))y(2)(u2) ⊗A · · · ⊗A y(2n−3)(u1
1374
+ −(n−1))y(2n−2)(un) ⊗A y(2n−1)(u1
1375
+ −(n))y(2n)(p(−1)) ⊗A y(0)(p(0)u1
1376
+ +)
1377
+ = y(1)(u1
1378
+ −(1))y(n+1)(u2) ⊗A · · · ⊗A y(n−1)(u1
1379
+ −(n−1))y(2n−1)(un) ⊗A y(n)(u1
1380
+ −(n))y(2n)(p(−1)) ⊗A y(0)(p(0)u1
1381
+ +)
1382
+ = y(1)(u1
1383
+ −)(1)y(2)(u2) ⊗A · · · ⊗A y(1)(u1
1384
+ −)(n−1)y(n)(un) ⊗A y(1)(u1
1385
+ −)(n)y(n+1)(p(−1)) ⊗A y(0)(p(0)u1
1386
+ +)
1387
+ = y(2)(u1
1388
+ −)(1)y(3)(u2) ⊗A · · · ⊗A y(2)(u1
1389
+ −)(n−1)y(n+1)(un) ⊗A y(2)(u1
1390
+ −)(n)y(n+2)(p(−1)) ⊗A y(0)(p(0))y(1)(u1
1391
+ +)
1392
+ = y(1)(u1)−(1)y(2)(u2) ⊗A · · · ⊗A y(1)(u1)−(n−1)y(n)(un) ⊗A y(1)(u1)−(n)y(n+1)(p(−1)) ⊗A y(0)(p(0))y(1)(u1)+
1393
+ (using (6.3))
1394
+ = y(1)(u1)−(1)y(2)(u2) ⊗A · · · ⊗A y(1)(u1)−(n−1)y(n)(un) ⊗A y(1)(u1)−(n)y(0)(p)(−1) ⊗A y(0)(p)(0)y(1)(u1)+
1395
+ (using (5.24))
1396
+ This proves the result.
1397
+
1398
+ 18
1399
+
1400
+ Finally, we recall from [14, § 4.3] that there are Hopf-Galois isomorphisms relating the modules C•(U; P) and C•(U; P)
1401
+ ξn(U; P) : Cn(U; P)
1402
+
1403
+ −→ Cn(U; P)
1404
+ p ⊗ u1 ⊗ · · · ⊗ un �→ u1
1405
+ (1) ⊗ u1
1406
+ (2)u2
1407
+ (1) ⊗ · · · ⊗ u1
1408
+ (n)u2
1409
+ (n−1) . . .un−1
1410
+ (2) un ⊗ p
1411
+ (6.11)
1412
+ We will conclude this section by showing that the morphisms induced by comodule measurings of SAYD modules are compat-
1413
+ ible with the Hopf-Galois isomorphisms in (6.11).
1414
+ Theorem 6.4. Let U = (U, AL, sL, tL, ∆L, ǫL, S ), and U′ = (U′, A′
1415
+ L, s′
1416
+ L, t′
1417
+ L, ∆′
1418
+ L, ǫ′
1419
+ L, S ′) be Hopf algebroids over k. Let P and P′
1420
+ be SAYD modules over U and U′ respectively. Let (Ψ, ψ) : C −→ V(U, U′) be a cocommutative measuring and let Ω : D −→
1421
+ Vectk(P, P′) be a (C, Ψ, ψ)-measuring comodule from P to P′. Then, for each y ∈ D, the following diagram commutes
1422
+ Cn(U; P)
1423
+ ξn(U;P)
1424
+ −−−−−−→ Cn(U; P)
1425
+ Ωn(y)
1426
+ �
1427
+ �Ω
1428
+ n(y)
1429
+ Cn(U; P)
1430
+ ξn(U;P)
1431
+ −−−−−−→ Cn(U; P)
1432
+ (6.12)
1433
+ Proof. We set N := n(n − 1)/2. For y ∈ D and p ⊗ u1 ⊗ · · · ⊗ un ∈ Cn(U; P), we see that
1434
+
1435
+ n(y)(ξn(U; P)(p ⊗ u1 ⊗ · · · ⊗ un))
1436
+ = Ω
1437
+ n(y)(u1
1438
+ (1) ⊗ u1
1439
+ (2)u2
1440
+ (1) ⊗ · · · ⊗ u1
1441
+ (n)u2
1442
+ (n−1) . . . un−1
1443
+ (2) un ⊗ p)
1444
+ = y(1)(u1
1445
+ (1)) ⊗ y(2)(u1
1446
+ (2))y(3)(u2
1447
+ (1)) ⊗ · · · ⊗ y(N+1)(u1
1448
+ (n))y(N+2)(u2
1449
+ (n−1)) . . . y(N+n−1)(un−1
1450
+ (2) )y(N+n)(un) ⊗ y(0)(p)
1451
+ = y(1)(u1
1452
+ (1)) ⊗ y(2)(u1
1453
+ (2))y(n+1)(u2
1454
+ (1)) ⊗ · · · ⊗ y(n)(u1
1455
+ (n))y(2n−1)(u2
1456
+ (n−1)) . . .y(N+n−1)(un−1
1457
+ (2) )y(N+n)(un) ⊗ y(0)(p)
1458
+ = y(1)(u1)(1) ⊗ y(1)(u1)(2)y(2)(u2)(1) ⊗ · · · ⊗ y(1)(u1)(n)y(2)(u2)(n−1) . . .y(n−1)(un−1)(2)y(n)(un) ⊗ y(0)(p)
1459
+ = ξn(U; P)(Ωn(y)(p ⊗ u1 ⊗ · · · ⊗ un))
1460
+ (6.13)
1461
+
1462
+ 7
1463
+ Operads with multiplication, comp modules and morphisms on cyclic homology
1464
+ We start the final section by recalling from Kowalzig [16] the following two notions.
1465
+ Definition 7.1. (see [16, Definition 2.2]) A non-Σ operad O over k consists of the following:
1466
+ (a) A collection of vector spaces O = {O(n)}n≥0.
1467
+ (b) A family of k-linear operations ◦i : O(p)⊗O(q) −→ O(p+q−1) and an identity 1 ∈ O(1) satisfying the following conditions
1468
+ (for φ ∈ O(p), ψ ∈ O(q), χ ∈ O(r))
1469
+ φ ◦i ψ
1470
+ = 0
1471
+ if p < i or p = 0
1472
+ (φ ◦i ψ) ◦ j χ
1473
+ =
1474
+ 
1475
+ (φ ◦ j χ) ◦i+r−1 ψ
1476
+ if j < i
1477
+ φ ◦i (ψ ◦ j−i+1 χ)
1478
+ if i ≤ j < q + i
1479
+ (φ ◦ j−q+1 χ) ◦i ψ
1480
+ if j ≥ q + i
1481
+ φ ◦i 1
1482
+ = 1 ◦1 φ = φ
1483
+ for i ≤ p
1484
+ (c) An operad multiplication µ ∈ O(2) and a unit e ∈ O(0) such that
1485
+ µ ◦1 µ = µ ◦2 µ
1486
+ µ ◦1 e = µ ◦2 e = 1
1487
+ (7.1)
1488
+ Definition 7.2. (see [16, Definition 3.1]) A cyclic unital comp module M over an operad O with multiplication consists of the
1489
+ following data:
1490
+ (a) A collection of vector spaces M = {M(n)}n≥0.
1491
+ 19
1492
+
1493
+ (b) A family of k-bilinear operations •i : O(p) ⊗ M(n) −→ M(n − p + 1), 0 ≤ i ≤ n + 1 − p satisfying the following conditions
1494
+ for φ ∈ O(p), ψ ∈ O(q), x ∈ M(n)
1495
+ φ •i (ψ • j x) =
1496
+ 
1497
+ ψ • j (φ •i+q−1 x)
1498
+ j < i
1499
+ (φ • j−i+1 ψ) •i x
1500
+ if j − p < i ≤ j
1501
+ ψ • j−p+1 (φ •i x)
1502
+ if 1 ≤ i ≤ j − p
1503
+ as well as 1 •i x = x for i = 1, 2, ..., n.
1504
+ (c) A cyclic operator t : M(n) −→ M(n) for n ≥ 1 satisfying
1505
+ t(φ •i x) = φ •i t(x)
1506
+ (7.2)
1507
+ for φ ∈ O(p), x ∈ M(n) and 0 ≤ i ≤ n − p as well as tn+1 = id.
1508
+ We take pairs (O, M) consisting of a non-linear Σ operad O and a cyclic unital comp module M over O. We now consider
1509
+ comodule measurings between such pairs
1510
+ Definition 7.3. A comodule measuring from (O, M) to (O′, M′) consists of the following:
1511
+ (a) A cocommutative coalgebra C and a family of morphisms {Φn : C −→ Vectk(O(n), O′(n))}n≥0 satisfying
1512
+ Φp+q−1(x)(φ ◦i ψ) = Φp(x(1))(φ) ◦′
1513
+ i Φq(x(2))(φ)
1514
+ Φ2(x)(µ) = ǫ(x)µ′
1515
+ Φ0(x)(e) = ǫ(x)e′
1516
+ (7.3)
1517
+ for φ ∈ O(p), ψ ∈ O(q) and any x ∈ C.
1518
+ (b) A comodule D over C and a family of morphisms {Ψn : D −→ Vectk(M(n), M′(n))}n≥0 satisfying
1519
+ Ψn−p+1(φ •i x) = Ψp(y(0))(φ) •i Ψn(y(1))(x)
1520
+ (7.4)
1521
+ for y ∈ D, φ ∈ O(p), x ∈ M(n), 0 ≤ i ≤ n + 1 − p and also
1522
+ Ψn(y)(t(x)) = t′(Ψn(y)(x))
1523
+ (7.5)
1524
+ for y ∈ D, x ∈ M(n), where t and t′ are respectively the cyclic operators on M and M′.
1525
+ We now recall from [16, Proposition 3.5] that the cyclic homology of (O, M) is obtained from the cyclic module C•(O, M) :=
1526
+ M(•) whose cyclic operators are t : M(n) −→ M(n) and whose face maps and degeneracies are given as follows:
1527
+ di(x) := µ •i x, (0 ≤ i < n)
1528
+ dn(x) := µ •0 t(x)
1529
+ sj(x) := e • j+1 x, 0 ≤ j ≤ n
1530
+ (7.6)
1531
+ The cyclic homologies of this cyclic module will be denoted by HC•(O, M). We conclude with the following result.
1532
+ Proposition 7.4. If D is a C-measuring comodule from (O, M) to (O′, M′), then each y ∈ D induces a morphism Ψcy
1533
+ • (y) :
1534
+ HC•(O, M) −→ HC•(O′, M′) on Hochschild homologies.
1535
+ Proof. We know from (7.5) that the action of any y ∈ D commutes with the cyclic operators. From the definitions in (7.6)
1536
+ and the conditions in (7.3), it is clear that the action also commutes with the degeneracies and face maps. The result is now
1537
+ clear.
1538
+
1539
+ References
1540
+ [1] M. Anel and A. Joyal, Sweedler theory for (co)algebras and the bar-cobar constructions, arXiv 1309.6952 (2013).
1541
+ [2] A. Banerjee and S. Kour, On measurings of algebras over operads and homology theories, Algebr. Geom. Topol. 22 (2022), no. 3, 1113–1158.
1542
+ [3] M. Batchelor, Difference operators, measuring coalgebras, and quantum group-like objects, Adv. Math. 105 (1994), no. 2, 190–218.
1543
+ [4]
1544
+ , Measuring comodules—their applications, J. Geom. Phys. 36 (2000), no. 3-4, 251–269.
1545
+ 20
1546
+
1547
+ [5] G. B¨ohm and K. Szlach´anyi, Hopf algebroids with bijective antipodes: axioms, integrals, and duals, J. Algebra 274 (2004), no. 2, 708–750.
1548
+ [6] G. B¨ohm, Galois theory for Hopf algebroids, Ann. Univ. Ferrara Sez. VII (N.S.) 51 (2005), 233–262.
1549
+ [7] G. B¨ohm, T. Brzezi´nski, and R. Wisbauer, Monads and comonads on module categories, J. Algebra 322 (2009), no. 5, 1719–1747.
1550
+ [8] T. Brzezinski and R. Wisbauer, Corings and comodules, London Mathematical Society Lecture Note Series, vol. 309, Cambridge University Press,
1551
+ Cambridge, 2003.
1552
+ [9] L. Grunenfelder and M. Mastnak, On bimeasurings, J. Pure Appl. Algebra 204 (2006), no. 2, 258–269.
1553
+ [10]
1554
+ , On bimeasurings. II, J. Pure Appl. Algebra 209 (2007), no. 3, 823–832.
1555
+ [11] M. Hyland, I. L´opez Franco, and C. Vasilakopoulou, Hopf measuring comonoids and enrichment, Proc. Lond. Math. Soc. (3) 115 (2017), no. 5, 1118–
1556
+ 1148.
1557
+ [12]
1558
+ , Measuring comodules and enrichment, arXiv 1703.10137 (2017).
1559
+ [13] N. Kowalzig and H. Posthuma, The cyclic theory of Hopf algebroids, J. Noncommut. Geom. 5 (2011), no. 3, 423–476.
1560
+ [14] N. Kowalzig and U. Kr¨ahmer, Cyclic structures in algebraic (co)homology theories, Homology Homotopy Appl. 13 (2011), no. 1, 297–318.
1561
+ [15] N. Kowalzig, Batalin-Vilkovisky algebra structures on (Co)Tor and Poisson bialgebroids, J. Pure Appl. Algebra 219 (2015), no. 9, 3781–3822.
1562
+ [16]
1563
+ , Gerstenhaber and Batalin-Vilkovisky structures on modules over operads, Int. Math. Res. Not. IMRN 22 (2015), 11694–11744.
1564
+ [17] J.-L Loday, Cyclic homology, 2nd ed., Grundlehren der mathematischen Wissenschaften, vol. 301, Springer-Verlag, Berlin, 1998. Appendix E by M. O.
1565
+ Ronco; Chapter 13 by the author in collaboration with T. Pirashvili.
1566
+ [18] P. Schauenburg, Bialgebras over noncommutative rings and a structure theorem for Hopf bimodules, Appl. Categ. Structures 6 (1998), no. 2, 193–222.
1567
+ [19]
1568
+ , Duals and doubles of quantum groupoids (×R-Hopf algebras), New trends in Hopf algebra theory (La Falda, 1999), Contemp. Math., vol. 267,
1569
+ Amer. Math. Soc., Providence, RI, 2000, pp. 273–299.
1570
+ [20] M. E. Sweedler, Hopf algebras, Mathematics Lecture Note Series, W. A. Benjamin, Inc., New York, 1969.
1571
+ [21] M. Takeuchi, Groups of algebras over A ⊗ A, J. Math. Soc. Japan 29 (1977), no. 3, 459–492.
1572
+ [22] C. Vasilakopoulou, Enrichment of categories of algebras and modules, arXiv 1205.6450 (2012).
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+ [23]
1574
+ , On enriched fibrations, Cah. Topol. G´eom. Diff´er. Cat´eg. 59 (2018), no. 4, 354–387.
1575
+ [24]
1576
+ , Enriched duality in double categories: V-categories and V-cocategories, J. Pure Appl. Algebra 223 (2019), no. 7, 2889–2947.
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+ 21
1578
+
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1
+ Constraining the Limitations of NEATM-like Models: A Case Study with Near-Earth
2
+ Asteroid (285263) 1998 QE2
3
+ Samuel A. Myers1
4
+ , Ellen S. Howell1
5
+ , Christopher Magri2
6
+ , Ronald J. Vervack, Jr.3
7
+ , Yanga R. Fernández4
8
+ ,
9
+ Sean E. Marshall5
10
+ , and Patrick A. Taylor6
11
+ 1 Lunar and Planetary Laboratory, University of Arizona, 1629 E. University Boulevard, Tucson, AZ 85721, USA; [email protected]
12
+ 2 University of Maine Farmington, 173 High Street, Farmington, ME 04938, USA
13
+ 3 Johns Hopkins Applied Physics Laboratory, 11100 John Hopkins Road, Laurel, MD 20723, USA
14
+ 4 University of Central Florida, 4111 Libra Drive, Orlando, FL 32816, USA
15
+ 5 Arecibo Observatory/University of Central Florida, HC-03 Box 53995, Arecibo, Puerto Rico 00612, USA
16
+ 6 National Radio Astronomy Observatory/Green Bank Observatory, 1180 Boxwood Estate Road, Charlottesville, VA 22903, USA
17
+ Received 2022 August 10; revised 2022 November 28; accepted 2022 December 1; published 2023 January 10
18
+ Abstract
19
+ Near-Earth asteroids (NEAs) are a key test bed for investigations into planet formation, asteroid dynamics, and
20
+ planetary defense initiatives. These studies rely on understanding NEA sizes, albedo distributions, and regolith
21
+ properties. Simple thermal models are a commonly used method for determining these properties; however, they
22
+ have inherent limitations owing to the simplifying assumptions they make about asteroid shapes and properties.
23
+ With the recent collapse of the Arecibo Telescope and a decrease of direct size measurements, as well as future
24
+ facilities such as LSST and NEO Surveyor coming online soon, these models will play an increasingly important
25
+ role in our knowledge of the NEA population. Therefore, it is key to understand the limits of these models. In this
26
+ work we constrain the limitations of simple thermal models by comparing model results to more complex
27
+ thermophysical models, radar data, and other existing analyses. Furthermore, we present a method for placing
28
+ tighter constraints on inferred NEA properties using simple thermal models. These comparisons and constraints are
29
+ explored using the NEA (285263) 1998 QE2 as a case study. We analyze QE2 with a simple thermal model and
30
+ data from both the NASA IRTF SpeX instrument and NEOWISE mission. We determine an albedo between 0.05
31
+ and 0.10 and thermal inertia between 0 and 425J m−2 s−1/2 K−1. We find that overall the simple thermal model is
32
+ able to well constrain the properties of QE2; however, we find that model uncertainties can be influenced by
33
+ topography, viewing geometry, and the wavelength range of data used.
34
+ Unified Astronomy Thesaurus concepts: Asteroids (72); Asteroid surfaces (2209); Near-Earth objects (1092)
35
+ 1. Introduction
36
+ Asteroids were once derided by astronomers as the “vermin
37
+ of the sky,” but they now form an important piece of our efforts
38
+ to understand our own solar system. Understanding their sizes,
39
+ albedo
40
+ distributions,
41
+ and
42
+ regolith
43
+ properties
44
+ is
45
+ key
46
+ for
47
+ investigations into many aspects of solar system science,
48
+ including solar system formation, main belt asteroid orbital
49
+ evolution, surface processes on airless bodies, and under-
50
+ standing our meteorite collection. Near-Earth asteroids (NEAs),
51
+ in particular, are excellent targets for these efforts owing to
52
+ their proximity to Earth.
53
+ In addition to understanding the albedos and regoliths of
54
+ these objects, accurately measuring the sizes of NEAs is pivotal
55
+ for planetary defense initiatives—the area of study focused on
56
+ preventing catastrophic asteroid impacts with Earth. This is
57
+ because the size of an object is directly related to the energy of
58
+ impact (Morrison & Teller 1995), which determines the impact
59
+ severity. Thus, observation and modeling techniques that
60
+ provide estimates of these properties are key for understanding
61
+ the NEA population.
62
+ There are a few methods for obtaining size estimates and
63
+ other physical properties from NEA observations. Radar
64
+ images, detailed thermophysical models, and simple thermal
65
+ models can all be used to obtain size estimates. All of these
66
+ methods, along with light-curve measurements, can also place
67
+ constraints on other physical properties of asteroids. Other
68
+ methods, such as direct imaging (Dollfus 1971; Marchis et al.
69
+ 2006; Marchis & Vega 2014), stellar occultations (Millis &
70
+ Dunham 1989; Arai et al. 2020), and spacecraft encounters
71
+ exist (Belton et al. 1992, 1996; Veverka et al. 2000; Lauretta
72
+ et al. 2019) but are only applicable in rare cases. Of the more
73
+ common methods, radar images can provide a size estimate
74
+ without other information (Ostro 1985). Radar observations
75
+ can also be used to construct detailed models of the asteroid’s
76
+ shape (Hudson & Ostro 1994; Magri et al. 2007, 2011; Nolan
77
+ et al. 2013). Light-curve measurements can also produce shape
78
+ models, although they are often less detailed than radar-derived
79
+ shape models and do not include an absolute size scale (Ďurech
80
+ et al. 2012 and references therein). These shape models can be
81
+ coupled with thermal spectra to constrain other physical
82
+ properties of the asteroid as well, such as thermal inertia or
83
+ surface roughness (Marshall et al. 2017; Howell et al. 2018;
84
+ Jones 2018; Hinkle et al. 2022).
85
+ Historically, the Arecibo Telescope has been a source of
86
+ numerous NEA radar observations. The Arecibo Telescope
87
+ detected over 900 NEAs and made size estimates of roughly
88
+ 400 of those (Howell et al. 2020). However, with the recent
89
+ loss of the Arecibo Telescope, there will be a lack of direct size
90
+ and shape measurements of NEAs. (Although Goldstone is able
91
+ to make radar measurements, it has a lower sensitivity and less
92
+ availability for targets of opportunity.) As a result, in the future
93
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
94
+ https://doi.org/10.3847/PSJ/aca89d
95
+ © 2023. The Author(s). Published by the American Astronomical Society.
96
+ Original content from this work may be used under the terms
97
+ of the Creative Commons Attribution 4.0 licence. Any further
98
+ distribution of this work must maintain attribution to the author(s) and the title
99
+ of the work, journal citation and DOI.
100
+ 1
101
+
102
+ there will be a greater reliance on other methods to understand
103
+ the
104
+ physical
105
+ properties
106
+ of
107
+ NEAs.
108
+ These
109
+ methods
110
+ will
111
+ necessarily be models, like simple thermal models, that assume
112
+ asteroid shapes or use less well-constrained shape models.
113
+ Simple thermal models, such as the Standard Thermal Model
114
+ (Lebofsky et al. 1986; Lebofsky & Spencer 1989) and the
115
+ Near-Earth
116
+ Asteroid
117
+ Thermophysical
118
+ Model
119
+ (NEATM;
120
+ Harris 1998), are a convenient method for obtaining NEA
121
+ sizes and physical properties in part because they are easy to
122
+ run. They require only visible and thermal infrared data and are
123
+ computationally
124
+ fast.
125
+ For
126
+ this
127
+ reason,
128
+ they
129
+ are
130
+ already
131
+ commonly used to analyze data collected by large survey
132
+ missions like NEOWISE (Mainzer et al. 2011b) and Explor-
133
+ eNEOs (Trilling et al. 2010). Due to the large volume of data
134
+ collected by these types of surveys and the sparse amount of
135
+ data collected on any single object, simple thermal models are
136
+ often the only practical way to quickly interpret the data. In
137
+ these cases, simple thermal models are used to identify both
138
+ scientifically interesting and potentially dangerous NEAs (e.g.,
139
+ Trilling et al. 2010).
140
+ However, simple thermal models make simplifying assump-
141
+ tions about the asteroid’s shape and surface that can result in
142
+ inaccuracies and thus poor constraints of inferred NEA
143
+ properties. This is especially relevant for determinations of
144
+ asteroid sizes—values that are pivotal for planetary defense
145
+ activities. Simple thermal models can only make direct
146
+ determinations of asteroid sizes in specific cases. If absolute
147
+ photometry in both the visible and infrared is available, size
148
+ can be solved for directly. However, these estimates require
149
+ assuming that the visible and infrared data were acquired at
150
+ similar viewing geometries. This assumption is often made
151
+ with models employing NEOWISE or ExploreNEOs observa-
152
+ tions. Alternatively, if only normalized flux is available, then
153
+ the size must be estimated from the modeled albedo in
154
+ combination with the absolute magnitude, H. In this case, the
155
+ estimates are subject to uncertainties in the magnitude (Bowell
156
+ et al. 1989; Jurić et al. 2002; Vereš et al. 2015), as well as
157
+ typically large error bars in the inferred albedo, producing poor
158
+ constraints. In fact, recent work has shown that there are
159
+ inconsistencies between sizes derived from NEOWISE data
160
+ using these models and sizes derived using other methods
161
+ (Howell et al. 2012; Taylor et al. 2014; Masiero et al. 2019;
162
+ Taylor et al. 2019; Masiero et al. 2021).
163
+ In this paper, we seek to better understand the limitations of
164
+ simple thermal models, such as NEATM, by comparing simple
165
+ thermal model results to more complex thermophysical models,
166
+ radar data, and other existing analyses of a given object. We
167
+ also present a method for placing tighter constraints on inferred
168
+ NEA properties using these simple thermal models. We use a
169
+ simple, NEATM-like model (Section 3) to model the observed
170
+ NEA, and the consistency of the best-fit parameters is then
171
+ checked by comparing the models to normalized flux data
172
+ collected across multiple nights that represent a range of
173
+ viewing geometries. We also compare the models to the
174
+ absolute photometry collected by the NEOWISE spacecraft. By
175
+ observing an object across multiple viewing geometries and
176
+ combining normalized flux spectra with absolute photometry,
177
+ we are able to place tight bounds on modeled NEA properties.
178
+ These simple thermal model results are then compared to
179
+ model results from SHERMAN (Magri et al. 2018), a complex
180
+ thermophysical
181
+ model;
182
+ radar
183
+ measurements;
184
+ and
185
+ other
186
+ observations
187
+ and
188
+ analyses
189
+ of
190
+ the
191
+ given
192
+ object.
193
+ These
194
+ comparisons allow us to place constraints on the overall
195
+ limitations of the simple thermal model and identify key factors
196
+ that influence uncertainties in simple thermal model results.
197
+ This analysis is performed on the well-studied NEA
198
+ (285263) 1998 QE2 (hereafter referred to as QE2). QE2 is a
199
+ spheroidal, binary NEA system, with an existing radar-derived
200
+ shape model (Springmann et al. 2014). The secondary has a
201
+ diameter ∼25% that of the primary (Springmann et al. 2014)
202
+ and thus contributes only 6% of the total flux. Therefore, the
203
+ primary object dominates the thermal emission from the
204
+ system, and we neglect the secondary in our analysis. QE2 is
205
+ an Xk-type asteroid in the Bus−DeMeo taxonomy, as derived
206
+ from our SpeX prism spectra and a visible spectrum obtained
207
+ by Hicks et al. (2013).
208
+ As part of our investigation into the limitations of the
209
+ NEATM-like model, we find a discrepancy in the currently
210
+ accepted H-magnitude for QE2. We find that the current value
211
+ is inconsistent with the size derived from the radar measure-
212
+ ments of QE2. We investigate this discrepancy and discuss
213
+ implications. As part of this investigation, we compare our
214
+ results to previous studies to understand QE2ʼs composition
215
+ and surface properties (Fieber-Beyer et al. 2020), as well as its
216
+ spin state (Moskovitz et al. 2017). These comparisons allow us
217
+ to further benchmark the uncertainties in the results of our
218
+ method for placing tight constraints on NEA properties derived
219
+ with simple thermal models.
220
+ In Section 2 we discuss the data used for our analysis. In
221
+ Section 3 we describe our simple, NEATM-like model, and in
222
+ Section 4 we present the results for QE2 from this model. In
223
+ Section 5 we describe our analysis of the uncertainties in these
224
+ model results. We compare our simple, NEATM-like model
225
+ results to model results from SHERMAN, radar data of QE2,
226
+ and the results of other previous studies. We then discuss
227
+ implications for the limitations of simple thermal models. We
228
+ conclude with a summary of our results in Section 6.
229
+ 2. Spectral and Radar Data
230
+ 2.1. IRTF Observations
231
+ The primary data used to constrain our models are normalized
232
+ flux spectra obtained with the SpeX instrument at the NASA
233
+ IRTF (Rayner et al. 2003). We use normalized flux, as it has
234
+ smaller uncertainties relative to absolute photometry. These
235
+ observations are carried out as part of our ongoing investigation
236
+ into the physical properties of NEAs. We observed using both
237
+ prism mode (0.8–2.5 μm) and Long-Wavelength Cross-Dispersed
238
+ (LDX)1.9 mode (2.2–4.1 μm). Note that the observations of QE2
239
+ presented here were done before the upgrade to SpeX that
240
+ expanded the wavelength ranges of all settings.
241
+ For QE2, observations were carried out over six nights, from
242
+ 2013 May 30 to 2013 July 10. Over this time, the solar phase
243
+ angle of QE2 varied from 18°.0 to 39°.7, which let us observe
244
+ different viewing geometries and illumination states. As a
245
+ result, we see the thermal emission at different local times of
246
+ day. This is important because it allows us to check the
247
+ consistency of the fit parameters (Section 3). The various sub-
248
+ Earth locations of QE2 that we observed are shown in Figure 1.
249
+ A summary of the observational parameters for our six nights
250
+ of SpeX data is shown in Table 1.
251
+ 2
252
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
253
+ Myers et al.
254
+
255
+ All SpeX observations were done in pairs, nodding the
256
+ telescope along a 15″ slit. We used exposure times of 15 s for
257
+ our LXD data and 10–30 s for our prism data. The data were
258
+ processed using the Spextool software package (Cushing et al.
259
+ 2004), and the spectra were extracted from summed images. In
260
+ addition to the object, we observed solar-analog stars in a
261
+ similar manner. At least one was a nearby G star within ∼5° of
262
+ the object on the sky. All stars were compared to a well-
263
+ characterized solar analog star on each night, and their spectra
264
+ were corrected for slight spectral slope variations if necessary.
265
+ Each asteroid–star pair was combined in a ratio after correcting
266
+ each for atmospheric absorption lines. The spectra were then
267
+ determined using a weighted average over all asteroid–star
268
+ pairs and binned to form the final spectra. Bad data points were
269
+ flagged and excluded from the fitting and averaging process.
270
+ The detailed methods for this entire process are given in
271
+ Howell et al. (2018).
272
+ The data are broken up across each night into several
273
+ independent sets of roughly 20–30 minutes each to sample
274
+ different areas of the surface. QE2 has a rotation period of
275
+ 4.749 ± 0.002 hr (Springmann et al. 2014), meaning that each
276
+ spectrum is separated by roughly 25°–40° of longitude at the
277
+ equator. The sub-Earth latitudes and longitudes at the midtimes of
278
+ the observations are shown in Figure 1. These sub-Earth
279
+ coordinates are calculated using the shape model of Springmann
280
+ et al. (2014). The LXD data for each of the six nights are shown in
281
+ Figure 2. Each spectrum is normalized at 1.6 μm to give
282
+ normalized flux. (Note that there is no significant thermal
283
+ Figure 1. Sub-Earth locations on QE2 during observations as determined by a radar shape model (Springmann et al. 2014). (a) The pole solution with the “bumpy”
284
+ topography in the northern hemisphere. (b) The pole solution with the topography partially in the southern hemisphere (Section 2.3). The range of sub-Earth locations
285
+ observed indicates that QE2 was observed across multiple different viewing geometries. This range of observations is key for constraining QE2ʼs parameters using our
286
+ NEATM-like model.
287
+ 3
288
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
289
+ Myers et al.
290
+
291
+ Sub-EarthLocations
292
+ 17
293
+ A)
294
+ 16
295
+ Latitude (degree)
296
+ Date
297
+ 15
298
+ 30May
299
+ 02 Jun
300
+ 4
301
+ 08 Jun
302
+
303
+ 15Jun
304
+
305
+ 18Jun
306
+ 13
307
+
308
+ 10Jul
309
+ 12
310
+ 11
311
+ B)
312
+
313
+ atitude(degree)
314
+ 5
315
+ Date
316
+ 30May
317
+ 02 Jun
318
+
319
+ 08 Jun
320
+ 15Jun
321
+ 18Jun
322
+ -10
323
+
324
+ 10Jul
325
+ -15
326
+ 0
327
+ 60
328
+ 120
329
+ 180
330
+ 240
331
+ 300
332
+ 360
333
+ Longitude(degree)contamination at this wavelength.) We use normalized flux
334
+ because the relative uncertainties are much smaller than for
335
+ absolutely calibrated photometry. We cover the range from
336
+ completely reflected to thermally dominated to ensure that our
337
+ simple thermal model is well constrained in both regimes. This
338
+ technique has the advantage of being more flexible but the
339
+ disadvantage that the data are highly correlated in wavelength.
340
+ 2.2. NEOWISE Observations
341
+ In addition to our SpeX data, we fit our simple thermal
342
+ model to data collected by NEOWISE. Unlike the SpeX data,
343
+ which measure normalized flux, NEOWISE measures absolute
344
+ photometry. Thus, fitting our simple thermal model to the
345
+ NEOWISE data allows us to check that the best-fit parameters
346
+ are consistent with both the spectrum shape and calibrated flux
347
+ values. This provides an additional independent check on the
348
+ consistency of the simple thermal model and allows us to
349
+ identify any potential issues with the model not observed when
350
+ fitting normalized flux data alone.
351
+ We retrieve the NEOWISE data and associated uncertainties
352
+ from the NASA/IPAC Infrared Science Archive (Mainzer
353
+ et al. 2011a, 2014).7 We do not use the raw images, but instead
354
+ retrieve processed data that list the magnitudes and uncertain-
355
+ ties for channels W1 (effective wavelength 3.4 μm) and W2
356
+ (effective wavelength 4.6 μm) for each time the object was
357
+ observed. We remove data points that are flagged for potential
358
+ contamination, such as by cosmic-ray hits, and average
359
+ together all remaining observations. The uncertainty in the
360
+ NEOWISE data is dominated by systematic errors and not
361
+ statistical noise. All observations, except one, have similar
362
+ uncertainties. We thus take a weighted average of the
363
+ observations and adopt the variance of the overall data set,
364
+ divided by the square root of the number of observations minus
365
+ one, as our 1σ uncertainties. For QE2, all observations were
366
+ taken over a short time interval such that the change in QE2ʼs
367
+ orbital position was minimal. Therefore, we averaged together
368
+ all available observations, resulting in one averaged set of data
369
+ points from eight individual observations that span roughly 29
370
+ hr and approximately six rotation periods. The individual
371
+ observations are evenly distributed across the rotation phase. A
372
+ summary of the observational parameters for the averaged
373
+ observation is given in Table 1. A list of the individual
374
+ observations is given in Table 2.
375
+ After retrieval, the data are then converted from NEOWISE
376
+ magnitudes to Fλ units following the procedures outlined in the
377
+ WISE Data Processing Handbook (Wright et al. 2010; Cutri
378
+ et al. 2012). For this process we apply a final blackbody color
379
+ correction corresponding to a 221 K object. This blackbody
380
+ temperature is determined by fitting ideal blackbody curves to
381
+ the NEOWISE data in an iterative process until the corrected
382
+ NEOWISE data and ideal blackbody curves converge. The
383
+ blackbody temperature used for the initial correction is
384
+ calculated using the theoretical blackbody temperature relation
385
+ T
386
+ L
387
+ A
388
+ r
389
+ 1
390
+ 16
391
+ ,
392
+ 1
393
+ H
394
+ sb
395
+ 4
396
+ 2
397
+ (
398
+ )
399
+ ( )
400
+
401
+ s
402
+ p
403
+ =
404
+ -
405
+ where Le is the solar luminosity, A is the Bond albedo, rH is the
406
+ object–Sun distance, and σsb is the Stefan–Boltzmann constant.
407
+ Table 1
408
+ Summary of Observations, Including Values Input Directly into the NEATM-like Model
409
+ Date
410
+ Set
411
+ Midtime
412
+ rH (au)
413
+ Δ (au)
414
+ α (deg)
415
+ Instrument
416
+ 2013 May 30
417
+ A
418
+ 06:46:50
419
+ 1.046 8
420
+ 0.040 3
421
+ 34.3
422
+ SpeX
423
+ 2013 May 30
424
+ B
425
+ 07:22:08
426
+ 1.046 8
427
+ 0.040 3
428
+ 34.2
429
+ SpeX
430
+ 2013 May 30
431
+ C
432
+ 08:36:57
433
+ 1.049 8
434
+ 0.040 2
435
+ 33.9
436
+ SpeX
437
+ 2013 Jun 02
438
+ A
439
+ 06:51:57
440
+ 1.052 2
441
+ 0.040 1
442
+ 18.3
443
+ SpeX
444
+ 2013 Jun 02
445
+ B
446
+ 07:08:19
447
+ 1.052 2
448
+ 0.040 1
449
+ 18.3
450
+ SpeX
451
+ 2013 Jun 02
452
+ C
453
+ 07:17:50
454
+ 1.052 2
455
+ 0.040 1
456
+ 18.3
457
+ SpeX
458
+ 2013 Jun 02
459
+ D
460
+ 07:34:17
461
+ 1.052 2
462
+ 0.040 1
463
+ 18.2
464
+ SpeX
465
+ 2013 Jun 08
466
+ A
467
+ 08:12:16
468
+ 1.067 1
469
+ 0.060 5
470
+ 30.0
471
+ SpeX
472
+ 2013 Jun 08
473
+ B
474
+ 09:25:01
475
+ 1.067 2
476
+ 0.060 8
477
+ 30.1
478
+ SpeX
479
+ 2013 Jun 08
480
+ C
481
+ 09:37:14
482
+ 1.067 2
483
+ 0.060 8
484
+ 30.1
485
+ SpeX
486
+ 2013 Jun 08
487
+ D
488
+ 10:38:10
489
+ 1.067 4
490
+ 0.061 0
491
+ 30.2
492
+ SpeX
493
+ 2013 Jun 08
494
+ E
495
+ 10:50:40
496
+ 1.067 4
497
+ 0.061 1
498
+ 30.2
499
+ SpeX
500
+ 2013 Jun 15
501
+ A
502
+ 11:06:28
503
+ 1.091 0
504
+ 0.098 8
505
+ 38.8
506
+ SpeX
507
+ 2013 Jun 15
508
+ B
509
+ 12:16:11
510
+ 1.091 2
511
+ 0.099 1
512
+ 38.8
513
+ SpeX
514
+ 2013 Jun 18
515
+ A
516
+ 13:07:51
517
+ 1.103 3
518
+ 0.116 9
519
+ 39.7
520
+ SpeX
521
+ 2013 Jul 10
522
+ A
523
+ 10:23:08
524
+ 1.218 8
525
+ 0.256 2
526
+ 34.0
527
+ SpeX
528
+ 2013 Jul 10
529
+ B
530
+ 10:29:19
531
+ 1.218 9
532
+ 0.256 2
533
+ 34.0
534
+ SpeX
535
+ 2013 Jul 10
536
+ C
537
+ 11:10:20
538
+ 1.219 0
539
+ 0.256 4
540
+ 34.0
541
+ SpeX
542
+ 2013 Jul 10
543
+ D
544
+ 11:49:53
545
+ 1.219 2
546
+ 0.256 6
547
+ 34.0
548
+ SpeX
549
+ 2013 Jul 10
550
+ E
551
+ 13:09:29
552
+ 1.219 6
553
+ 0.257 0
554
+ 34.0
555
+ SpeX
556
+ 2017 Jul 01
557
+ A
558
+ 10:51:35
559
+ 1.767 6
560
+ 1.445 3
561
+ 35.1
562
+ NEOWISE
563
+ Note. Set refers to different data sets on a given night. Midtime is the midtime of observation for the data set in UTC time. (Each SpeX observation spans roughly
564
+ 20–30 minutes, while the NEOWISE observation spans 29 hr. Thus, each SpeX spectrum is separated by roughly 25°–40° of longitude.) rH is the Sun–object distance,
565
+ Δ is the Earth–object distance, and α is the solar phase angle. Note that the observations are carried out across a range of solar phase angles and viewing geometries.
566
+ 7
567
+ https://www.ipac.caltech.edu/doi/irsa/10.26131/IRSA144
568
+ 4
569
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
570
+ Myers et al.
571
+
572
+ Figure 2. Processed LXD data sets for each night of observations with SpeX and NEOWISE. (a–f) SpeX data for each of the six nights. The different letters within
573
+ each panel indicate different data sets collected each night (Table 1). The y-axis is normalized flux, normalized to 1.6 μm. (Note that there is no significant thermal
574
+ contamination at this wavelength.) (g) NEOWISE data in absolute flux density. Note that the NEOWISE data are plotted over a different wavelength range. We plot
575
+ both the 1σ and 3σ uncertainties. (h) The “A“ data set for each night of SpeX data. These spectra highlight how different viewing geometries across the different nights
576
+ produce a range of spectral slopes. We see that changes in viewing geometry produce changes in the spectra shape both within nights and across all nights of
577
+ observations. Modeling these differences allows us to place tighter constraints on NEA properties.
578
+ 5
579
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
580
+ Myers et al.
581
+
582
+ 125
583
+ A)
584
+ B)
585
+ 100
586
+ xnI
587
+ 2013 May 30
588
+ 2013 Jun 02
589
+ Normalized
590
+ 75
591
+ AB
592
+ 50
593
+ CD
594
+ 25
595
+ 0
596
+ 125
597
+ C
598
+ D)
599
+ 100
600
+ Flux
601
+ Normalized
602
+ 75
603
+ 2013 Jun 15
604
+ 2013 Jun 08
605
+ A
606
+ A
607
+ 50
608
+ BCDE
609
+ +
610
+ 25
611
+ 0
612
+ 125
613
+ F)
614
+ E)
615
+ 100
616
+ Normalized
617
+ 75
618
+ 2013 Jul 10
619
+ 2013 Jun 18
620
+ AB-
621
+ +A
622
+ +
623
+ 50
624
+ +
625
+ CDE
626
+ +
627
+ 25
628
+ 3.2
629
+ 3.7
630
+ 4.2
631
+ 7
632
+ 3.2
633
+ 3.7
634
+ 4.2
635
+ Wavelength (microns)
636
+ Wavelength (microns)
637
+ 1e-20
638
+ 125
639
+ G)
640
+ H)
641
+ _wn
642
+ 8e-21
643
+ 100
644
+ SpeX, All Nights
645
+ 2017 Jul 01
646
+ Normalized I
647
+ 2013 May 30
648
+ 6e-21
649
+ 75
650
+ 2013 Jun 02
651
+ 3g
652
+ 2013 Jun 08
653
+ +
654
+ 2013 Jun 15
655
+ 4e-21
656
+ 50
657
+ 2013 Jun 18
658
+ 2013 Jul 10
659
+ 25
660
+ 2e-21
661
+ 0e+00
662
+ 3.2
663
+ 2.5
664
+ 3.5
665
+ 4.5
666
+ 3.7
667
+ 4.2
668
+ 3.0
669
+ 4.0
670
+ 5.0
671
+ Wavelength (microns)
672
+ Wavelength (microns)The Bond albedo is estimated according to the method
673
+ described in Lebofsky & Spencer (1989):
674
+ A
675
+ G p
676
+ 0.29
677
+ 0.684
678
+ ,
679
+ 2
680
+ (
681
+ )
682
+ ( )
683
+ =
684
+ +
685
+ where G is the slope parameter in the HG magnitude system
686
+ (Bowell et al. 1989) and p is the visual geometric albedo. The
687
+ standard assumption of G = 0.15 is used, and p is taken from
688
+ the model fits to the SpeX data. Note that since the fitting
689
+ process is iterative, choices of the initial guess parameters do
690
+ not strongly affect the final result. The end products of this
691
+ conversion process are flux densities reported in units of W
692
+ cm−2 μm−1, which match the units of our simple thermal
693
+ model output. The final NEOWISE data for QE2 are shown in
694
+ Figure 2. We show the data with both 1σ and 3σ uncertainties.
695
+ 2.3. Radar Shape Model
696
+ As part of our investigation into the limitations of simple
697
+ thermal models, we compare the results of our NEATM-like
698
+ models to many other data sources and models, including radar
699
+ images and a radar shape model. The radar image is a direct
700
+ measurement of the size that only depends on the viewing
701
+ geometry and the speed of light. A spheroidal object, such as
702
+ QE2, shows a radius in radar range at nearly all aspects and is a
703
+ robust size estimate. We compare the radar size to sizes derived
704
+ from our NEATM-like model, based on the magnitude and
705
+ albedo. We emphasize that this information is not used as an
706
+ input of our NEATM-like model and is only used to compare
707
+ with our NEATM-like model results.
708
+ The radar shape model for QE2 is described by Springmann
709
+ et al. (2014). The model is constructed using observations from
710
+ the Arecibo Observatory and Goldstone. Data used were
711
+ collected between 2013 May 31 and June 9, during QE2ʼs close
712
+ approach to Earth. These radar images are used to derive a
713
+ shape model as described in Magri et al. (2011). A nonlinear
714
+ iterative process is used to adjust synthetic radar images to
715
+ match the observations by minimizing the difference between
716
+ them. This process is described in detail in several papers for
717
+ other objects (Magri et al. 2011; Nolan et al. 2013). The shape
718
+ model of QE2 is preliminary, and the complete analysis is
719
+ beyond the scope of this paper. However, the derived diameter
720
+ of the principal axes of QE2 is robust and reliable as a
721
+ comparison to values obtained here. This analysis gives a
722
+ diameter for QE2 of 3.2 ± 0.3 km and a diameter of the
723
+ secondary of 800 ± 80 m. QE2 is spheroidal, with a few
724
+ dominant surface features.
725
+ Springmann
726
+ et
727
+ al.
728
+ (2014)
729
+ find
730
+ a
731
+ rotation
732
+ rate
733
+ of
734
+ 4.749 ± 0.002 hr for QE2 and two possible pole solutions,
735
+ both of which are prograde. One of these solutions, which we
736
+ refer to as the A solution, places most of the “bumpy”
737
+ topography of QE2 in the northern hemisphere. This solution
738
+ has a pole position of λ = 119° and β = 55°, where λ is the
739
+ ecliptic pole longitude and β is the ecliptic pole latitude. The
740
+ second solution, which we refer to as the B solution, places the
741
+ “bumpy” topography partially in the southern hemisphere. This
742
+ solution has a pole position of λ = 158° and β = 41°. Both
743
+ solutions are shown in Figure 3.
744
+ 3. NEATM-like Model
745
+ The simple thermal model we use to fit the data is based on
746
+ the
747
+ Standard
748
+ Thermal
749
+ Model
750
+ (Lebofsky
751
+ et
752
+ al.
753
+ 1986;
754
+ Lebofsky & Spencer 1989) and NEATM (Harris 1998). Our
755
+ Figure 3. Sky views of QE2 on 2013 July 10 that show the radar shape model from Springmann et al. (2014). The arrows indicate the pole and spin direction. Left: the
756
+ A solution with a pole position of λ = 119° and β = 55°. Right: the B solution with a pole position of λ = 158° and β = 41°.
757
+ Table 2
758
+ List of Individual NEOWISE Observations Used to Obtain the Single
759
+ Averaged NEOWISE Data Set
760
+ Date
761
+ Midtime
762
+ m1 (mag)
763
+ σ1 (mag)
764
+ m2 (mag)
765
+ σ2 (mag)
766
+ 2017 Jun 30
767
+ 19:32:22
768
+ 16.768
769
+ 0.468
770
+ 13.609
771
+ 0.136
772
+ 2017 Jun 30
773
+ 22:41:03
774
+ 16.256
775
+ 0.253
776
+ 13.844
777
+ 0.158
778
+ 2017 Jul 01
779
+ 03:23:49
780
+ 16.625
781
+ 0.392
782
+ 13.944
783
+ 0.172
784
+ 2017 Jul 01
785
+ 06:32:19
786
+ 16.966
787
+ 0.535
788
+ 13.658
789
+ 0.131
790
+ 2017 Jul 01
791
+ 15:58:00
792
+ 16.449
793
+ 0.338
794
+ 14.193
795
+ 0.292
796
+ 2017 Jul 01
797
+ 19:06:30
798
+ 16.927
799
+ 0.522
800
+ 13.694
801
+ 0.135
802
+ 2017 Jul 01
803
+ 22:15:00
804
+ 16.557
805
+ 0.476
806
+ 13.801
807
+ 0.161
808
+ 2017 Jul 02
809
+ 01:23:41
810
+ 16.539
811
+ 0.375
812
+ 13.770
813
+ 0.124
814
+ 2017 Jul 01
815
+ 10:51:35
816
+ 16.528
817
+ 0.092
818
+ 13.758
819
+ 0.051
820
+ Note. Midtime is the midtime of observation in UTC time. m1 and m2 are the
821
+ NEOWISE reported magnitudes for W1 (effective wavelength 3.4 μm) and W2
822
+ (effective wavelength 4.6 μm), respectively. σ1 and σ2 are the NEOWISE
823
+ reported magnitude uncertainties for W1 and W2, respectively. The last row is
824
+ the averaged observation.
825
+ 6
826
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
827
+ Myers et al.
828
+
829
+ model is a variation of these models that we call our NEATM-
830
+ like model (Howell et al. 2018). Like these models, for a given
831
+ set of asteroid parameters, our NEATM-like model produces a
832
+ theoretical thermal emission spectrum of the object that can be
833
+ fit to any subset of the visible to near-IR spectra of an asteroid.
834
+ However, our model also utilizes a simple incorporation of the
835
+ rotation rate of the object that allows us to model the thermal
836
+ inertia. The thermal inertia is a measurement of how well the
837
+ object’s surface retains heat energy from the Sun and is
838
+ measured in J m−2 s−1/2 K−1 (hereafter referred to as TIU for
839
+ thermal inertia units). By determining the thermal inertia, in
840
+ combination with the rotation rate, our NEATM-like model is
841
+ able to account for differences across the day and night sides of
842
+ an object. Thus, when incorporating many different observa-
843
+ tions of a single object, taken at different viewing geometries,
844
+ we are able to model how changes in thermal inertia affect the
845
+ thermal emission of an object. Overall, this incorporation
846
+ allows us to get a more robust picture of the properties of the
847
+ object. We note that other than this addition, this model is
848
+ functionally similar to the standard NEATM model.
849
+ In addition to incorporating these parameters, our model also
850
+ makes the typical assumption of a spherical shape for the
851
+ asteroid. It also assumes subsolar and subobserver points on the
852
+ asteroid’s equator and prograde rotation at a fixed rotation rate.
853
+ (The NEATM-like model does not account for shape effects,
854
+ and the radar-derived shape model of Springmann et al. 2014 is
855
+ only used to compare to the NEATM-like model results to
856
+ investigate the limitations of the NEATM-like model.) The
857
+ model also incorporates a free-floating beaming parameter—a
858
+ scaling factor between the observed and predicted flux from the
859
+ asteroid. This factor accounts for additional effects not included
860
+ in the model, such as surface roughness, deviations from a
861
+ spherical shape, local shadowing, and nonzero obliquity. The
862
+ beaming parameter generally ranges between ∼0.5 and 2.0,
863
+ with higher values usually occurring at higher phase angles or
864
+ for more irregularly shaped asteroids.
865
+ Overall, our model includes three free-floating parameters:
866
+ the visual geometric albedo, thermal inertia, and beaming
867
+ parameter. The output of each run is a model spectrum of the
868
+ asteroid, based on the input parameters, for each combination
869
+ of the free-floating parameters. Thus, identifying best-fit
870
+ parameters requires inspecting the model results and making
871
+ direct comparisons to the data.
872
+ For a given object, the consistency of these fit parameters
873
+ can be checked by comparing the results to thermal infrared
874
+ data collected across multiple nights that represent a range of
875
+ viewing geometries. This is important because many combina-
876
+ tions of albedo, thermal inertia, and beaming parameter can fit
877
+ any individual observation. By comparing model results for a
878
+ single object to data taken at multiple different viewing
879
+ geometries of that object, we can thus identify consistent values
880
+ of albedo and thermal inertia that fit every observation,
881
+ breaking degeneracies in the solution. The beaming parameter
882
+ is allowed to vary, as it is expected to change in value across
883
+ each observation. Thus, across multiple different viewing
884
+ geometries, only a tight range of albedo and thermal inertia
885
+ values will fit every observation. This is true even when the
886
+ beaming parameter is allowed to vary, as more extreme
887
+ deviations in albedo or thermal inertia would require increas-
888
+ ingly extreme values of the beaming parameter to fit the
889
+ observations, and realistic beaming parameters are generally
890
+ constrained to the range of ∼0.5–2.0 (Delbó et al. 2003). Note
891
+ that these comparisons are done solely to constrain the
892
+ parameter fits of the NEATM-like model and are separate
893
+ from the comparisons done as part of our investigation into the
894
+ limitations of the NEATM-like model (Section 5).
895
+ The fixed model inputs for our NEATM-like model are the
896
+ object's rotation period, a visible-to-near-IR reflectance ratio,
897
+ Earth–object and Sun–object distances, solar phase angle,
898
+ emissivity, and spherical equivalent diameter. For QE2, we use
899
+ a rotation period of 4.749 ± 0.002 hr that was used by a
900
+ previously derived radar shape model (Springmann et al. 2014).
901
+ We also use a spherical equivalent diameter of 3.2 km from the
902
+ same shape model. We note that since the shape of QE2 is very
903
+ close to spherical, the assumption of spherical shape by the
904
+ NEATM-like model is a very good assumption. The visible-to-
905
+ near-IR reflectance ratio is estimated to be 1.127 using our
906
+ SpeX prism spectra and a visible spectrum obtained by Hicks
907
+ et al. (2013). This is a color correction factor used to relate the
908
+ visible albedo to the near-infrared albedo at 1.6 μm, chosen as
909
+ the normalization wavelength of the spectra. Earth–object and
910
+ Sun–object distances, as well as solar phase angle, are
911
+ calculated for each observation using JPL Horizons8 based
912
+ on the midtime of observation for each data set. These values
913
+ are listed in Table 1. The emissivity is set to 0.9.
914
+ 4. NEATM-like Model Results
915
+ We generate NEATM-like models for each of our normal-
916
+ ized flux SpeX data sets and our single absolute photometry
917
+ NEOWISE data set. Models are generated across a wide range
918
+ of albedos, thermal inertias, and beaming parameters. Models
919
+ are then compared to the data using an objective function to
920
+ constrain QE2ʼs properties. For any given data set, models of
921
+ varying parameters change monotonically (Figure 4). These
922
+ models are sorted by calculating a reduced χ2 between the
923
+ model and the data. When performing this calculation, we only
924
+ consider data points between 3.00 and 4.05 μm, as this is the
925
+ region of strongest thermal emission without significant
926
+ overlap with atmospheric water vapor lines. For the NEOWISE
927
+ data set, both NEOWISE data points are used.
928
+ It is important to note that the reduced χ2 value we calculate
929
+ is not a formal χ2, as it does not reach a minimum at unity and
930
+ does not go up by a value of 1 when the model is 1σ away from
931
+ the data. This is because the uncertainties in the data are
932
+ dominated by systematic effects, not statistical errors. The data
933
+ points are not independent, as they are strongly correlated in
934
+ wavelength and are affected by changing effects such as
935
+ atmospheric conditions on different days, viewing geometry,
936
+ and rotational changes of the asteroid. As a result, this
937
+ calculation can be used to sort the goodness of fit of models for
938
+ a given data set but cannot be used to compare models across
939
+ data sets. Thus, for each data set, we use this method to identify
940
+ the range of albedos and thermal inertias that produce models
941
+ that lie within the 1σ uncertainties of the data. Figure 5 shows
942
+ the variation in models that were accepted to fit the data for
943
+ each data set. (Note that for the NEOWISE data we also
944
+ examine the models that fit within the 3σ uncertainties. This
945
+ range is also shown for the NEOWISE data.) Any models
946
+ within the shown region are considered to fit the data. All other
947
+ models for the given data set are discarded, as they are poor fits
948
+ to the data.
949
+ 8
950
+ https://ssd.jpl.nasa.gov/horizons/
951
+ 7
952
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
953
+ Myers et al.
954
+
955
+ For each data set, we then have a range of albedos and
956
+ thermal inertias that can be said to fit that given data set. These
957
+ individual fit spaces are shown in Figure 6. (For the NEOWISE
958
+ data, we show the models that fit the 1σ uncertainties.) Overall,
959
+ we have 21 such data sets: 20 data sets spread across six nights
960
+ of IRTF SpeX observations, and 1 set of NEOWISE data. To
961
+ identify the range of albedos and thermal inertias that describe
962
+ QE2 overall, we then search for the region of overlap between
963
+ each of these 21 different model sets. These results are shown
964
+ in Figure 7. There is a clear section in the parameter space of
965
+ models that fit nearly every data set. We define this region as
966
+ the best-fit space.
967
+ All models within this space are consistent with the SpeX
968
+ data, but do not fit the NEOWISE data with 1σ uncertainties.
969
+ We then examine models that fit the NEOWISE data with 3σ
970
+ uncertainties, and find that all models within the best-fit space
971
+ are consistent with the NEOWISE data. This could be because
972
+ the NEOWISE observations were taken at a much higher Sun–
973
+ object distance than the SpeX data. As a result, QE2 was much
974
+ colder at the time of these observations which may be
975
+ introducing complexities to the thermal emission that our
976
+ simple thermal model is not able to capture. Such effects may
977
+ be better understood using a more complex thermophysical
978
+ model, however a full investigation of this effect is beyond the
979
+ scope of this work.
980
+ Overall, our analysis gives best-fit ranges of 0.05–0.10 for
981
+ the visual geometric albedo and 0–425 TIU for the thermal
982
+ inertia. Note that there is a correlation such that higher thermal
983
+ inertias require lower albedos. Results are summarized in
984
+ Table 3.
985
+ In general, we find a preference for lower beaming
986
+ parameters of ∼0.55–0.80. Beaming parameter results are
987
+ shown in Figure 8. We remind the reader that we expect the
988
+ beaming parameter to change across observations, and so we
989
+ do not attempt to fit for a single overall value of the beaming
990
+ parameter. These values are calculated by taking the best-fit
991
+ beaming parameter value for a fixed albedo of 0.07 and a fixed
992
+ thermal inertia of 150 TIU. These values are chosen because
993
+ they are near the center of the best-fit region. The NEOWISE
994
+ beaming parameters are calculated using the 3σ uncertainties as
995
+ they are the results consistent with the SpeX data. As expected,
996
+ the beaming parameter is generally higher for higher phase
997
+ angles. The exceptions to this trend are July 10 and the
998
+ NEOWISE data, both of which have substantially greater rH
999
+ and Δ values than the other nights. These larger distances also
1000
+ explain the noisier data observed on July 10.
1001
+ 5. Limits of the NEATM-like Model
1002
+ In calculating our best-fit model ranges, we compared our
1003
+ model results across many data sets taken at different viewing
1004
+ geometries of QE2 (Figure 1). These comparisons have
1005
+ allowed us to place tighter constraints on our modeled albedo
1006
+ and thermal inertia than would be possible with single
1007
+ observations. These albedos and thermal inertias can then be
1008
+ compared to results from more complex thermophysical
1009
+ models, radar data, and other observations to identify how
1010
+ accurately the NEATM-like model was able to constrain the
1011
+ properties of QE2. Our model results also provide us with a
1012
+ range of beaming parameter values that change as a function of
1013
+ viewing geometry. Analyzing these changes in beaming
1014
+ parameter can allow us to identify the unmodeled factors
1015
+ limiting the accuracy of our NEATM-like model. Overall, by
1016
+ comparing our model results to previous studies of QE2, we
1017
+ can gain insight into the limitations of simple thermal models
1018
+ as applied to a single object. In the subsections below we walk
1019
+ through comparisons of our simple thermal model results to
1020
+ various other models and data sets. For each comparison, we
1021
+ discuss in what ways our simple thermal model results differ
1022
+ and discuss implications for the factors affecting the uncertain-
1023
+ ties of simple thermal model results.
1024
+ 5.1. Albedo, Size, and H-magnitude
1025
+ Our modeled visual geometric albedo for QE2 of 0.05–0.10
1026
+ is higher than but overlaps with previously published values of
1027
+ 0.03 0.02
1028
+ 0.03
1029
+ -
1030
+ +
1031
+ (Moskovitz et al. 2017) and 0.04 ± 0.01 (Fieber-
1032
+ Beyer et al. 2020). We can use our modeled albedo, in
1033
+ combination with a radar-derived size, to estimate QE2ʼs H-
1034
+ magnitude. This is given by the relationship
1035
+
1036
+
1037
+
1038
+
1039
+ H
1040
+ p
1041
+ D
1042
+ 5 log
1043
+ 1329 km ,
1044
+ 3
1045
+ 10
1046
+ ( )
1047
+ = -
1048
+ where p is the albedo and D is the object diameter in kilometers
1049
+ (Pravec & Harris 2007, Equation (3)). Using the diameter of
1050
+ 3.2 ± 0.3 km given by Springmann et al. (2014) and our
1051
+ modeled albedo range of 0.05–0.10, we get an H-magnitude of
1052
+ 15.4–16.6. This value is lower than (but partially overlaps with)
1053
+ previously given H-magnitude values of 16.4 (Trilling et al.
1054
+ 2010) and 17.3 (Moskovitz et al. 2017) for QE2.
1055
+ However, the radar shape model constrains the diameter with
1056
+ high accuracy. The radar-derived shape can be considered a
1057
+ true constraint on QE2ʼs size, as size can be measured directly
1058
+ from a radar image (Ostro 1985). Figure 9 shows a radar image
1059
+ of QE2 taken by the Arecibo Telescope on 2013 June 10. The
1060
+ vertical extent of the image shows distance from the observer to
1061
+ the terminator of the object. Thus, the resolution of the pixels,
1062
+ combined with knowledge of the speed of light, directly gives
1063
+ the object’s radius. In this image, QE2 covers 210 pixels in the
1064
+ vertical extent at 7.5 m pixel−1, giving an apparent radius of
1065
+ 1575 m or a diameter of 3.15 km. However, using an H-
1066
+ magnitude of 17.3 and albedos of 0.05–0.10 gives a diameter
1067
+ Figure 4. A range of NEATM-like models compared to one of our SpeX data
1068
+ sets. As either the albedo or thermal inertia changes monotonically, the models
1069
+ correspondingly change monotonically across the data. This property allows us
1070
+ to identify a range of models that fit the data and is typical to all of our data
1071
+ sets. All models that fall within the 1σ error bars of the data would be
1072
+ considered good fits to the data. As such, in this case only the pV = 0.06 and
1073
+ Γ = 100 TIU model would be considered a good fit. Models shown here all
1074
+ have η = 0.86. Changes in beaming parameter can also monotonically affect
1075
+ how the models fit to the data.
1076
+ 8
1077
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1078
+ Myers et al.
1079
+
1080
+ Variation in NEATM-like Models
1081
+ 125
1082
+
1083
+ 30 May A
1084
+ 100
1085
+ pv =0.03, =100
1086
+ Normalized Flux
1087
+ pv =0.06, I =100
1088
+ pv =0.09, I =100
1089
+ 75
1090
+ pv =0.06, I =0
1091
+
1092
+ pv =0.06, I =200
1093
+
1094
+
1095
+
1096
+
1097
+ 50
1098
+ 25
1099
+ 3.2
1100
+ 3.7
1101
+ 4.2
1102
+ Wavelength (microns)Figure 5. The variation in NEATM-like models that were accepted to fit the data for each data set. Any models within the shaded region are considered to fit the data.
1103
+ All other models for the given data set are discarded, as they are poor fits to the data. An objective function is used to identify which models fall within the shown
1104
+ region (Section 4). (a–f) SpeX data. The y-axis is normalized flux. The spectra are offset for clarity. (g) NEOWISE data in absolute flux density. Note that the
1105
+ NEOWISE data are plotted over a different wavelength range. For the NEOWISE data we examine models that fit within both the 1σ and 3σ uncertainties. Both
1106
+ regions are shown.
1107
+ 9
1108
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1109
+ Myers et al.
1110
+
1111
+ 250
1112
+ A)
1113
+ B)
1114
+ 200
1115
+ xn
1116
+ 2013 Jun 02
1117
+ 2013 May 30
1118
+ ABCD
1119
+ ABC
1120
+ Normali
1121
+ 100
1122
+ 50
1123
+ 0
1124
+ 250
1125
+ C)
1126
+ D)
1127
+ 2013 Jun 08
1128
+ 2013 Jun 15
1129
+ A
1130
+ BCDE
1131
+ A
1132
+ Normal
1133
+ B
1134
+ 100
1135
+ 50
1136
+ 0
1137
+ 250
1138
+ E)
1139
+ F)
1140
+ 200
1141
+ lux
1142
+ 2013 Jul 10
1143
+ 2013 Jun 18
1144
+ 十+
1145
+ ABCDE
1146
+ + A
1147
+ 100
1148
+ 50
1149
+ 0
1150
+ 2.7
1151
+ 3.2
1152
+ 3.7
1153
+ 4.2
1154
+ 3.2
1155
+ 3.7
1156
+ 4.2
1157
+ Wavelength (microns)
1158
+ Wavelength (microns)
1159
+ 1e-20
1160
+ G)
1161
+ wn
1162
+ 9e-21
1163
+ 8e-21
1164
+ 2017 Jul 01
1165
+ 7e-21
1166
+ 6e-21
1167
+ 1g
1168
+ 3g
1169
+ 5e-21
1170
+ 4e-21
1171
+ 3e-21
1172
+ 2e-21
1173
+ 1e-21
1174
+ 0e+00
1175
+ 2.5
1176
+ 3.0
1177
+ 3.5
1178
+ 4.0
1179
+ 4.5
1180
+ 5.0
1181
+ Wavelength (microns)Figure 6. Reduced χ2 maps for each of the spectra as fit by our simple, NEATM-like model. Warmer colors mean higher values (worse fits), and cooler colors mean
1182
+ lower values (better fits). Note that different max values are used for different spectra, as the reduced χ2 are not directly comparable across different spectra
1183
+ (Section 4). Each χ2 map is equivalent to showing the range of models that fit a given data set.The fit space of the NEOWISE data corresponds to the 1σ uncertainties
1184
+ 10
1185
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1186
+ Myers et al.
1187
+
1188
+ 0.18
1189
+ 0.16
1190
+ X
1191
+ 30 May A
1192
+ 30 May B
1193
+ 7.00
1194
+ 30 May C
1195
+ 6
1196
+ 0.14
1197
+ 5.25
1198
+ 0.12
1199
+ 3.50
1200
+ 1.75
1201
+ 0.00
1202
+ 0.06
1203
+ 0.04
1204
+ 0.02
1205
+ 0.18
1206
+ 0.16
1207
+ X
1208
+ 02 Jun A
1209
+ 02 Jun B
1210
+ 02 Jun C
1211
+ 0.14
1212
+ 2
1213
+ 0.12
1214
+ 0.06
1215
+ 0.04
1216
+ 0.02
1217
+ 0.18
1218
+ 0.16
1219
+ x
1220
+ 02 Jun D
1221
+ 08 Jun A
1222
+ 08 Jun B
1223
+ 0.14
1224
+ 6
1225
+ 4
1226
+ 0.12
1227
+ 2
1228
+ 2
1229
+ 0
1230
+ 0.06
1231
+ 0.04
1232
+ 0.02
1233
+ 0.18
1234
+ 0.16
1235
+ X
1236
+ 08 Jun C
1237
+ 08 Jun D
1238
+ 08 Jun E
1239
+ 0.14
1240
+ 3
1241
+ 0.12
1242
+ 2
1243
+ 0 0.08
1244
+ 0.06
1245
+ 0.04
1246
+ 0.02
1247
+ 0.18
1248
+ 0.16
1249
+ x
1250
+ 15 Jun A
1251
+ 15 Jun B
1252
+ 18 Jun A
1253
+ 6
1254
+ 6
1255
+ 12
1256
+ 0.14
1257
+ 4
1258
+ 0.12
1259
+ 2
1260
+ ?
1261
+ 0.06
1262
+ 0.04
1263
+ 0.02
1264
+ 0.18
1265
+ 0.16
1266
+ 10 Jul A
1267
+ 10 Jul B
1268
+ 10 Jul C
1269
+ 0.14
1270
+ 3
1271
+ 0.12
1272
+ 2
1273
+ 0.06
1274
+ 0.04
1275
+ 0.02
1276
+ 0.18
1277
+ 0.16
1278
+ 10 Jul D
1279
+ 10 Jul E
1280
+ 3.00
1281
+ 0.14
1282
+ 5.25
1283
+ .25
1284
+ 0.12
1285
+ 3.50
1286
+ .50
1287
+ 1.75
1288
+ 0.75
1289
+ 0.00
1290
+ 1.2
1291
+ 0.00
1292
+ 0.9
1293
+ 0.6
1294
+ 0.06
1295
+ 0.3
1296
+ 0.04
1297
+ NEOWISE
1298
+ 0.0
1299
+ 0.02
1300
+ 0 50 100 150 200 250 300 350 400 450 500 550 050 100 150 200 250 300 350 400 450 500 550 050 100 150 200 250 300 350 400 450 500 550
1301
+ Thermal Inertia (TIU)
1302
+ Thermal Inertia (TIU)
1303
+ Thermal Inertia (TIU)between 1.5 and 2.1 km, well outside of the 1σ errors of the
1304
+ radar measurement.
1305
+ We investigate this unusually large discrepancy in the H-
1306
+ magnitude by looking at existing observations. Using an H-
1307
+ magnitude value and an assumed G value, we can calculate
1308
+ predicted apparent magnitudes. These predicted apparent
1309
+ magnitudes can then be compared to observed apparent
1310
+ magnitudes reported to the Minor Planet Center (MPC).9
1311
+ Ephemeris values are calculated for QE2 using JPL Horizons10
1312
+ at 1-day intervals throughout 2013. We then calculate predicted
1313
+ apparent magnitudes for the H-magnitude consistent with the
1314
+ radar-determined
1315
+ size and our modeled albedo, the H-
1316
+ magnitude used by Moskovitz et al. (2017), and a range of G
1317
+ values from 0 to 0.15. This was done following the procedure
1318
+ in Bowell et al. (1989). These predicted apparent magnitudes
1319
+ are then compared to all the apparent magnitudes listed in the
1320
+ MPC. The results are shown in Figure 10. We see that H-
1321
+ magnitudes of neither 16.0 nor 17.3 perfectly match the data,
1322
+ but instead provide an upper and lower bound, respectively.
1323
+ However, we note that an H-magnitude of 16.0 appears to
1324
+ provide a more reasonable fit than an H-magnitude of 17.3.
1325
+ So what could be causing these H-magnitude differences?
1326
+ One possible explanation is related to the G parameter. The G
1327
+ parameter is often assumed to be 0.15 and is not fitted directly.
1328
+ Figure 10 shows that for H = 16.0 lower G values fit better,
1329
+ while for H = 17.3 higher G values fit better. For QE2, we
1330
+ would expect a lower G value, as lower G values are generally
1331
+ preferred
1332
+ for
1333
+ low-albedo
1334
+ objects
1335
+ owing
1336
+ to
1337
+ the
1338
+ smaller
1339
+ opposition effect. However, we note that the differences do
1340
+ not exceed ∼0.5 mag and thus cannot fully explain the
1341
+ discrepancy.
1342
+ Another possible explanation is related to color effects;
1343
+ however, the color of QE2 is very close to solar, and thus this is
1344
+ also unlikely to be a large factor in this case. The discrepancy
1345
+ could also be due to the secondary contributing to the
1346
+ magnitude. Using the radar shape model (Springmann et al.
1347
+ 2014), we can calculate the effective diameter of the combined
1348
+ primary and secondary to be 3.3 ± 0.3 km. Using our modeled
1349
+ albedo range, this gives an H-magnitude difference of only
1350
+ ∼0.1 and thus is an ignorable contribution to the uncertainty.
1351
+ Therefore, none of these effects by themselves can fully explain
1352
+ the observed differences. Overall, given the accuracy of the
1353
+ radar measurement of the diameter and our tightly constrained
1354
+ albedo range, the true H-magnitude cannot be as high as 17.3.
1355
+ It is therefore likely that a better estimate of the H-magnitude
1356
+ lies somewhere in between 16.0 and 17.3. Furthermore, our
1357
+ analysis shows that higher H-magnitudes and thus lower
1358
+ albedos are
1359
+ likely favored
1360
+ for QE2, potentially
1361
+ further
1362
+ constraining the results from our simple thermal model.
1363
+ 5.2. Wavelength Range of Observations
1364
+ We can also analyze our results by leveraging the large
1365
+ wavelength range of our observations. Our observations span
1366
+ 0.8–4.1 μm, and thus we are able to observe both the thermally
1367
+ dominated region of the spectra (3.0 μm) and the thermal tail
1368
+ (∼2.0–2.5 μm). We are therefore able to compare our model
1369
+ fits to both regions. This is notable because many studies (e.g.,
1370
+ Moskovitz et al. 2017) rely only on the tail region. We show
1371
+ this comparison for a selection of our data sets in Figure 11.
1372
+ We find that in nearly all cases the models that best fit the
1373
+ thermally dominated region also fit the tail region. However,
1374
+ for some dates (such as some data sets for 2013 July 10), an
1375
+ albedo increase of ∼0.02 relative to the model that fits the
1376
+ thermally dominated region is required to fit the tail region.
1377
+ This implies that QE2 may have an inhomogeneous surface and
1378
+ that we may be observinglocal thermal variations. Such
1379
+ variations could impart a wavelength-dependent change in the
1380
+ flux, thus creating the observed discrepancy. Another possibi-
1381
+ lity is that some other effect, such as surface roughness, that our
1382
+ NEATM-like model does not account for may be causing this
1383
+ mismatch. This result is important because it shows the dangers
1384
+ of relying on only a limited spectral region to derive surface
1385
+ properties such as albedo.
1386
+ 5.3. Surface Topography
1387
+ The potential effects of a surface inhomogeneity can be
1388
+ investigated by comparing our NEATM-like model results to
1389
+ results from a more complex thermal model. In addition to our
1390
+ NEATM-like models, we generate models using SHERMAN.
1391
+ SHERMAN is a more complex thermophysical model that
1392
+ Figure 7. Final best-fit space for the visible geometric albedo and thermal
1393
+ inertia for QE2 using our simple, NEATM-like model. The color of the points
1394
+ represents the number of data sets that are fit by the associated parameter
1395
+ values. A cooler color means that the given parameters are consistent with more
1396
+ data sets. White indicates models consistent with £ 2 data sets. The black line
1397
+ outlines the region of best fit. This region corresponds to the region of overlap
1398
+ between all the individual model ranges found to fit each individual data set
1399
+ (Section 4). There is a correlation such that higher thermal inertias require
1400
+ lower albedos. All models were run with the same fixed model inputs listed in
1401
+ Section 3 and using ephemeris inputs listed in Table 1. This figure is generated
1402
+ using the results from the 1σ uncertainties on the NEOWISE data.
1403
+ Table 3
1404
+ Best-fit Model Ranges for the Three Free-floating Parameters of Our NEATM-
1405
+ like Model
1406
+ Parameter
1407
+ Range
1408
+ Albedo
1409
+ 0.05–0.10
1410
+ Thermal inertia
1411
+ 0–425 TIU
1412
+ Beaming parameter
1413
+ ∼0.55–0.80
1414
+ Note. Albedo is visual geometric albedo. We expect the albedo and thermal
1415
+ inertia to be consistent across all data sets, and thus the ranges given represent
1416
+ the uncertainty in our model results. However, we expect the range of
1417
+ acceptable beaming parameters to change across observations, and thus the
1418
+ range given represents the range of values observed across all data sets.
1419
+ 9
1420
+ https://minorplanetcenter.net/
1421
+ 10 https://ssd.jpl.nasa.gov/horizons/
1422
+ 11
1423
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1424
+ Myers et al.
1425
+
1426
+ Number of Data Sets Fit per Mode
1427
+ Geometric Albedo
1428
+ 0.18
1429
+ 0.16
1430
+ Number
1431
+ 0.14
1432
+ 20
1433
+ 0.12
1434
+ 12
1435
+ 0.10
1436
+ 3
1437
+ 0.08
1438
+ 0.06
1439
+ Visual
1440
+ 0.04
1441
+ 0.02
1442
+ 0.00
1443
+ 0
1444
+ 50100150200250300350400450500550
1445
+ Thermal Inertia (TIU)takes account of the object’s shape and that can separate the
1446
+ effects of obliquity and self-shadowing. (For a full description
1447
+ of SHERMAN, see Magri et al. 2018.) We give SHERMAN
1448
+ the radar-derived shape model of QE2 (Springmann et al.
1449
+ 2014), as well as our SpeX thermal infrared data. We also input
1450
+ a reflectance spectrum from our prism data, as well as a Hapke
1451
+ Figure 8. Plot of fitted beaming parameters as a function of solar phase angle adjusted so that 0° corresponds to QE2ʼs minimum phase angle during its close approach
1452
+ to Earth. We also compare our beaming parameters to those found by Moskovitz et al. (2017). Note the introduction of negative phase angles to differentiate between
1453
+ observations taken before (positive values) and after (negative values) opposition. The error bars represent the range of beaming parameters. The range is calculated by
1454
+ identifying models that fit the data with fixed albedo and thermal inertia (Section 4). Moskovitz et al. (2017) values are taken from their Figure 3. We see that our data
1455
+ exhibit roughly the same trend where the data overlap, but that our beaming values are significantly offset from the Moskovitz et al. (2017) values.
1456
+ Figure 9. Radar image of QE2 taken by the Arecibo Telescope on 2013 June 10. The vertical extent of the image shows distance from the observer to the terminator of
1457
+ the object. The horizontal extent shows Doppler shift, with blueshift to redshift going left to right. The resolution of the pixels, combined with knowledge of the speed
1458
+ of light, directly gives the object’s radius. In this image, QE2 covers 210 pixels in the vertical extent at 7.5 m pixel−1, giving an apparent radius of 1575 m or a
1459
+ diameter of 3.15 km.
1460
+ 12
1461
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1462
+ Myers et al.
1463
+
1464
+ Beaming Parameter vs. Solar Phase Angle
1465
+ 2.0
1466
+ 1.9
1467
+ 1.8
1468
+ 1.7
1469
+ Moskovitz et al. (2017)
1470
+ 1.6
1471
+ This Work
1472
+ May11
1473
+ 1.5
1474
+ 1.4
1475
+ 1.3
1476
+ n
1477
+ 1.2
1478
+ May 30巫
1479
+ Jun15
1480
+ 巫 Jun 08
1481
+ 1.1
1482
+ Jul5
1483
+ Jun 02
1484
+ 1.0
1485
+ 0.9
1486
+ 0.8
1487
+ Jun18Jun15
1488
+ May 30 巫
1489
+ 0.7
1490
+ Jul 10巫
1491
+ 巫 Jun 08
1492
+ 巫 Jun 02
1493
+ 0.6
1494
+ NEOWISE 巫
1495
+ 0.5
1496
+ -30
1497
+ -20
1498
+ -10
1499
+ 0
1500
+ 10
1501
+ 20
1502
+ 30
1503
+ 40
1504
+ 50
1505
+ 60
1506
+ Adiusted αscattering function. SHERMAN has three free-floating para-
1507
+ meters: visual geometric albedo, thermal inertia, and crater
1508
+ fraction. The crater fraction is a proxy for surface roughness
1509
+ and describes the fraction of each model facet covered with
1510
+ hemispherical craters, following the method of Lagerros
1511
+ (1998). SHERMAN outputs a modeled thermal spectrum that
1512
+ we then compare with our thermal infrared data.
1513
+ SHERMAN is a forward model, so we generate many
1514
+ models across different values of the free-floating parameters to
1515
+ match to our data. Some preliminary model results are shown
1516
+ in Figure 12. We find that an albedo of 0.053, thermal inertia of
1517
+ 200 TIU, and crater fraction of 70% can roughly match the
1518
+ data. These values are also consistent with the results of the
1519
+ NEATM-like model.
1520
+ The SHERMAN results also show that the topography of
1521
+ QE2 is affecting the thermal emission.Using SHERMAN, we
1522
+ run models using both possible pole solutions. The results
1523
+ show slight differences in the model fits to the data between
1524
+ these solutions, with a clear preference for the B solution,
1525
+ implying that these features are most likely located in QE2ʼs
1526
+ southern hemisphere (Figure 12). Thus, topography is likely
1527
+ playing a role for QE2 and is likely affecting the uncertainties
1528
+ in the simple thermal model results. Furthermore, topography
1529
+ may be one of the effects being captured by variations in our
1530
+ NEATM-like model’s beaming parameter.
1531
+ 5.4. Beaming Parameter Trends
1532
+ The NEATM-like model’s beaming parameter is a scaling
1533
+ factor that accounts for additional effects not included in the
1534
+ model. As such, we can analyze the trend in our measured
1535
+ beaming parameters across each night of observation to
1536
+ understand the limitations of our NEATM-like model. We find
1537
+ beaming parameters that range from 0.54 to 0.78. These values
1538
+ therefore differ significantly from the value of η = 1.2 predicted
1539
+ by Harris (1998) for NEAs. Our modeled beaming parameters
1540
+ are instead much closer to the η ≈ 0.75 value predicted by
1541
+ Lebofsky et al. (1986) for main belt objects. Since the beaming
1542
+ parameter accounts for additional factors not incorporated into
1543
+ the NEATM-like model, we can use these differences to
1544
+ identify potential properties affecting QE2ʼs thermal emission.
1545
+ QE2 is a particularly good target for this analysis owing to its
1546
+ extremely spherical shape. Therefore, shape effects are likely a
1547
+ very small contributor to changes in the beaming parameter.
1548
+ One potential method for investigating beaming parameters
1549
+ is by looking for trends as a function of solar phase angle.
1550
+ Moskovitz et al. (2017) previously applied this method to QE2.
1551
+ Using beaming parameter as a proxy for thermal emission,
1552
+ Moskovitz et al. (2017) identified QE2 as a prograde rotator.
1553
+ We investigate this trend by showing the phase angle for QE2,
1554
+ which has a minimum value of 17°.1 on June 3, along with the
1555
+ fitted beaming parameters for the best-fit NEATM models for
1556
+ each night. We compare our results to those found by
1557
+ Moskovitz et al. (2017) in Figure 8.
1558
+ We find that our beaming parameter values do exhibit
1559
+ roughly the same trend as the Moskovitz et al. (2017) data but
1560
+ are significantly offset from the Moskovitz et al. (2017) data.
1561
+ We find much lower beaming parameter values than the
1562
+ Moskovitz et al. (2017) values of ∼1.1–1.4. We also find a
1563
+ range of thermal inertias that is overlapping with, but lower
1564
+ than their estimated range of ∼200–400 TIU done by
1565
+ comparing their NEATM results to more complex models.
1566
+ This is not unexpected, as our beaming parameter has been
1567
+ Figure 10. Plot of predicted apparent magnitudes for QE2 compared to all magnitudes reported to the MPC. All observations are from 2013 during QE2ʼs close
1568
+ approach to Earth. The predicted apparent magnitudes were calculated using ephemeris from JPL Horizons at 1-day intervals throughout 2013. We used H = 16.0 (a
1569
+ value from our modeled H-magnitude range) and H = 17.3 (the H-magnitude from Moskovitz et al. 2017), as well as a range of G values. We see that a lower H-
1570
+ magnitude, more consistent with our modeled range, agrees with the data for low G values.
1571
+ 13
1572
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1573
+ Myers et al.
1574
+
1575
+ Predicted Apparent Magnitudes Compared to MPC
1576
+ Observations of QE2 in 2013
1577
+ 10
1578
+ H,G
1579
+ MPc Observations
1580
+ 12
1581
+ H=16, G=0
1582
+ H=16, G=0.05
1583
+ H=16, G=0.15
1584
+ H=17.3, G=0
1585
+ H=17.3, G=0.05
1586
+ 14
1587
+ H=17.3, G=0.15
1588
+ 18
1589
+ 20
1590
+ Jan
1591
+ Mar
1592
+ Jun
1593
+ Sep
1594
+ Dec
1595
+ Timeseparated from the thermal inertia. The Moskovitz et al. (2017)
1596
+ beaming parameter must account for all the effects of thermal
1597
+ inertia, as they do not model thermal inertia explicitly, unlike
1598
+ our NEATM-like model, which does incorporate thermal
1599
+ inertia.
1600
+ Another possible explanation for why we observe different
1601
+ beaming parameters is because of our expanded wavelength
1602
+ range (Section 5.2). We incorporate data up to 4.05 μm in our
1603
+ NEATM-like model, while Moskovitz et al. (2017) only
1604
+ incorporate data up to 2.5 μm. As shown in Figure 11,
1605
+ Figure 11. Plot of NEATM-like models with varying visual geometric albedos across a selected range of dates. The data sets shown for May 30 and June 15 are the
1606
+ “A” data sets. All models shown have thermal inertia and beaming parameters that are within the best-fit ranges for the given date. Each row is a different data set. The
1607
+ left panels show the tail region, and the right panels show the thermally dominated region. We see that for July 10 A the models that fit the thermally dominated region
1608
+ do not fit the tail region and vice versa. An increase in albedo of ∼0.02 is required to fit the tail region for July 10 A. This is indicative of some kind of surface
1609
+ inhomogeneity.
1610
+ 14
1611
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1612
+ Myers et al.
1613
+
1614
+ 4
1615
+ 125
1616
+ Normalized Flux
1617
+ 100
1618
+ 3
1619
+ 75
1620
+ 30 May
1621
+ 30 May
1622
+ pv =0.07
1623
+ pv =0.07
1624
+ 50
1625
+ 25
1626
+ 0
1627
+ 0
1628
+ 125
1629
+ 4
1630
+ 100
1631
+ 3
1632
+ Normalized Flux
1633
+ L
1634
+ 75
1635
+ + 15 Jun
1636
+ 15 Jun
1637
+ Normali
1638
+ pv =0.08
1639
+ pv =0.08
1640
+ 50
1641
+ 25
1642
+ 0
1643
+ 125
1644
+ 4
1645
+ 100
1646
+ 3
1647
+ Normalized Flux
1648
+ L
1649
+ 10 Jul A
1650
+ 10 Jul A
1651
+ pv =0.07
1652
+ 75
1653
+ pv =0.07
1654
+ pv =0.08
1655
+ pv =0.08
1656
+ Normali
1657
+ pv =0.09
1658
+ pv =0.09
1659
+ 50
1660
+ 25
1661
+ 0
1662
+ 0
1663
+ 125
1664
+ 4
1665
+ 100
1666
+ 3
1667
+ FI
1668
+ Normalized
1669
+ Normalized
1670
+ 75
1671
+ 10 Jul D
1672
+ 12
1673
+ 10 Jul D
1674
+ pv =0.09
1675
+ pv =0.09
1676
+ 50
1677
+ 25
1678
+ 0
1679
+ 2.0
1680
+ 2.2
1681
+ 2.4
1682
+ 2.6
1683
+ 2.8
1684
+ 3.0
1685
+ 3.2
1686
+ 3.7
1687
+ 4.2
1688
+ Wavelength (microns)
1689
+ Wavelength (microns)mismatches in model fits between the thermally dominated
1690
+ region and tail region of the spectra are possible. We check this
1691
+ by comparing the Moskovitz et al. (2017) fits to our data at
1692
+ longer wavelengths (Figure 13). As expected, we see that
1693
+ although the Moskovitz et al. (2017) models fit the tail region,
1694
+ they do not fit the thermally dominated region.
1695
+ The differences in measured beaming parameters could also
1696
+ be related to the illumination geometry of QE2. The technique
1697
+ used by Moskovitz et al. (2017) relies on assuming that the
1698
+ observations of the asteroids were made with equatorial
1699
+ illumination and thus may not be as robust when viewing an
1700
+ object with a different illumination geometry. (Moskovitz et al.
1701
+ 2017 also recognize this possibility.) Although the observations
1702
+ of QE2 are made at low sub-Earth latitudes, it is possible that
1703
+ the discrepancy in the beaming parameters could arise from
1704
+ high subsolar latitudes. For QE2 these can range from ∼30° to
1705
+ ∼45° for the A pole solution or from ∼10° to ∼15° for the B
1706
+ pole solution. Thus, because QE2 is not being observed
1707
+ looking directly at its equator, this means that self-shadowing
1708
+ from topographical features on the asteroid’s surface is likely to
1709
+ be important. Even for the more equatorial illuminated B pole
1710
+ solution, self-shadowing could still be playing a significant
1711
+ role, as QE2 does not have an equatorial ridge and thus still has
1712
+ topographical variation at the equator. This agrees with our
1713
+ SHERMAN results that show the importance of topography on
1714
+ QE2, which may be contributing to observed temperature
1715
+ differences (Section 5.3). Thus, this may further explain why
1716
+ our beaming parameter results differ from those of Moskovitz
1717
+ et al. (2017).
1718
+ 6. Summary and Conclusions
1719
+ We present simple thermal model fits using our NEATM-
1720
+ like model for the NEA (285263) 1998 QE2. Furthermore,
1721
+ we compare these model results to more complex thermo-
1722
+ physical models, radar data, and other existing analyses of
1723
+ QE2 to understand the key factors affecting the uncertainties
1724
+ in simple thermal model results. For our simple thermal
1725
+ model fits, QE2 was observed with the SpeX instrument on
1726
+ the NASA IRTF on six nights in 2013, representing a range
1727
+ of viewing and illumination geometries. Additional data were
1728
+ acquired by the NEOWISE spacecraft in 2017. A visual
1729
+ geometric albedo between 0.05 and 0.10 and thermal inertia
1730
+ between 0 and 425 TIU are found to be consistent with all six
1731
+ nights of SpeX data. These results are also consistent with the
1732
+ NEOWISE absolute photometry at the 3σ level. These
1733
+ constraints are more robust than they would be using
1734
+ NEOWISE observations alone, due to the larger uncertainties
1735
+ on absolute photometry. The general model agreement with
1736
+ both
1737
+ absolute
1738
+ flux
1739
+ and
1740
+ normalized
1741
+ flux
1742
+ measurements
1743
+ increases our confidence in our model results, while also
1744
+ allowing us to benefit from the smaller uncertainties on
1745
+ normalized flux data. This is possible because of our
1746
+ incorporation of data representing a range of viewing
1747
+ geometries. As a result, we are able to break degeneracies
1748
+ in model results based on a single night of observations.
1749
+ In order to constrain the limits of simple thermal models as
1750
+ applied to a single object, we compare our results to more
1751
+ complex thermophysical models and previous observations.
1752
+ We find that our modeled albedo values are higher than but
1753
+ overlap with previously published values (Moskovitz et al.
1754
+ 2017; Fieber-Beyer et al. 2020) and are consistent with results
1755
+ from the complex thermophysical model SHERMAN. We also
1756
+ identify a discrepancy in the resulting H-magnitude value when
1757
+ using the radar-derived size measurement (Springmann et al.
1758
+ 2014). Based on the tight constraints we place on QE2ʼs albedo
1759
+ and the tighter constraints Springmann et al. (2014) place on
1760
+ QE2ʼs diameter, we believe that the true H-magnitude value
1761
+ must be brighter than current measurements suggest. As a
1762
+ result, the true albedo is likely toward the lower end of the
1763
+ range we identify using our NEATM-like model.
1764
+ We also leverage the wide wavelength range of our data set
1765
+ to compare our best-fit model results to both the tail region and
1766
+ thermally dominated region of our spectra. We find that for
1767
+ some dates, although our models fit the thermally dominated
1768
+ region well, they require a higher albedo to fit the tail region.
1769
+ This highlights the need to incorporate data across a wide
1770
+ wavelength range when modeling asteroid surface properties.
1771
+ We posit that these differences may be due tolocal thermal
1772
+ variations, but a full investigation is beyond the scope of
1773
+ this work.
1774
+ In addition to these discrepancies, we also find differences
1775
+ between our modeled beaming parameters and existing models.
1776
+ The most likely source of these differences may be the
1777
+ orientation of QE2 and wavelength range of data used.
1778
+ Observing these differences has also allowed us to infer that
1779
+ topography may play a significant role in determining the
1780
+ thermal emission of QE2. Thus, in this case, the inability to
1781
+ model self-shadowing effects from topographical variations
1782
+ may be a key limiting aspect of the simple thermal models.
1783
+ Furthermore, this analysis again shows the importance of
1784
+ incorporating data from a wide wavelength range when
1785
+ working with simple thermal models.
1786
+ Overall, our work has demonstrated our ability to place
1787
+ tighter constraints on the results of simple thermal models by
1788
+ comparing
1789
+ data
1790
+ taken
1791
+ across
1792
+ multiple
1793
+ different
1794
+ viewing
1795
+ geometries. By combining normalized flux with absolute
1796
+ photometry, we are able to place tighter constraints than would
1797
+ be possible with absolute photometry alone. Finally, we are
1798
+ able to place some constraints on the limits of simple thermal
1799
+ models as applied to single objects, finding that topography,
1800
+ viewing geometry, and the wavelength range of data used can
1801
+ all affect simple thermal model results. This work is important
1802
+ Figure 12. SHERMAN model results for June 8 and July 10 using both the A
1803
+ and B pole solutions. All models have a visual geometric albedo of 0.053,
1804
+ thermal inertia of 200 TIU, and crater fraction of 70%. We see a clear
1805
+ preference for the B pole solution in the June 8 data and a slight preference for
1806
+ the B pole solution in the July 10 data. Thus, we see that QE2ʼs topography
1807
+ may be playing a role in shaping its thermal emission. We also note that the
1808
+ albedo and thermal inertia are consistent with our NEATM-like model.
1809
+ 15
1810
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1811
+ Myers et al.
1812
+
1813
+ SHERMAN Models for o8 Jun
1814
+ and 10 Ju
1815
+ 125
1816
+ Normalized Flux
1817
+ 08 Jun
1818
+ 100
1819
+ 08 Jun - A
1820
+ 08 Jun - B
1821
+ 75
1822
+ 10 Jul
1823
+ 10 Jul- A
1824
+ 10 Jul - B
1825
+ 50
1826
+ 25
1827
+ 0
1828
+ 2.7
1829
+ 3.2
1830
+ 3.7
1831
+ 4.2
1832
+ Wavelength (microns)for diagnosing cases (such as QE2) where more detailed
1833
+ analysis of an object may be required to fully understand its
1834
+ properties.
1835
+ Being able to extract more information from simple thermal
1836
+ models, like our NEATM-like model, will be critical as we
1837
+ move into the future of large survey missions such as LSST and
1838
+ NEO Surveyor. The large data volumes produced by these
1839
+ missions will necessitate the use of simple models to make full
1840
+ use of the data. Using these data as efficiently as possible will
1841
+ require further insights into the limitations of simple thermal
1842
+ models. As this work shows, although these models are reliable
1843
+ for statistical measurements of large groups of objects, the
1844
+ results
1845
+ for
1846
+ individual
1847
+ objects
1848
+ may
1849
+ be
1850
+ subject
1851
+ to
1852
+ great
1853
+ uncertainties. Addressing these issues will therefore allow us
1854
+ to make full use of these models and gain even greater insights
1855
+ into fields such as planet formation, asteroid dynamics, and
1856
+ planetary defense.
1857
+ This work was partially funded by the NASA YORPD
1858
+ program (NASA grant 80NSSC21K0658) and NSF AST
1859
+ 1856411. S.A.M. was supported by the University of Arizona,
1860
+ Lunar and Planetary Laboratory, Lieutenant Colonel Kenneth
1861
+ Rondo Carson and Virginia Bryan Carson Graduate Fellow-
1862
+ ship. This material is based on work supported by the National
1863
+ Science Foundation Graduate Research Fellowship Program
1864
+ under grant No. DGE-2137419. Any opinions, findings, and
1865
+ conclusions or recommendations expressed in this material are
1866
+ those of the author(s) and do not necessarily reflect the views of
1867
+ the National Science Foundation. S.E.M. was supported by
1868
+ NASA’s Near-Earth Object Observations Program through
1869
+ grant 80NSSC19K0523.
1870
+ ORCID iDs
1871
+ Samuel A. Myers
1872
+ https://orcid.org/0000-0001-8500-6601
1873
+ Ellen S. Howell
1874
+ https://orcid.org/0000-0002-7683-5843
1875
+ Figure 13. Plot of best-fit models from Moskovitz et al. (2017) compared to our longer-wavelength data. These models are generated using our simple, NEATM-like
1876
+ model. All data sets shown are the “A” data set for the given date. All models shown have zero thermal inertia and albedos of 0.03, as per the Moskovitz et al. (2017)
1877
+ fits. The shown η values correspond to the ranges reported for each date by Moskovitz et al. (2017). The left panels show the tail region, and the right panels show the
1878
+ thermally dominated region. We see that the models fit the tail region well, as expected. However, we note that these models do not fit the thermally dominated region.
1879
+ This discrepancy may explain why we find different modeled beaming parameters than Moskovitz et al. (2017).
1880
+ 16
1881
+ The Planetary Science Journal, 4:5 (17pp), 2023 January
1882
+ Myers et al.
1883
+
1884
+ 125
1885
+ 4
1886
+ 100
1887
+ 3
1888
+ Normalized Flux
1889
+ 30 May
1890
+ 30 May
1891
+ n=1.10
1892
+ n =1.10
1893
+ Normalized |
1894
+ n =1.15
1895
+ 75
1896
+ n =1.15
1897
+ n =1.20
1898
+ n
1899
+ =1.20
1900
+ 2
1901
+ 50
1902
+ 25
1903
+ 0
1904
+ 0
1905
+ 125
1906
+ 4
1907
+ 100
1908
+ Normalized Flux
1909
+ Normalized
1910
+ 02 Jun
1911
+ 75
1912
+ 02 Jun
1913
+ n =1.05
1914
+ n =1.05
1915
+ 2
1916
+ n =1.10
1917
+ n =1.10
1918
+ n =1.15
1919
+ 50
1920
+ 王全
1921
+ 25
1922
+ 0
1923
+ 0
1924
+ 125
1925
+ 4
1926
+ 100
1927
+ Normalized Flux
1928
+ Normalized
1929
+ 15 Jun
1930
+ 15 Jun
1931
+ 75
1932
+ n =1.10
1933
+ n =1.10
1934
+ 乡乡乡乡多
1935
+ n =1.15
1936
+ n =1.15
1937
+ n =1.20
1938
+ n =1.20
1939
+ 50
1940
+ 25
1941
+ 0
1942
+ 2.0
1943
+ 2.2
1944
+ 2.4
1945
+ 2.6
1946
+ 2.8
1947
+ 3.0
1948
+ 3.2
1949
+ 3.7
1950
+ 4.2
1951
+ Wavelength (microns
1952
+ Wavelength (microns)Christopher Magri
1953
+ https://orcid.org/0000-0002-2200-4622
1954
+ Ronald J. Vervack, Jr.
1955
+ https://orcid.org/0000-0002-
1956
+ 8227-9564
1957
+ Yanga R. Fernández
1958
+ https://orcid.org/0000-0003-1156-9721
1959
+ Sean E. Marshall
1960
+ https://orcid.org/0000-0002-8144-7570
1961
+ Patrick A. Taylor
1962
+ https://orcid.org/0000-0002-2493-943X
1963
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@@ -0,0 +1,2016 @@
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
1
+ 1
2
+ TinyVers: A Tiny Versatile System-on-chip with
3
+ State-Retentive eMRAM for ML Inference at the
4
+ Extreme Edge
5
+ Vikram Jain, Sebastian Giraldo, Jaro De Roose, Linyan Mei, Bert Boons, and Marian Verhelst
6
+ Abstract—Extreme edge devices or Internet-of-thing nodes
7
+ require both ultra-low power always-on processing as well as
8
+ the ability to do on-demand sampling and processing. Moreover,
9
+ support for IoT applications like voice recognition, machine
10
+ monitoring, etc., requires the ability to execute a wide range
11
+ of ML workloads. This brings challenges in hardware design to
12
+ build flexible processors operating in ultra-low power regime.
13
+ This paper presents TinyVers, a tiny versatile ultra-low power
14
+ ML system-on-chip to enable enhanced intelligence at the Ex-
15
+ treme Edge. TinyVers exploits dataflow reconfiguration to enable
16
+ multi-modal support and aggressive on-chip power management
17
+ for duty-cycling to enable smart sensing applications. The SoC
18
+ combines a RISC-V host processor, a 17 TOPS/W dataflow
19
+ reconfigurable ML accelerator, a 1.7 µW deep sleep wake-up
20
+ controller, and an eMRAM for boot code and ML parameter
21
+ retention. The SoC can perform up to 17.6 GOPS while achieving
22
+ a power consumption range from 1.7 µW-20 mW. Multiple ML
23
+ workloads aimed for diverse applications are mapped on the SoC
24
+ to showcase its flexibility and efficiency. All the models achieve
25
+ 1-2 TOPS/W of energy efficiency with power consumption below
26
+ 230 µW in continuous operation. In a duty-cycling use case for
27
+ machine monitoring, this power is reduced to below 10 µW.
28
+ Index Terms—Extreme edge, tinyML, machine learning accel-
29
+ erators, ultra-low power, system-on-chip.
30
+ I. INTRODUCTION
31
+ E
32
+ Xtreme edge devices [1] or Internet-of-Things (IoT)
33
+ nodes mostly perform non-vision tasks and can achieve
34
+ good accuracy, even with small and lightweight neural network
35
+ (NN) models [2]. This is in contrast to more traditional tasks
36
+ designed for processing image data and contain millions to
37
+ billions of parameters and operations with high hardware re-
38
+ source demands. Consider the Google voice assistant as an ex-
39
+ ample, which needs only 14 kilo bytes (kB) of NN parameters
40
+ to run a keyword-spotting application on edge devices [3]. The
41
+ insight that not all applications require maximum accuracy,
42
+ large and complex NN models, has resulted in a new paradigm
43
+ of ML application development, called tinyML or ML at the
44
+ extreme edge [4]. This trend, at its core, has been driven by the
45
+ V. Jain, L. Mei, and M. Verhelst are with the Department of Electrical
46
+ Engineering - MICAS, KU Leuven, Belgium.
47
+ S. Giraldo was with the Department of Electrical Engineering - MICAS,
48
+ KU Leuven, Belgium. He is now with B12 Consulting, Belgium.
49
+ J. De Roose and B. Boons were with the Department of Electrical
50
+ Engineering - MICAS, KU Leuven, Belgium. They are now with Magics
51
+ Technologies, Belgium.
52
+ © 2023 IEEE. Personal use of this material is permitted. Permission from
53
+ IEEE must be obtained for all other uses, in any current or future media,
54
+ including reprinting/republishing this material for advertising or promotional
55
+ purposes, creating new collective works, for resale or redistribution to servers
56
+ or lists, or reuse of any copyrighted component of this work in other works.
57
+ requirements imposed by battery-operated, performance- and
58
+ power-constrained IoT nodes. Most IoT sensor nodes consist
59
+ of a microcontroller unit (MCU) with a subset of sensors, a
60
+ memory for storing acquired data, a CPU and a wireless data
61
+ transceiver. The presence of these MCUs for data collection
62
+ provides opportunities to process data very close to the sensor
63
+ when the NN model is small, and avoids the high penalty of
64
+ raw data transmission to more powerful edge or cloud units.
65
+ Yet, this local ML processing, brings several new chal-
66
+ lenges: 1.) As these nodes are battery-operated, the system is
67
+ typically severely power or energy constrained requiring ultra-
68
+ low power operation, with the ability to idle. 2.) the MCU,
69
+ moreover, has limited compute power and memory space,
70
+ resulting in a critical trade-off between model size, execution
71
+ performance and hardware complexity; 3.) despite the need
72
+ for efficiency, the system should also be flexible enough
73
+ to support different classes of NN models across different
74
+ applications, and 4.) it should have a small footprint. Several
75
+ hardware for ML have been proposed in the recent literature
76
+ and can be divided into three main categories: 1) extremely
77
+ specialized edgeML accelerators designed for ultra-low power
78
+ operation with little to no flexibility at low performance [5]–
79
+ [8], 2) multi-modal edgeML accelerators providing medium
80
+ level of flexibility with high performance at medium to high
81
+ power consumption [9]–[13], and, 3) commercial-off-the-shelf
82
+ (COTS) MCUs delivering higher flexibility but at low perfor-
83
+ mance and medium power consumption [14]–[16]. Most of
84
+ these hardware designs do not meet all the requirements of an
85
+ extreme edge device. An exception is Vega [17] which presents
86
+ a complete SoC, however, the specialized accelerator of Vega
87
+ does not have the flexibility to handle all DNN workloads.
88
+ Thus, a new class of flexible ultra-low power (ULP) platforms
89
+ towards extreme edge deployment is needed.
90
+ In this context, this work presents TinyVers [18], a highly
91
+ adaptive SoC platform which significantly enhances the trade-
92
+ off between energy efficiency and flexibility needed in extreme
93
+ edge devices, through the use of: A.) a RISC-V proces-
94
+ sor extended with a flexible ML accelerator (FlexML) with
95
+ dataflow reconfiguration supporting diverse ML workloads and
96
+ support for efficient zero-skipping in block structured sparsity
97
+ and deconvolution; B.) an embedded magnetoresistive random
98
+ access memory (eMRAM) for non-volatile storage enabling
99
+ standalone operation with efficient power-down (or idling);
100
+ C.) a programmable wake-up controller (WuC) supporting
101
+ different power-on and idle modes to enable both always-on
102
+ inference as well as on-demand and duty-cycled smart sensing
103
+ arXiv:2301.03537v1 [cs.AR] 9 Jan 2023
104
+
105
+ 2
106
+ and computation used in typical tinyML IoT applications. The
107
+ SoC provides users flexibility not only in mapping diverse
108
+ ML workloads for diverse tinyML applications, but also in
109
+ supporting various use cases such as duty-cycling and smart
110
+ sensing. We demonstrate TinyVers’ capabilities and improve-
111
+ ments over state-of-the-art (SotA) on diverse applications in
112
+ machine monitoring, anomaly detection, audio signal analysis,
113
+ and image classification through the use of both deep learning
114
+ as well as traditional ML workloads.
115
+ The rest of the paper is organized as follows. The basics of
116
+ ML compute kernels is introduced in Section II. Section III
117
+ discusses the architecture overview of TinyVers, followed by
118
+ Section IV providing further details of the FlexML accelerator.
119
+ Section V provides details on how the software stack for
120
+ ML deployment on TinyVers is undertaken. Subsequently,
121
+ Section VI presents the experimental results of mapping
122
+ different workloads and application use cases. Finally, Sec-
123
+ tion VII compares TinyVers’ performance with related works
124
+ and Section VIII concludes the paper.
125
+ II. ALGORITHMIC BACKGROUND
126
+ ML applications heavily exploit deep neural networks
127
+ (DNN) with traditional convolutional (CNN) and fully con-
128
+ nected (FC) layers. However, a plethora of new NN layer
129
+ topologies are emerging. Some examples of these are the use
130
+ of temporal convolutional networks (TCN) used in audio tasks
131
+ like keyword spotting [19]–[21], or auto-encoders (AE) using
132
+ convolution and deconvolution pairs in machine monitoring
133
+ and anomaly detection tasks [22]–[24]. Morever, also machine
134
+ learning models not relying on neural network layers are still
135
+ used in extreme edge IoT nodes, such as support vector ma-
136
+ chines (SVM) [25] used in novelty and anomaly detection ap-
137
+ plications. The execution efficiency of all these workloads can
138
+ can be improved with orders of magnitude when deployed on
139
+ specialized accelerators. Yet, the wide variety in the compute
140
+ kernels of interest complicates their efficient mapping on a
141
+ single hardware platform. The following subsections deal with
142
+ the different ML operation characteristics, their categorization
143
+ into mathematical operations, and their hardware implications.
144
+ A. Convolution and Dense Operation
145
+ Convolutional and dense layers are the most common com-
146
+ pute kernels used in DNNs and they can be decomposed
147
+ into matrix-matrix multiplication (MMM) and matrix-vector
148
+ multiplication (MVM) resp.. These two matrix operations can
149
+ be represented mathematically as nested for loops as shown in
150
+ Fig. 1. Most ML compute kernels can be categorized into one
151
+ of these two mathematical operations, with some special layers
152
+ requiring extra hardware changes. One such kernel is the TCN
153
+ layer which can be represented as a 1D CNN and requires extra
154
+ support for programmable dilation which is similar to strides
155
+ in a convolution. Recurrent neural networks (RNN) like long
156
+ short-term memory (LSTM) and gated recurrent unit (GRU)
157
+ can be decomposed to MVM with need for extra hardware
158
+ for activation functions. These hardware changes would be
159
+ discussed further in Section IV.
160
+ C
161
+ C
162
+ IY
163
+ FY
164
+ OY
165
+ OX
166
+ IX
167
+ FX
168
+ K
169
+ *
170
+ K
171
+ Convolution Operation = MMM
172
+ Input FMAP
173
+ Weights
174
+ Output FMAP
175
+ C
176
+ C
177
+ *
178
+ K
179
+ Dense Operation = MVM
180
+ Input FMAP
181
+ Weights
182
+ Output FMAP
183
+ TCN
184
+ CNN
185
+ GAN
186
+ AE
187
+ LSTM
188
+ FC
189
+ SVM
190
+ K
191
+ for(y=0 to Y-1); for each output row
192
+ for(x=0 to X/N-1); for each output column
193
+ for(k=0 to K/N-1); for each output channel
194
+ for(c=0 to C-1); for each input channel
195
+ for(fy=0 to Fy-1); for each filter row
196
+ for(fx=0 to Fx-1); for each filter column
197
+ o[k][x][y] += i[c][x+fx][y+fy]*w[k][c][fx][fy]
198
+ for(k=0 to K/N-1); for each output channel
199
+ for(c=0 to C/N-1); for each input channel
200
+ o[k] += i[c]*w[k][c]
201
+ PE
202
+ Spatial Unrolling X
203
+ Temporal
204
+ Unrolling
205
+ Spatial Unrolling Y
206
+ PE
207
+ PE
208
+ PE
209
+ PE
210
+ PE
211
+ PE
212
+ PE
213
+ PE
214
+ PE
215
+ PE
216
+ PE
217
+ PE
218
+ PE
219
+ PE
220
+ PE
221
+ Fig. 1. Different ML models and their mathematical representation in terms
222
+ of MMM and MVM. The nested for loop representation can be mapped onto
223
+ specialized accelerators through spatial and temporal unrolling.
224
+ When mapping MMMs and MVMs on specialized hardware
225
+ accelerators, the nested for loops can be unrolled spatially
226
+ and temporally, which is called dataflow in literature [26].
227
+ On a 2D processing element (PE) array, two for loops can
228
+ be spatially unrolled, i.e., the loops can be parallelized along
229
+ the X and Y dimensions, as shown in Fig. 1. In the rest
230
+ of the paper, this spatial unrolling is represented as (Spatial
231
+ Unrolling X)|(Spatial Unrolling Y). The remaining for loops
232
+ are temporally unrolled, i.e., sequential execution. Depending
233
+ on the available parallelism and available re-usability, the
234
+ spatial unrolling (X and Y) needs to be configurable, to be
235
+ able to efficiently map all workloads, detailed in Section IV-B.
236
+ B. Deconvolution
237
+ Autoencoders used in many machine monitoring applica-
238
+ tions consist of an encoder and a decoder pair, which tries
239
+ to reconstruct the input data. After training on normal data,
240
+ a reconstruction error signals an anomaly in the test data.
241
+ Deconvolution or transposed convolution are used in these
242
+ autoencoders and are built by combining the convolution and
243
+ upsampling into a single operation. Deconvolution can be
244
+ mapped as a convolution (MMM) but needs extra hardware
245
+ to support zero-skipping of input for efficient mapping. Hard-
246
+ ware modification can improve the mapping efficiency of this
247
+ operation, and better exploit its inherent sparsity, as will be
248
+ discussed in Section IV-C.
249
+ C. Support Vector Machines (SVMs)
250
+ SVMs are ML algorithms used for classification and re-
251
+ gression tasks. When classification of input data between
252
+ normal behavior and an anomaly is required, a binary classifier
253
+ called a one-class support vector machine (OC-SVM) can be
254
+
255
+ 3
256
+ used [27], [28]. The decision function of a OC-SVM using the
257
+ radial basis function (RBF) kernel is given by the equation (1).
258
+ For the Laplacian kernel, the L2 norm is replaced by L1 norm.
259
+ f(x) =
260
+ N
261
+
262
+ i=0
263
+ αi · exp
264
+ −∥x−svi∥2
265
+ 2σ2
266
+ − b
267
+ (1)
268
+ where x is the input vector with length D, sv are the support
269
+ vectors with length D, N is the number of support vectors,
270
+ σ the standard deviation, α the Lagrange multiplier, and b the
271
+ bias. The number of support vectors N, in combination with
272
+ the vector length D, can become large in these workloads,
273
+ making the L1 and L2 norm calculation complex, and their
274
+ deployment can gain orders of magnitude in performance
275
+ when deployed on specialized accelerators. The D and N
276
+ dimensions of the norm operations can be treated similar to
277
+ C and K dimensions of a dense layer (MVM) and can be
278
+ spatially unrolled on the PE array. In addition to unrolling
279
+ the norms, extra hardware to support squaring, subtraction,
280
+ rounding and absolute operation needs to be added to each
281
+ PE. The result of the norm calculation can then be used by a
282
+ CPU core to compute the overall kernel.
283
+ D. Structured Sparsity
284
+ Exploiting sparsity in DNNs can help to reduce the com-
285
+ putational complexity and memory requirements, by skipping
286
+ zeros and compressing the NN parameters. However, random
287
+ pruning or unstructured sparsity tends to be hard to efficiently
288
+ map on hardware and requires special logic for zero-skipping
289
+ and load balancing [29]–[31]. The structure of sparsity (gran-
290
+ ularity of pruning) has high impact on hardware efficiency and
291
+ prediction accuracy. Some works have found that unstructured
292
+ sparsity achieves better prediction accuracy than structured
293
+ sparsity but structured sparsity tends to be more hardware
294
+ amenable and improves computational efficiency [30]. Thus, a
295
+ structured sparse model could be trained with more iterations
296
+ to revert back closer to the same prediction accuracy achieving
297
+ similar overall efficiency/cost. Moreover, more coarse-grained
298
+ sparsity can reduce the additional memory requirements im-
299
+ posed for storing indices of non-sparse data.
300
+ With all of these diverse ML workloads and their charac-
301
+ teristics in mind, a platform which can efficiently map all of
302
+ the above, needs to be designed.
303
+ III. TINYVERS HARDWARE ARCHITECTURE
304
+ TinyVers, as shown in Fig. 2, is a heterogeneous SoC
305
+ consisting of a single core RISC-V processor, a flexible ML
306
+ accelerator called FlexML, a 512 kB shared level-2 (L2)
307
+ SRAM memory, a micro-DMA (uDMA) for data movement
308
+ between peripherals/memory, a 512 kB eMRAM for non-
309
+ volatile storage, and a WuC for power management. The SoC
310
+ development is rooted in the PULPissimo platform [32]. It
311
+ embeds a 2 kB read-only memory (ROM), which acts as the
312
+ first stage boot loader (FSBL) and also controls boot from
313
+ JTAG, external SPI flash or the eMRAM. Two communication
314
+ busses are used: 1.) a logarithmic interconnect, which enables
315
+ a tightly-coupled data memory (TCDM) providing single cycle
316
+ eMRAM
317
+ (512 KB)
318
+ ROM
319
+ Shared Memory L2 (512 kB)
320
+ GPIO UART
321
+ SPI
322
+ I2C
323
+ I2S
324
+ CPI
325
+ JTAG
326
+ SCAN
327
+ CHAINS
328
+ eMRAM
329
+ CNTL
330
+ LP Data acq. Memory L2
331
+ (64 kB)
332
+ TCDM interconnect
333
+ uDMA
334
+ DMA
335
+ Source
336
+ Source
337
+ Sink
338
+ RISC-V
339
+ APB
340
+ WuC (RTC
341
+ &
342
+ Power FSM)
343
+ 2D SIMD
344
+ Array
345
+ 8x8
346
+ Weight L1
347
+ Memory
348
+ Instruction
349
+ Memory
350
+ Activation L1
351
+ Memory
352
+ DMA
353
+ Control
354
+ Registers
355
+ Logic PD
356
+ LP Data
357
+ Acq. Mem
358
+ Data Acq.
359
+ Mem PD
360
+ L1 PD
361
+ UDMA
362
+ PD
363
+ AON PD
364
+ MRAM
365
+ PD
366
+ Power
367
+ Modes
368
+ PD= Power Domain
369
+ Boot
370
+ OFF
371
+ OFF
372
+ OFF
373
+ OFF
374
+ OFF
375
+ OFF
376
+ OFF
377
+ OFF
378
+ OFF
379
+ OFF
380
+ OFF
381
+ OFF
382
+ ON/OFF
383
+ OFF
384
+ ON
385
+ ON
386
+ ON
387
+ ON
388
+ ON
389
+ ON
390
+ ON
391
+ ON
392
+ ON
393
+ ON
394
+ ON
395
+ ON
396
+ ON
397
+ ON
398
+ ON
399
+ ON
400
+ ON
401
+ ON
402
+ ON
403
+ ON
404
+ ON
405
+ Active
406
+ Data Acq.
407
+ LP Data Acq.
408
+ Deep Sleep
409
+ % VDD WAKE
410
+ * VDD SCL
411
+ ** VDD SRAM
412
+ ^^ VDD MRAM
413
+ # VCS MRAM
414
+ V+ bias
415
+ V- bias
416
+ ^^
417
+
418
+ #
419
+ %
420
+ %
421
+ Data
422
+ Mover
423
+ FSM
424
+ FlexML Accelerator
425
+ *
426
+ *
427
+ *
428
+ *
429
+ *
430
+ *
431
+ *
432
+ *
433
+ **
434
+ **
435
+ **
436
+ **
437
+ **
438
+ FlexML
439
+ Control
440
+ Unit
441
+ Fig. 2. Overview of the complete TinyVers SoC showing the different power
442
+ domains (PD) with their constituting modules and the power modes supported.
443
+ access to the shared L2, and 2.) the APB standard bus, which
444
+ is used for controlling different memory mapped modules.
445
+ The interface between the SoC and FlexML accelerator is
446
+ based on the HWPE framework presented in [33]. Using the
447
+ streamers from [33], data is moved to-and-from the shared L2
448
+ memory with the help of FlexML’s DMA engine which is a
449
+ FSM controlling the data (un)loading of its private memories
450
+ and double buffering operation. Several peripheral interface
451
+ protocols are supported by the SoC including UART, SPI, I2C,
452
+ I2S, and CPI, in addition to having 32 general purpose IOs
453
+ (GPIO). Separate clocks are used for the main core logic,
454
+ the peripheral interfaces, and the always-on domain which
455
+ includes the WuC and the IO pads.
456
+ A. Smart Sensing Modes for TinyML
457
+ IoT tinyML applications typically operate by collecting data
458
+ across a specified time window through an array of sensors,
459
+ after which the collected data can be processed to make
460
+ decisions. In many applications, the time window across which
461
+ the data needs to be collected before processing can start,
462
+ can vary from a few ms to sec. Moreover, during the sensor
463
+ data collection, many modules of the MCU are not used since
464
+ no heavy processing is done yet. This brings opportunities in
465
+ improving power saving in many tinyML applications: during
466
+ data collection, only the modules necessary for moving the
467
+ windowed data from the sensor peripheral interfaces to the
468
+ memory need to remain active, while e.g. the CPU can be
469
+ put to sleep. Furthermore, in applications which work on
470
+ time series data like audio, the memory requirement for the
471
+ windowed data is small (< 64 kB), such that also a large part
472
+ of the main memory of the MCU can be powered-down to
473
+ avoid leakage power of the unused memory section.
474
+ To this end, TinyVers introduces two tinyML optimized
475
+ data acquisition power modes: 1.) ‘Data acq.’ and 2.) ‘LP
476
+ data acq.’, as shown in Fig. 2. The data acq. mode, targeted
477
+ towards applications with large sample data like vision, keeps
478
+ the uDMA module and the complete shared L2 memory (512
479
+
480
+ 4
481
+ Full Active
482
+ Data Acq
483
+ LP Data Acq
484
+ 0
485
+ 100
486
+ 200
487
+ 300
488
+ 31
489
+ 20
490
+ 8
491
+ 325
492
+ 77
493
+ 10
494
+ 356
495
+ 97
496
+ 18
497
+ Power(µW)
498
+ Dynamic
499
+ Leakage
500
+ Total
501
+ Fig. 3.
502
+ Power simulation of post-synthesis netlist undertaken in Cadence
503
+ Genus tool for the three power modes. In all the three modes, I2S data is
504
+ collected at a sampling frequency of 44.1 kHz for a window of 2 seconds.
505
+ Full active power reported includes configuration of uDMA by RISC-V core
506
+ and interrupt handling procedure, in addition to data collection.
507
+ Power
508
+ uDMA
509
+ Power
510
+ OFF
511
+ Power
512
+ ON
513
+ Switch
514
+ Power 1
515
+ Switch
516
+ Power 2
517
+ Power
518
+ OFF
519
+ Reset
520
+ Isolate
521
+ Clk
522
+ enable
523
+ Power
524
+ ON
525
+ Top level FSM
526
+ Bottom level FSM
527
+ Power
528
+ Logic &
529
+ L1
530
+ Power
531
+ MRAM
532
+ Power
533
+ L2 &
534
+ L2 udma
535
+ Fig. 4. Flow diagram showing the hierarchical FSM used in the WuC.
536
+ kB) powered up. In contrast to that, the LP data acq. mode
537
+ only keeps part of the shared L2 memory (64 kB) powered up,
538
+ in addition to the uDMA. This mode is specifically targeted
539
+ towards applications which needs time series and audio data
540
+ like keyword spotting, machine monitoring, biosignal analysis,
541
+ etc. Fig. 3 shows an estimation of the power saving that can
542
+ be achieved when moving from a full active mode to the
543
+ two tinyML sensing modes, with almost 3.5× improvement
544
+ between the full active and data acq. modes and 5.5× between
545
+ data acq. and LP data acq. modes.
546
+ B. Power Management
547
+ Aggressive power management is pursued in TinyVers on
548
+ top of standard low power design. The SoC is divided into 6
549
+ switchable power domains and 1 always-on domain (AON),
550
+ as shown in Fig. 2. Each switchable power domain consists
551
+ of multiple power gating switches, which isolate the VDD
552
+ of the power domain from the global VDD supply. These
553
+ power gating switches are controlled by control signals driven
554
+ from the WuC of the AON domain. All interconnect crossings
555
+ between the power domains are equipped with bidirectional
556
+ level shifters and isolation cells, such that the individual supply
557
+ voltages of the domains can be controlled independently.
558
+ The smart WuC is in charge of this power management
559
+ control, relying on a real-time counter (RTC). The counter
560
+ can be programmed by the RISC-V core with millisecond
561
+ granularity. The RISC-V core can instruct the WuC to bring
562
+ the SoC into one of the five supported power modes shown in
563
+ Fig. 2. To this end, the WuC encompasses hierarchical finite-
564
+ state machines (FSM) driven by the RTC, as shown in Fig. 4,
565
+ controlling the power-up and power-down of the complete SoC
566
+ and the different power domains. The top level FSM controls
567
+ the sequence of power-up/down of the different power domains
568
+ and the bottom level FSMs control the fine-grain sequence to
569
+ (de)activate the isolation cells and the power gating switches
570
+ of the individual power domains.
571
+ Emerging memories like ReRAM, MRAM, FeRAM, PCM,
572
+ etc. [34], [35], have shown promise in building cost-effective
573
+ embedded non-volatile memories (NVM) targeting applica-
574
+ tions in edge computing for automotive or industry 4.0. NVM
575
+ memories can be used as the storage space for boot code
576
+ and other parameters that need to be stored. This enables
577
+ two things: 1.) Duty-cycling can be used as a means of
578
+ reducing power consumption in applications which do not
579
+ require always-on operation; and 2.) the SoC does not need
580
+ to go to a central cloud server in order to fetch its boot codes
581
+ and NN parameters when it is power-cycled. Moreover, the
582
+ availability of the NVM embedded on-chip, avoids the high
583
+ energy cost of fetching data from off-chip.
584
+ MRAM promoted as a universal memory, uses magnetic
585
+ polarity to store data in its bitcells [36]. Being non-volatile
586
+ and almost as dense as traditional SRAM, they are a good fit
587
+ for tinyML applications using extreme edge SoCs. With this
588
+ in mind, TinyVers integrates a 512 kB embedded MRAM on-
589
+ chip, enabling extreme power management strategies for smart
590
+ sensing and on-demand computation. In the SoC, the eMRAM
591
+ acts as a non-volatile storage for the boot code that the RISC-
592
+ V needs to wake-up and start processing, and can also store the
593
+ NN parameters of the mapped ML workloads. The eMRAM
594
+ can, finally, also be used as a non-volatile scratchpad space
595
+ for storing windowed data in smart sensing applications. The
596
+ interface between eMRAM and the shared L2 memory uses
597
+ the uDMA unit and the design is based on the work of [17].
598
+ IV. FLEXML ACCELERATOR
599
+ This section firstly describes the architecture overview of the
600
+ FlexML accelerator, followed by the dataflow reconfiguration
601
+ used for flexible mapping, efficient zero-skipping used for
602
+ deconvolution and structured sparsity, and finally the hardware
603
+ for supporting SVM, as briefly discussed in Section II.
604
+ A. FlexML Architecture Overview
605
+ The FlexML accelerator is TinyVers’ specialized, versatile
606
+ hardware accelerator. FlexML is designed to efficiently support
607
+ the large diversity in ML workloads for tinyML applications,
608
+ while exploiting the data reuse present in individual layer
609
+ characteristics. This is achieved through a zero-latency runtime
610
+ dataflow reconfiguration, discussed in Section IV-B. As shown
611
+ in Fig. 5, FlexML encompasses an 8×8 single instruction
612
+ multiple data (SIMD) array of processing elements (PE),
613
+ wherein each processing element consists of a precision-
614
+ scalable multiply-accumulate (MAC) unit with support for INT
615
+ 8/4/2 [37], shown in Fig. 6. As a result of the precision-
616
+ scalability, the SIMD array can be reconfigured to be a
617
+ 8×8/16/32 array of INT8/4/2 MAC units, resp.. Each PE per-
618
+ forms 1/2/4 MAC operations per cycle based on the selected
619
+ precision (INT8/4/2) and the results are accumulated in a 32-
620
+ bit register with full/partial output stationarity, reducing the
621
+ movement cost of the large bit-width partial sums. The final
622
+ output is passed through a ReLU function (if enabled), fol-
623
+ lowed by re-quantization to the selected precision and written
624
+
625
+ 5
626
+ DMA Engine
627
+ Inst.
628
+ Mem
629
+ Cntl
630
+ FSM
631
+ Sparsity
632
+ Mem
633
+ 2x2 kB
634
+ Weight
635
+ Mem (L1)
636
+ 2x32 kB
637
+ Adder Trees
638
+ Act
639
+ Mem (L1)
640
+ 2x32 kB
641
+ NLFG
642
+ &
643
+ Max
644
+ Pool
645
+ Input FIFO (L0)
646
+ SIMD PE Array 8x8
647
+ IX
648
+ Layer Type
649
+ ucode
650
+ Inst.
651
+ K
652
+ Fx
653
+ Fy
654
+ Input
655
+ pointer
656
+ Weight
657
+ Pointer
658
+ .........
659
+ IY
660
+ C
661
+ PE
662
+ PE
663
+ PE
664
+ PE
665
+ PE
666
+ PE
667
+ PE
668
+ PE
669
+ PE
670
+ PE
671
+ PE
672
+ PE
673
+ PE
674
+ PE
675
+ PE
676
+ PE
677
+ PE
678
+ PE
679
+ PE
680
+ PE
681
+ Fig. 5. FlexML accelerator architecture overview with ucode instruction.
682
+ *
683
+ >>
684
+ ABS
685
+ REG
686
+ REG
687
+ Round
688
+ Sub
689
+ ReLU
690
+ Overflow
691
+ Control
692
+ Input
693
+ Activation
694
+ Output
695
+ Activation
696
+ 1
697
+ 0
698
+ 0
699
+ 0
700
+ Input
701
+ Weight
702
+ From Neighbor
703
+ PE
704
+ -
705
+ +
706
+ 8b
707
+ 20b
708
+ 8b
709
+ 16b
710
+
711
+ … …
712
+
713
+ … …
714
+ unused
715
+ 4b
716
+ 4b
717
+ Gated
718
+ 4b
719
+ 4b
720
+ Gated
721
+ 12b
722
+ 9b
723
+ 2b 2b 2b
724
+
725
+ … …
726
+
727
+ … …
728
+ Gated
729
+ 2b
730
+ Gated
731
+ 2b
732
+ 2b
733
+ 2b
734
+ 2b
735
+ 8b
736
+ 6b
737
+ Fig. 6.
738
+ Block diagram of the processing elements used in the flexML
739
+ accelerator, showing the precision-scalable MAC unit and the additional
740
+ hardware to support SVM.
741
+ back to the activation L1. Mixed precision quantization can
742
+ help in improving performance of DNN models when moving
743
+ below 8 bits precision. However, the hardware overhead of
744
+ mixed precision can reduce the overall efficiency of PEs
745
+ due to varying bandwidth and serialized dataflow [38]. Thus,
746
+ FlexML only supports symmetric precision for its weights and
747
+ activation. In addition, a simple shift and ReLU is used for
748
+ normalization of output, which also keeps hardware overhead
749
+ low. In order to maintain accuracy of the models, a hardware
750
+ aware training framework, mentioned in Section V, is used.
751
+ Supporting the SIMD PE array, are private level-1 (L1)
752
+ SRAM based memories for storing both weights (64 kB)
753
+ and activations (64 kB). Both the weight L1 and activation
754
+ L1 are composed of two 32 kB banks operating in a ping-
755
+ pong manner to overlap data writing and reading, improving
756
+ the overall performance. An intermediate memory level L0 is
757
+ provided between the activation L1 and the PE array. This
758
+ L0 memory is a FIFO buffer of size 16×8 bits, used to
759
+ improve data locality when doing shifting window operation
760
+ in convolution. Furthermore, a separate non-linear function
761
+ generator (NLFG) and a max pooling unit are provided. The
762
+ for(y=0 to Y-1); for each output row
763
+ for(x=0 to X/8-1); for each output column
764
+ for(k=0 to K/8-1); for each output channel
765
+ for(c=0 to C-1); for each input channel
766
+ for(fy=0 to Fy-1); for each filter row
767
+ for(fx=0 to Fx-1); for each filter column
768
+ parfor(k=0 to 8-1); spatial unrolled output channel
769
+ parfor(x=0 to 8-1); spatial unrolled output column
770
+ o[k][x][y] += i[c][x+fx][y+fy]*w[k][c][fx][fy]
771
+ for(k=0 to K/8-1); for each output channel
772
+ for(c=0 to C/8-1); for each input channel
773
+ parfor(k=0 to 8-1); spatial unrolled output channel
774
+ parfor(c=0 to 8-1); spatial unrolled input channel
775
+ o[k] += i[c]*w[k][c]
776
+ FIFO
777
+ PE
778
+ PE
779
+ PE
780
+ PE
781
+ PE
782
+ PE
783
+ PE
784
+ PE
785
+ PE
786
+ PE
787
+ PE
788
+ PE
789
+ PE
790
+ PE
791
+ PE
792
+ PE
793
+ C
794
+ Weight Memory
795
+ FIFO
796
+ MMM
797
+ MVM
798
+ Weight Memory
799
+ OX
800
+ K
801
+ PE
802
+ PE
803
+ PE
804
+ PE
805
+ PE
806
+ PE
807
+ PE
808
+ PE
809
+ PE
810
+ PE
811
+ PE
812
+ PE
813
+ PE
814
+ PE
815
+ PE
816
+ PE
817
+ K
818
+ Bank 0
819
+ Bank 1
820
+ Bank 3
821
+ Bank 0
822
+ Bank 1
823
+ Bank 3
824
+ Bank 7
825
+ Bank 7
826
+ Fig. 7. Diagram showing the dataflow reconfiguration used to switch from
827
+ OX|K dataflow (left) for MMM to C|K dataflow for MVM. The nested for
828
+ loops below show the addition of parfor loops for the spatial unrolling used.
829
+ NLFG uses LUT-based linear approximation to generate the
830
+ various activation functions (other than ReLU) used in NN
831
+ models such as tanh, sigmoid, etc. To control the dataflow
832
+ and control flow inside the accelerator, a control unit with
833
+ FSMs fetches ucode instructions from the instruction memory,
834
+ decodes the instruction and deploys the relevant layer on the
835
+ PE array by updating the control signals and counters that
836
+ track the workload. The ucode instructions are generated by a
837
+ pseudo-compiler built in python (Section V), and consists of
838
+ CISC-like layerwise long instructions with hyperparameters
839
+ and shown in Fig. 5. The control unit is also extended to
840
+ enable support for efficient zero-skipping of activations in the
841
+ case of deconvolution and zero-skipping of pruned weights in
842
+ conjunction with the sparsity index memories (Section IV-C).
843
+ B. Dataflow Reconfiguration
844
+ In order to efficiently map the diverse set of ML workloads,
845
+ runtime dataflow reconfiguration is supported in the FlexML
846
+ accelerator at no latency overhead. The configurability enables
847
+ efficient mapping of both: 1.) MMMs used for CNN, decon-
848
+ volution and TCN, exploiting both input and weight spatial
849
+ data reuse under an OX|K dataflow with output stationarity,
850
+ and 2.) MVMs used for FC, RNNs and norm calculation
851
+ of SVMs with batch size 1, exploiting the available input
852
+ spatial data reuse under a C|K dataflow with partial output
853
+ stationarity. Multiple previous works have proposed dataflow
854
+ reconfiguration in hardware to optimally map different work-
855
+ loads [39]–[41]. However, these works suffer from large hard-
856
+ ware overhead and latency for diverse dataflow support and
857
+ are not suitable for extreme edge devices. This work limits the
858
+ dataflows to two optimal mapping schemes, thereby, keeping
859
+ hardware and power overhead low. Moreover, none of the prior
860
+ works have looked into mapping of TCN, AE, and SVM on
861
+ the same hardware accelerator. Fig. 7 shows the OX|K (left)
862
+ and C|K dataflow (right) and their hardware implementation,
863
+ resp.. In the OX|K dataflow, the spatial unrolling is applied to
864
+ the OX and the K dimension of the nested for loop, allocating
865
+ the unrolled OX dimension along the columns and the unrolled
866
+ K along the rows of the SIMD PE array of dimension 8×8.
867
+
868
+ 6
869
+ Input FIFO
870
+ Input FIFO
871
+ Input data from activation L1
872
+ Normal operation
873
+ Deconvolution operation
874
+ Input data from activation L1
875
+ 0
876
+ 0
877
+ 0
878
+ 0
879
+ 0
880
+ 0
881
+ 0
882
+ 0
883
+ Ctrl
884
+ Control Unit
885
+ Fetch instruction and enable
886
+ deconvolution
887
+ Control the demux and muxes
888
+ for deconvolution
889
+ Skip rows and columns with all zeros
890
+ Cycle #0: Enable demux to push data to input FIFO
891
+ Cycle #1: Set Ctrl to 0, data sent to PEs -> a 0 b 0 c 0 d 0
892
+ Cycle #2: Set Ctrl to 1, data sent to PEs -> 0 b 0 c 0 d 0 e,
893
+ Shift 0 into input FIFO
894
+ Cycle #3: Set Ctrl to 0, data sent to PEs -> b 0 c 0 d 0 e 0
895
+ IX
896
+ Input Activation
897
+ Filter
898
+ Deconvolution layer in software
899
+ *Orange represents pruned pixels
900
+ IY
901
+ Fig. 8. Representation of deconvolution layer in software (top left), control
902
+ unit running the zero-skip operation (bottom left), the architectural change
903
+ required on the L0 FIFO to support deconvolution (top right), and cycle by
904
+ cycle operation of the FIFO and PEs (bottom right).
905
+ The rest of the for loops are temporally unrolled as shown
906
+ in the nested for loops in Fig. 7, resulting in an output
907
+ stationary dataflow. Under this dataflow regime, the activation
908
+ L1 memory multicasts input activation data in the vertical
909
+ dimension to the L0 FIFO memory, which fetches 8 words
910
+ in the first cycle followed by single word during the shifting
911
+ window operation, thereby, reducing the memory bandwidth
912
+ and number of memory fetches by utilizing the reuse oppor-
913
+ tunity. The weight L1 memory provides data in the horizontal
914
+ dimension, providing 8 words using 2 internal banks, where
915
+ each word is multi-cast along the row. Due to the output
916
+ stationarity, accumulation continues till the final output is
917
+ generated which are then systolically shifted out vertically to
918
+ the activation L1, requiring 8 cycles to complete the output
919
+ write-back. The input data shifting inside the L0 FIFO is made
920
+ programmable to support the variable dilation used in TCNs
921
+ or variable strides in general.
922
+ The alternative C|K dataflow is used for MVM, as this
923
+ workload cannot utilize the OX|K dataflow efficiently due
924
+ to lack of re-usability of weights. Under this dataflow, the
925
+ C dimension is spatially unrolled along the vertical column
926
+ dimension and the K dimension along the horizontal row
927
+ dimension. The activation L1 memory multicasts 8 words of
928
+ input activation along the vertical dimension, bypassing the
929
+ L0 FIFO memory. With a batch size of 1, no weight reuse
930
+ is available and, thus, each PE needs a new weight every
931
+ cycle. In order to meet this requirement, the weight memory
932
+ utilizes all of its 8 banks to unicast 64 different weight words
933
+ to the PEs. PE rows operate on different input channels (C) of
934
+ the same output channel (K). Hence, once the required MAC
935
+ operations per PE are done, the outputs of PEs of the same
936
+ row are accumulated using an adder tree and one final output
937
+ per row is shifted out to the activation memory.
938
+ C. Efficient Zero-skipping for Deconvolution and Blockwise
939
+ Structured Sparsity
940
+ The FlexML accelerator supports efficient zero-skipping of
941
+ deconvolution workloads. As shown in Fig. 8, the input FIFO
942
+ Sparsity Index Mem
943
+ storing the sparse nature
944
+ Sparse
945
+ block
946
+ 1
947
+ 0101
948
+ 0000
949
+ 0000
950
+ 3
951
+ C
952
+ 0
953
+ 1010
954
+ 2
955
+ C
956
+ C
957
+ K
958
+ *
959
+ K
960
+ x8
961
+ K
962
+ 8
963
+ 8
964
+ Blockwise Str. Sparsity for CNN
965
+ Input
966
+ Weight Matrix
967
+ Weights
968
+ Blockwise Str. Sparsity for FC/RNN
969
+ Output
970
+ Control Unit
971
+ Fetch sparsity index for block 1 to 8 from sparsity memory
972
+ Check bit wise, if one present then update counters of
973
+ control FSM to skip current C
974
+ Fetch next blockwise index and repeat
975
+ *Orange represents pruned pixels
976
+ Fig. 9. Blockwise structured sparsity applied to CNN and dense layers (top),
977
+ control unit operation in tandem with sparsity index memory to support zero-
978
+ skipping (bottom).
979
+ is designed such that when in deconvolution mode, it only
980
+ fetches one set of words and shuffles it with zero padding. The
981
+ control unit skips the rows and columns with zeros that would
982
+ result in redundant computation, resulting in a performance
983
+ gain of up to 2× compared to running deconvolution in
984
+ convolution mode with upsampling.
985
+ TinyVers also supports structured sparsity, more specifically,
986
+ blockwise kernel-level sparsity (2D) for both convolutional
987
+ and dense layers [29], [31]. In this scheme, shown in Fig. 9,
988
+ complete input channels of the filter kernels are pruned with a
989
+ constraint that a block size of 8 filter kernels (K = 8) should
990
+ share the same pruning. The block size is decided by the
991
+ dimension of the PE array and the spatial unrolling of K along
992
+ the horizontal dimension of the 2D PE array. In our case, the
993
+ selected block size makes controlling the dataflow and control
994
+ flow easier. Applying the same channel pruning to all the 8
995
+ filter kernels mapped in parallel on the PE array makes the
996
+ mapping efficiency higher as all the rows can still operate with
997
+ a common control logic, and enables not only energy savings,
998
+ but also throughput benefits. For this, the FlexML accelerator
999
+ consists of specialized sparsity index memories which store the
1000
+ bit encoded indices of the pruned channel groups. Fig. 9 shows
1001
+ the sparsity index memory and the control flow logic used in
1002
+ the control unit. Before every filter kernel block increment, the
1003
+ control unit fetches an index memory word and checks the data
1004
+ bit-by-bit for sparsity state, as the input channels increment.
1005
+ If a sparse channel is detected, the complete computation of
1006
+ the channel is skipped, thus, avoiding any zero computation.
1007
+ D. Support Vector Machine
1008
+ The L1 and L2 norm of OC-SVM requires modification
1009
+ of the PEs in order to use the same hardware for mapping
1010
+ the workload. As shown in Fig, 6, each PE is extended with
1011
+ a subtraction block, absolute unit, rounding unit, and the
1012
+ modification of the multiplier to also enable squaring for the
1013
+ norm calculation within the PE array. The input data vector x
1014
+ and the support vector svi are of dimension D and the number
1015
+ of support vectors is N. When used in the C|K dataflow, the
1016
+
1017
+ 7
1018
+ 1.00E-01
1019
+ L1 MEMORY
1020
+ 2.5 mm
1021
+ 2.5 mm
1022
+ L2
1023
+ MEM
1024
+ RISC-V
1025
+ &
1026
+ ACCEL
1027
+ uDMA
1028
+ eMRAM
1029
+ WuC
1030
+ Fig. 10. Measurement setup and chip microphotograph.
1031
+ D dimension of the input data vector of x is unrolled and
1032
+ multicasted vertically (C) along the PE array, while the N
1033
+ dimension of the support vector svi are unrolled and unicasted
1034
+ horizontally (K). The results of the N norm calculations,
1035
+ computed in the PEs, are then sent to the shared L2 memory
1036
+ where it is then post-processed by the RISC-V core with the
1037
+ GNU C in-built exponential function, multiplication with α
1038
+ and summation over N to generate the final output shown in
1039
+ equation (1).
1040
+ V. DEPLOYMENT OF NEURAL NETWORKS ON TINYVERS
1041
+ Hardware used for ML applications also requires a user
1042
+ programmable full stack that can translate ML algorithms
1043
+ directly from existing ML training and inference frameworks
1044
+ like Tensorflow, Keras, PyTorch, etc. This makes the quick and
1045
+ easy deployment of various ML workloads onto an existing
1046
+ hardware possible. A python based pseudo-compiler frame-
1047
+ work created for TinyVers taking into account its heterogeneity
1048
+ is created. An ML algorithm is first quantized to selected
1049
+ precision using the QKeras framework [42] for quantized-
1050
+ aware training. The quantization-aware training framework
1051
+ takes into consideration the hardware constraints such as
1052
+ symmetric quantization and the shift based scaling of output
1053
+ in the PEs of the accelerator. The quantized model is then
1054
+ passed to a python-based NN compilation which takes in the
1055
+ hardware description and provides a set of C-based header
1056
+ files for the RISC-V core, consisting of ucode instructions for
1057
+ the accelerator, NN parameters and also a golden model for
1058
+ verification of the mapped workload.
1059
+ VI. CHIP IMPLEMENTATION AND MEASUREMENT
1060
+ The TinyVers chip microphotograph shown in Fig. 10 was
1061
+ implemented and fabricated in GlobalFoundries 22FDXTM.
1062
+ The figure shows the different sub-modules used in the SoC
1063
+ and detailed in previous sections. Fig. 10 also shows the lab
1064
+ setup used for measurements and benchmarking. The follow-
1065
+ ing subsections details the measurements and benchmarking
1066
+ done on the SoC for power, energy efficiency and performance.
1067
+ A. Peak Performance Analysis
1068
+ First, a peak performance analysis is undertaken using a
1069
+ single CNN layer with 32 input channels, 32 output channels
1070
+ and a 3×3 filter kernel. Selection of the used layer for peak
1071
+ @Vdd Mem, Vdd Logic
1072
+ 0.5
1073
+ 1.0
1074
+ 1.5
1075
+ 2.0
1076
+ 3.0
1077
+ 2.5
1078
+ 3
1079
+ 6
1080
+ 9
1081
+ 12
1082
+ 18
1083
+ 15
1084
+ 5
1085
+ Clock Frequency (MHz)
1086
+ Peak energy eff. (TOPS/W)
1087
+ Throughput (GOPS)
1088
+ 10
1089
+ 20
1090
+ 30
1091
+ 40
1092
+ 50
1093
+ 100
1094
+ 120
1095
+ 150
1096
+ @0.5, 0.4V
1097
+ @0.55, 0.5V
1098
+ @0.65, 0.5V
1099
+ @0.65, 0.6V
1100
+ @0.65, 0.6V
1101
+ @0.65, 0.6V
1102
+ @0.8, 0.8V
1103
+ @0.8, 0.8V
1104
+ @0.8, 0.8V
1105
+ 0.586
1106
+ 2.47
1107
+ 2.0
1108
+ 1.9
1109
+ 1.85
1110
+ 1.43
1111
+ 1.44
1112
+ 0.833
1113
+ 0.838
1114
+ 0.863
1115
+ 1.17
1116
+ 2.35
1117
+ 4.69
1118
+ 3.52
1119
+ 5.86
1120
+ 11.7
1121
+ 14.1
1122
+ 17.6
1123
+ Fig. 11. Peak performance analysis of CNN3×3 layer.
1124
+ 5 MHz
1125
+ 10 MHz
1126
+ 20 MHz
1127
+ 30 MHz
1128
+ 40 MHz
1129
+ 50 MHz
1130
+ 100 MHz
1131
+ 120 MHz
1132
+ 150 MHz
1133
+ 0
1134
+ 5,000
1135
+ 10,000
1136
+ 15,000
1137
+ 20,000
1138
+ Power(µW)
1139
+ WuC
1140
+ L2
1141
+ L2uDMA
1142
+ L1
1143
+ Logic
1144
+ DMA
1145
+ Mram(P)
1146
+ Mram(A)
1147
+ Fig. 12. Power breakdown of the peak perf. analysis with CNN3×3. MRAM
1148
+ power consumption is negligible as it is OFF in active mode. MRAM(A) and
1149
+ MRAM(P) represents MRAM array and MRAM periphery resp..
1150
+ performance is driven by the fact that convolutional layers
1151
+ with a 3×3 filter kernel are the most commonly used layer
1152
+ in modern DNN models. The hyperparameter selection of the
1153
+ CNN layer is driven by the constraint of maximum utilization
1154
+ of the PE array and the size of the private L1 memories
1155
+ of the accelerator. The 8 bit quantized activation and non-
1156
+ sparse (structured) weights of the CNN are generated using
1157
+ the compiler framework using the Google speech dataset for
1158
+ keyword spotting [43] and verified against the golden model
1159
+ for functional correctness.
1160
+ Fig. 11 plots the peak energy efficiency and the throughput
1161
+ with respect to the clock frequency while sweeping the voltage
1162
+ supply of the logic and memories for the benchmarked CNN
1163
+ layer. For fair comparison with other SotA chips, no body
1164
+ biasing is applied. Fig. 12 shows the power breakdown of
1165
+ individual modules when running the benchmarking layer. The
1166
+ SoC shows a large flexibility in delivered performance ranging
1167
+ from high energy efficiency/low throughput of 2.5 TOPS/W,
1168
+ 586 MOPS when operating at a clock frequency of 5 MHz
1169
+ with 0.4 V logic, 0.5 V memories, to low energy efficiency
1170
+ / high throughput of 0.8 TOPS/W, 17.6 GOPS operating at
1171
+ 150 MHz with 0.8 V logic and memories. This provides a
1172
+ large range for extreme edge tinyML applications to operate,
1173
+ trading-off between speed and energy efficiency.
1174
+ B. Workload Benchmarks
1175
+ Using the peak energy efficiency operating point (5 MHz,
1176
+ 0.4 V logic and 0.5 V memory) from Section VI-A, further
1177
+ performance analysis of different synthetic and actual real-
1178
+ time benchmarks are evaluated. Table I shows the SoCs
1179
+ flexibility through mapping of different ML layers and full
1180
+
1181
+ MICAS
1182
+ naikraveraels
1183
+ ADIGILENT
1184
+
1185
+
1186
+ K2_VDD_L1K2_0D_L
1187
+ ZedBoardLens: E20:X80
1188
+ 2022/02/038
1189
+ TABLE I
1190
+ WORKLOAD BENCHMARKS
1191
+ Workload
1192
+ Acc.
1193
+ Power
1194
+ (µW)
1195
+ Peak
1196
+ perf.
1197
+ (GOPS)
1198
+ Peak
1199
+ (effective NZ)
1200
+ energy eff.
1201
+ (TOPS/W)
1202
+ Synthetic
1203
+ CNN@8b
1204
+ -
1205
+ 237
1206
+ 0.586
1207
+ 2.47(2.47)
1208
+ CNN@4b
1209
+ -
1210
+ 197
1211
+ 1.17
1212
+ 5.94(5.94)
1213
+ CNN@2b
1214
+ -
1215
+ 197
1216
+ 2.35
1217
+ 11.9(11.9)
1218
+ CNN@8b,
1219
+ -
1220
+ 239
1221
+ 1.03
1222
+ 4.31(2.46)
1223
+ 50% sparse
1224
+ CNN@8b,
1225
+ -
1226
+ 212
1227
+ 3.64
1228
+ 17.1(2.76)
1229
+ 87.5% sparse
1230
+ FC/RNN/SVM,
1231
+ -
1232
+ 140
1233
+ 0.116
1234
+ 0.829(0.829)
1235
+ batch=16
1236
+ Deconv@8b
1237
+ -
1238
+ 235
1239
+ 1.36
1240
+ 5.78(2.49)
1241
+ Real-time
1242
+ TCN (KWS)
1243
+ 93.3%∗
1244
+ 193
1245
+ 0.204
1246
+ 1.05(1.05)
1247
+ CAE
1248
+ -
1249
+ 209
1250
+ 0.442
1251
+ 2.11(1.27)
1252
+ ResNet-8
1253
+ 82%+
1254
+ 228
1255
+ 0.267
1256
+ 1.17(1.17)
1257
+ OC-SVM
1258
+ -
1259
+ 129
1260
+ 0.126
1261
+ 0.972(0.972)
1262
+ ∗ 12-class task, baseline=93.46%, + baseline=85%
1263
+ 2%
1264
+ ResNet8
1265
+ OC-SVM
1266
+ CAE
1267
+ TCN
1268
+ 1%
1269
+ 31%
1270
+ 2%
1271
+ 21%
1272
+ 41%
1273
+ 4%
1274
+ 0%
1275
+ 29%
1276
+ 2%
1277
+ 19%
1278
+ 44%
1279
+ 6%
1280
+ WuC
1281
+ L2
1282
+ L2uDMA
1283
+ L1
1284
+ Logic
1285
+ DMA
1286
+ Mram(P)
1287
+ Mram(A)
1288
+ 0%
1289
+ 31%
1290
+ 18%
1291
+ 44%
1292
+ 5%
1293
+ 1%
1294
+ 47%
1295
+ 3%
1296
+ 15%
1297
+ 25%
1298
+ 9%
1299
+ Power: 129 μW,
1300
+ Latency: 4.3ms
1301
+ Power: 228 μW,
1302
+ Latency: 76ms
1303
+ Power: 193 μW,
1304
+ Latency: 11ms
1305
+ Power: 209 μW,
1306
+ Latency: 30ms
1307
+ Fig. 13. Energy breakdown showing the distribution of measured energy of the
1308
+ chip modules for running a single inference of the four real-time workloads
1309
+ on FlexML and RISC-V with input data already available in L2 memory.
1310
+ The power and latency measurements starts from setting up of accelerator
1311
+ parameters by RISC-V, data movement from L2 to L1, inference computations,
1312
+ and ends with post processing by RISC-V core. MRAM power consumption
1313
+ is negligible as it is OFF in active mode.
1314
+ workloads. The CNN layer from Section VI-A is extended and
1315
+ measured with different precision and blockwise structured
1316
+ sparsity (BSS) levels. When moving to lower precision of INT-
1317
+ 4 and INT-2, the peak throughput improves by 2× and 4×
1318
+ while the peak energy efficiency improves by 2.4× and 4.8×
1319
+ resp., achieving a maximum of 11.9 TOPS/W at INT-2. As
1320
+ shown in Table I, at 8 bit precision with 50% BSS (16/32
1321
+ input channels pruned) the performance improves by around
1322
+ 1.7× while at 87.5% BSS (28/32 input channels pruned)
1323
+ the performance increases by approximately 6.9×. Further
1324
+ performance improvement can be gained when moving to
1325
+ lower precision, however, low precision combined with high
1326
+ BSS levels can cause a large drop in accuracy and, thus, is not
1327
+ explored in this benchmarking. Other synthetic benchmarks
1328
+ such as FC, RNN, SVM and a deconvolutional layer similar
1329
+ to the CNN layer in terms of hyperparameters are explored
1330
+ and the results are shown in the table. For the dense layers,
1331
+ batching of 16 is used.
1332
+ Finally, 4 real-time application benchmarks are used to
1333
+ TABLE II
1334
+ MEASUREMENT RESULTS OF DIFFERENT LOW POWER MODES.
1335
+ Power Mode
1336
+ AON
1337
+ Freq.
1338
+ (kHz)
1339
+ Core
1340
+ Freq.
1341
+ (MHz)
1342
+ Power
1343
+ (µW)
1344
+ Wakeup
1345
+ Latency
1346
+ (µs)
1347
+ Deep Sleep
1348
+ 33
1349
+ -
1350
+ 1.7
1351
+ 788
1352
+ LP Data acq.∗
1353
+ 33
1354
+ 5
1355
+ 23.6
1356
+ 788
1357
+ Data acq.∗
1358
+ 33
1359
+ 5
1360
+ 67
1361
+ 788
1362
+ ∗ @Fs=44.1 kHz
1363
+ Wake-up latency (s)
1364
+ 4
1365
+ 8
1366
+ 12
1367
+ 16
1368
+ 24
1369
+ 20
1370
+ 0.033
1371
+ Clock Frequency (MHz)
1372
+ Power (μW)
1373
+ 1
1374
+ 5
1375
+ 10
1376
+ 788 μs
1377
+ 26 μs
1378
+ 5.2 μs
1379
+ 2.6 μs
1380
+ 20
1381
+ 40
1382
+ 1.3 μs 650 ns
1383
+ 1.7 μW 2.1 μW
1384
+ 5.8 μW
1385
+ 7.8 μW
1386
+ 12.7 μW
1387
+ 22.8 μW
1388
+ Fig. 14. Deep sleep power-latency-frequency tradeoff.
1389
+ show the capabilities of the SoC: 1.) keyword spotting (KWS)
1390
+ using TCN model [21], [44] on google speech dataset, 2.)
1391
+ continuous machine monitoring with a convolutional auto-
1392
+ encoder (CAE) [24] on MIMII dataset [45], 3.) ResNet-8
1393
+ image classification on CIFAR-10 used in MLPerfTM tiny
1394
+ benchmark [46], and 4.) Novelty detection with OC-SVM [47].
1395
+ Table I shows the peak performance characteristics of these
1396
+ benchmarks on the SoC, more specifically the RISC-V core
1397
+ and FlexML, with 8-bit precision, a single inference, and
1398
+ assuming all input data is available in the shared L2 memory.
1399
+ For TCN and ResNet-8, hardware-aware quantization was used
1400
+ and the energy and performance metrics were measured, while
1401
+ for the CAE and OC-SVM workloads, random inputs and
1402
+ weights were used. All the 4 workloads can be deployed with
1403
+ less than 230 µW of continuous real-time power at peak energy
1404
+ efficiency between 1-2 TOPS/W. This means that the SoC can
1405
+ provide high level of flexibility in workload mapping at sub-
1406
+ mW power to enable truly power efficient tinyML application
1407
+ on extreme edge devices. Fig. 13 shows the power breakdown
1408
+ of the 4 real-time workloads. For OC-SVM (dense operation),
1409
+ the power consumption of memory dominates, due to the lack
1410
+ of re-usability of weights leading to more data fetches. On the
1411
+ other hand, power breakdown of CNN based workloads (TCN,
1412
+ ResNet8 and CAE) shows equal distribution between memory
1413
+ and logic as the dataflow exploits maximum re-usability.
1414
+ C. Power Management
1415
+ Table II shows the measured real-time power of the different
1416
+ low power modes of the SoC detailed in Section III-B. In deep
1417
+ sleep mode the SoC operates with an AON clock frequency
1418
+ of 33 kHz. In this mode, only the AON domain consisting of
1419
+ the WuC and the logic controlling the IO pads stays powered
1420
+
1421
+ 9
1422
+ 1.00E-06
1423
+ 1.00E-05
1424
+ 1.00E-04
1425
+ 1.00E-03
1426
+ 1.00E-02
1427
+ 1.00E-01
1428
+ Power (W)
1429
+ Time (ms)
1430
+ 0
1431
+ 280
1432
+ 140
1433
+ Erase followed by write output
1434
+ to MRAM
1435
+ TCN processing (16 batch)
1436
+ Boot from MRAM
1437
+ I2S LP data acq. (2s window)
1438
+ Deep sleep
1439
+ Vdd SCL, Mem: 0.55 V
1440
+ Vdd AON: 0.7 V
1441
+ Core Freq. : 5 MHz
1442
+ 2000 2140 2280
1443
+ Fig. 15.
1444
+ Instantaneous power trace showing the KWS application scenario
1445
+ with one full period of smart sensing and TCN processing followed by idling.
1446
+ ON. The resulting deep sleep power measured is 1.7 µW when
1447
+ operating at 0.7 V voltage supply. When compared to the peak
1448
+ power measured for the CNN layer, the deep sleep power is
1449
+ 12,000× lower. The measure latency of waking up the SoC
1450
+ from deep sleep mode to active mode is 788 µs. This wake-
1451
+ up latency can be traded off to deep sleep power by sweeping
1452
+ the AON clock frequency. Fig. 14 plots the this trade-off for
1453
+ the measured power and wake-up latency when sweeping the
1454
+ AON clock frequency. Applications that need low latency can
1455
+ operate the AON clock at 40 MHz to attain a wake-up latency
1456
+ of 650 ns at a real-time power of 22.8 µW.
1457
+ Table II also shows the measured power for the two tinyML
1458
+ optimized power modes of data acq. and LP data acq. These
1459
+ power modes are measured with an I2S protocol based win-
1460
+ dowed test vector collection with the AON clock frequency at
1461
+ 33 kHz and the core and peripheral clock frequency at 5 MHz.
1462
+ The SoC is programmed to collect I2S audio data through its
1463
+ uDMA at a sampling frequency of 44.1 kHz and a sampling
1464
+ window of 2 second. The sampling clock is generated by the
1465
+ SoC using the 5 MHz clock and lasts for the duration of
1466
+ sampling window. The data acq. or LP data acq. mode is then
1467
+ initiated and power is measured. The measured power for LP
1468
+ data acq. and data acq. is 23.6 µW and 67 µW resp. which is
1469
+ 850× and 300× reduced power consumption compared to the
1470
+ peak power, when the core and peripheral frequencies can be
1471
+ dynamically lowered to 5 MHz.
1472
+ D. Instantaneous Power Trace
1473
+ In order to show the complete end-to-end application de-
1474
+ ployable on the SoC and to show the SoC’s full ML func-
1475
+ tionality, duty cycling and features of power management,
1476
+ two applications are mapped onto the heterogeneous SoC
1477
+ with windowed data collection done in the LP data acq.
1478
+ mode: keyword spotting with a TCN model operating in
1479
+ continuous mode [21]; and a machine monitoring use case with
1480
+ a Mel Frequency Energy Coefficient (MFEC) based feature
1481
+ extraction with a CAE in duty cycled mode [24].
1482
+ 1) Keyword-spotting Application: The first application sce-
1483
+ nario is the keyword-spotting with TCN model. In this ap-
1484
+ plication scenario, audio data from a microphone of window
1485
+ 1.00E-06
1486
+ 1.00E-05
1487
+ 1.00E-04
1488
+ 1.00E-03
1489
+ 1.00E-02
1490
+ 1.00E-01
1491
+ Power (W)
1492
+ MFEC processing on RISC-V
1493
+ Autoencooder processing on FlexML
1494
+ Boot from MRAM
1495
+ I2S LP data acq. (1s window)
1496
+ Deep sleep
1497
+ Time (ms)
1498
+ Vdd SCL, Mem: 0.55 V
1499
+ Vdd AON: 0.7 V
1500
+ Core Freq. : 5 MHz
1501
+ Fig. 16. Instantaneous power trace showing the machine monitoring appli-
1502
+ cation scenario with one period of smart sensing, FE, and CAE processing
1503
+ followed by idling.
1504
+ size 2 seconds (16 batches) at a sampling frequency of 44.1
1505
+ kHz is collected using the I2S peripheral interface protocol,
1506
+ the collected data is simultaneously stored in the special L2
1507
+ uDMA memory using the SoC’s uDMA with the SoC being
1508
+ in the LP data acq. mode. After 2 seconds the SoC wake’s
1509
+ up into active mode and the collected data is processed using
1510
+ the TCN model from Section VI-B. The output of the TCN
1511
+ processing is then stored into the MRAM for future processing
1512
+ or transmission while the SoC can either go into deep sleep
1513
+ mode or collect new windowed sampling data. Fig. 15 shows
1514
+ the complete instantaneous power consumption trace of the
1515
+ KWS application scenario. When operating in this duty-cycled
1516
+ mode, the average power of the complete application is 173
1517
+ µW. The power can be further reduced to 10-20 µW by using
1518
+ the deep sleep power mode of the SoC during periods of no
1519
+ sensing or computation.
1520
+ 2) Machine Monitoring Application: Machine monitoring
1521
+ used for predictive maintenance is the second application
1522
+ scenario selected. In this scenario, I2S peripheral interface
1523
+ protocol is used to collect audio data from a microphone with
1524
+ window size 1 second at a sampling frequency of 16 kHz.
1525
+ The collection of I2S audio data is operated in the LP data
1526
+ acq. mode of the SoC. Once the complete windowed data is
1527
+ collected, the SoC switches to the active mode in which the
1528
+ RISC-V core is used for the MFEC based feature extraction
1529
+ followed by running the CAE on the accelerator. Fig. 16
1530
+ plots the instantaneous power trace of running the machine
1531
+ monitoring application. Unlike the previous application which
1532
+ works on raw audio data, the CAE model need pre-processing
1533
+ MFEC data. As the MFEC algorithm is not supported on
1534
+ the accelerator, it is executed on the RISC-V core with
1535
+ INT16 precision instead of INT32 or FP32 to reduce power
1536
+ consumption [52]. The power trace plots show that running
1537
+ large feature extraction on RISC-V is not energy efficient
1538
+ taking large time to complete owing to single core operation.
1539
+ The average power for continuous operation remains below
1540
+ 164 µW, but for this use case, 9.5 µW is consumed with a
1541
+ duty cycling of 0.05. The MFEC execution on the RISC-V
1542
+
1543
+ 10
1544
+ TABLE III
1545
+ PERFORMANCE COMPARISON WITH STATE-OF-THE-ART.
1546
+ [48]
1547
+ [17]
1548
+ [49]
1549
+ TinyVers
1550
+ [50]
1551
+ [51]
1552
+ Extreme Edge SoCs
1553
+ edgeML Accelerators
1554
+ Technology
1555
+ 28nm FDSOI
1556
+ 22FDX
1557
+ 55nm
1558
+ 22FDX
1559
+ 28nm
1560
+ 65nm
1561
+ Die Area (mm2)
1562
+ 4.5
1563
+ 12
1564
+ 10
1565
+ 6.25
1566
+ 0.55
1567
+ 16
1568
+ Applications
1569
+ IoT GP, DNN,
1570
+ IoT GP, DNN,
1571
+ IoT GP, DNN,
1572
+ IoT GP, DNN+,
1573
+ Always-on KWS
1574
+ DNN
1575
+ NSA
1576
+ NSA
1577
+ NSA
1578
+ Trad. ML, NSA
1579
+ Supported
1580
+ CNN,
1581
+ CNN,
1582
+ CNN,
1583
+ CNN,
1584
+ DSCNN
1585
+ CNN,
1586
+ ML layers
1587
+ FC/RNN
1588
+ FC/RNN
1589
+ FC/RNN
1590
+ FC/RNN, GAN,
1591
+ FC/RNN
1592
+ AE, TCN, SVM
1593
+ Architecture
1594
+ 1×RI5CY+
1595
+ 10×RI5CY+
1596
+ 9×RI5CY
1597
+ 1×RI5CY+
1598
+ DSCNN
1599
+ DNN
1600
+ ML accel.
1601
+ ML accel.
1602
+ FlexML accel.
1603
+ accel.
1604
+ accel.
1605
+ SRAM
1606
+ 464 kB (40 kB)
1607
+ 128 kB(L1)
1608
+ 64 kB (L1)
1609
+ 132 kB (L1)
1610
+ 2 kB
1611
+ 256 kB
1612
+ (State retentive)
1613
+ (16-1600 kB (L2))
1614
+ (512 kB (L2))
1615
+ (64/512 kB (L2))
1616
+ eNVM
1617
+ -
1618
+ 4 MB MRAM
1619
+ -
1620
+ 512 kB MRAM
1621
+ -
1622
+ -
1623
+ Deep sleep power (µW)
1624
+ -
1625
+ 1.7
1626
+ 3.6
1627
+ 1.7
1628
+ -
1629
+ -
1630
+ SRAM ret.
1631
+ 6.4
1632
+ 2.8-123.7
1633
+ 30
1634
+ 23.6-67
1635
+ -
1636
+ -
1637
+ sleep power (µW)
1638
+ Int precision (bits)
1639
+ 8, 16, 32
1640
+ 8, 16, 32
1641
+ 8, 16, 32
1642
+ 2, 4, 8
1643
+ 8
1644
+ 1-16
1645
+ Supply voltage (V)
1646
+ 0.45-0.9
1647
+ 0.5-0.8
1648
+ 1-1.2
1649
+ 0.4-0.9
1650
+ 0.41
1651
+ 0.63-1.1
1652
+ Max frequency (MHz)
1653
+ 350
1654
+ 450
1655
+ 250
1656
+ 150
1657
+ 0.04
1658
+ 200
1659
+ Power range
1660
+ 6.4µW-96mW
1661
+ 1.7µW-49.4mW
1662
+ 3.6µW-75mW
1663
+ 1.7µW-20mW
1664
+ 0.51µW
1665
+ 3.2-297mW
1666
+ Best ML perf.
1667
+ 36 GOPS
1668
+ 32.2 GOPS
1669
+ 12 GOPS
1670
+ 17.6 GOPS
1671
+ 2.3 MOPS+
1672
+ 691.2 GOPS
1673
+ @8b∗
1674
+ @8b∗
1675
+ @8b∗
1676
+ @8b∗∗
1677
+ @8b∗∗
1678
+ @8b ∗∗
1679
+ Best ML eff.
1680
+ 1.3 TOPS/W@
1681
+ 1.3 TOPS/W@
1682
+ 200 GOPS/W@
1683
+ 2.47 TOPS/W@
1684
+ 4.5 TOPS/W@
1685
+ 5.57 TOPS/W,
1686
+ @Perf
1687
+ 2.8 GOPS, 8b∗
1688
+ 15.6 GOPS, 8b∗
1689
+ 7 GOPS, 8b∗
1690
+ 0.58 GOPS, 8b∗∗
1691
+ 2.3 MOPS, 8b∗∗
1692
+ 8b∗∗
1693
+ 11.9 TOPS/W@
1694
+ 11.6 TOPS/W,
1695
+ 2.4 GOPS, 2b∗∗
1696
+ 4b∗∗
1697
+ + estimated at 90% utilization of MACs, ∗ Matmul, ∗∗ CNN, 1 MAC = 2 Ops
1698
+ can be optimized using special DSP extensions available with
1699
+ the PULP libraries, which is left for future work.
1700
+ VII. COMPARISON WITH SOTA
1701
+ Table III shows the comparison of our SoC with SoTA on
1702
+ two fronts: on one hand, comparing with existing extreme edge
1703
+ SoCs (left), and on the other hand, with edge ML accelera-
1704
+ tors (right). Our SoC has similar or increased flexibility in
1705
+ application mapping compared to the extreme edge SoCs on
1706
+ the left, with much improved energy efficiency and power.
1707
+ TinyVers supports not only the IoT general processing (GP),
1708
+ DNNs and near-sensor analytics (NSA) like [17], [48], [49],
1709
+ but also DNN+ such as TCN and AE and traditional ML
1710
+ like SVM, all at better energy efficiency because of efficient
1711
+ mapping. This is evident from the best energy efficiency of
1712
+ 2.47 TOPS/W for running a CNN layer on TinyVers. The
1713
+ energy efficiency is further enhanced to 11.9 TOPS/W when
1714
+ the CNN workload is quantized to INT2. Compared to the
1715
+ extreme edge SoCs, TinyVers provides support for precision
1716
+ scalability and, thus, can take advantage of improved perfor-
1717
+ mance using quantization. Furthermore, by utilizing support
1718
+ for block structured sparsity, TinyVers can reach a peak
1719
+ performance of 17 TOPS/W for an 8-bit CNN layer. This is
1720
+ much higher than the efficiencies reported by [17], [48], [49].
1721
+ Compared to the edge ML accelerators on the right,
1722
+ TinyVers shows much more flexibility at comparable per-
1723
+ formance metrics in terms of energy efficiency and power
1724
+ consumption. The edgeML accelerators only support a single
1725
+ or few models extremely efficiently, but this approach has
1726
+ drawbacks in deployment for extreme edge devices. For ex-
1727
+ ample, [50] can only perform KWS with depthwise separable
1728
+ CNN and its performance is much lower than TinyVers with
1729
+ comparable energy efficiency. UNPU [51], can only support
1730
+ CNN and FC/RNN layers and also does not have a complete
1731
+ standalone SoC, which effects efficiency at the system level.
1732
+ Moreover, these edgeML accelerators cannot support any kind
1733
+ of duty cycling as they lack power management and retention
1734
+ memory support. TinyVers supports the multi-modal require-
1735
+ ments of extreme edge devices at relatively similar energy
1736
+ efficiencies of the order of TOPS/W. Moreover, it adds the
1737
+ possibility of extreme low power idle states for duty-cycling
1738
+ use cases to enable < 10µW operation, shown empirically in
1739
+ Section VI-D. To summarize, TinyVers brings the best of both
1740
+ worlds of extreme edge processors and edgeML accelerators.
1741
+ VIII. CONCLUSION
1742
+ TinyML applications at the extreme edge needs not only
1743
+ heterogeneous SoCs with flexible accelerators to support di-
1744
+ verse workloads, but also adaptive power management for
1745
+ different duty-cycling operations. Moreover, to enable such
1746
+ adaptive power management, the need for embedded non-
1747
+ volatile memories arises. TinyVers extends a RISC-V core
1748
+ with a flexible ML accelerator supporting a diverse set of
1749
+ ML workload mapping in terms of diverse compute kernels,
1750
+ different precision and structured sparsity conditions. Further-
1751
+ more, the inclusion of a WuC and an eMRAM enables the
1752
+ adaptive power management required in many duty-cycling
1753
+ use cases. Measurement result shows that the chip can achieve
1754
+ an energy efficiency range of 0.8-17 TOPS/W at 0.58 GOPS
1755
+ to 17.6 GOPS of throughput. The different low power modes
1756
+ enable the chip to achieve power range from 1.7µW-20 mW.
1757
+ The application of machine monitoring takes advantage of the
1758
+
1759
+ 11
1760
+ deep sleep mode to consume only 9.5µW of power at a duty
1761
+ cycle of 0.05. Thus, TinyVers takes a step towards creating a
1762
+ new class of ultra-low power extreme edge SoCs.
1763
+ ACKNOWLEDGMENTS
1764
+ The authors would like to thank ETHZ for their support
1765
+ on PULP platform and GlobalFoundries for 22FDX tapeout
1766
+ support. The work has been supported under ISAAC project
1767
+ (FOD Economie Belgium Energietransitiefonds (oproep II)) in
1768
+ collaboration with Magics Technologies and received funding
1769
+ from the Flemish Government (AI Research Program).
1770
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+ Energy-Efficient Deep Neural Network Accelerator With Fully Variable
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+ Weight Bit Precision,” IEEE Journal of Solid-State Circuits, vol. 54,
2011
+ no. 1, pp. 173–185, 2019.
2012
+ [52] M. Fariselli, M. Rusci, J. Cambonie, and E. Flamand, “Integer-Only
2013
+ Approximated MFCC for Ultra-Low Power Audio NN Processing on
2014
+ Multi-Core MCUs,” in 2021 IEEE 3rd International Conference on
2015
+ Artificial Intelligence Circuits and Systems (AICAS), 2021, pp. 1–4.
2016
+
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1
+ Trapped Ion Quantum Computing using Optical Tweezers and the Magnus Effect
2
+ M. Mazzanti,1 R. Gerritsma,1, 2 R. J. C. Spreeuw,1, 2 and A. Safavi-Naini2, 3
3
+ 1Van der Waals-Zeeman Institute, Institute of Physics, University of Amsterdam, 1098 XH Amsterdam, Netherlands
4
+ 2QuSoft, Science Park 123, 1098 XG Amsterdam, the Netherlands
5
+ 3Institute for Theoretical Physics, Institute of Physics, University of Amsterdam, Science Park 904, 1098 XH Amsterdam, the Netherlands
6
+ (Dated: January 13, 2023)
7
+ We consider the implementation of quantum logic gates in trapped ions using tightly focused optical tweezers.
8
+ Strong polarization gradients near the tweezer focus lead to qubit-state dependent forces on the ion. We show
9
+ that these may be used to implement quantum logic gates on pairs of ion qubits in a crystal. The qubit-state
10
+ dependent forces generated by this effect live on the plane perpendicular to the direction of propagation of
11
+ the laser beams opening new ways of coupling to motional modes of an ion crystal. The proposed gate does
12
+ not require ground state cooling of the ions and does not rely on the Lamb-Dicke approximation, although the
13
+ waist of the tightly focused beam needs to be comparable with its wavelength in order to achieve the needed
14
+ field curvature. Furthermore, the gate can be performed on both ground state and magnetic field insensitive
15
+ clock state qubits without the need for counter-propagating laser fields. This simplifies the setup and eliminates
16
+ errors due to phase instabilities between the gate laser beams. Finally, we show that imperfections in the gate
17
+ execution, in particular pointing errors < 30 nm in the tweezers reduce the gate fidelity from F ≳ 0.99998 to
18
+ ≳ 0.999.
19
+ Trapped ions are one of the most mature platforms for the
20
+ implementation of quantum computing and quantum logic
21
+ gates have been implemented with very high fidelity in these
22
+ systems [1, 2]. Usually, the quantum logic gates in trapped
23
+ ions rely on state-dependent forces applied to the ions by
24
+ laser fields or magnetic fields.
25
+ The exchange of motional
26
+ quanta between the ions then leads to effective qubit-qubit in-
27
+ teractions. Several recent works have explored how the use
28
+ of state-of-the-art optical tweezer technology can benefit the
29
+ trapped ion quantum computer. Optical tweezers can be used
30
+ to confine atoms very strongly by inducing a dipole in them
31
+ and find application in neutral atomic quantum simulators, in
32
+ which tweezers are used to levitate individual atoms [3–7].
33
+ In trapped ions, tweezers may be used to tune the soundwave
34
+ spectrum in the ion crystal and thereby to program the inter-
35
+ actions between the qubits [8–10]. Furthermore, in a recent
36
+ work [11] we have proposed combining state-dependent opti-
37
+ cal tweezers with oscillating electric fields to build a universal
38
+ trapped ion quantum computer with extremely long-ranged in-
39
+ teractions between the qubits.
40
+ In this work, we consider another scenario, in which we
41
+ make use of the strong polarization gradients that occur in op-
42
+ tical tweezers. We note that strong gradients in optical po-
43
+ tentials have been previously investigated to implement two-
44
+ qubit gates without the need for ground-state cooling [12–
45
+ 14]. However, our approach utilizes the state-dependent dis-
46
+ placement of the tweezer potential due to polarization gradi-
47
+ ents [15–17]. We propose to use this optical analogue of the
48
+ Magnus effect to implement quantum logic gates in trapped
49
+ ions.
50
+ Setup – We consider linearly x-polarized, Gaussian tweez-
51
+ ers, pointing in the −y direction and tightly focused at two
52
+ qubits between which we wish to implement a quantum logic
53
+ gate. The quantum computing platform here considered is a
54
+ linear crystal of N alkali-like trapped ions of mass m. In the
55
+ focal plane the ions experience a strong polarization gradient
56
+ along the x direction, such that the polarization is linear (x)
57
+ in the center and circular (σ±)z in the wings of the Gaussian.
58
+ b)
59
+ a)
60
+ ⃗y
61
+ ⃗x
62
+ ⃗z
63
+ mj
64
+ P1/2
65
+ −1/2
66
+ +1/2
67
+ |0⟩
68
+ |1⟩
69
+ Ω−
70
+ S1/2
71
+ Ω+
72
+ nX+
73
+ +
74
+ +
75
+ +
76
+ +
77
+ +
78
+ +
79
+ +
80
+ −6 −4 −2
81
+ 0
82
+ 2
83
+ 4
84
+ 6
85
+ x/λ
86
+ −4
87
+ −2
88
+ 0
89
+ 2
90
+ 4
91
+ z/λ
92
+ (σ−)z
93
+ −6 −4 −2
94
+ 0
95
+ 2
96
+ 4
97
+ 6
98
+ x/λ
99
+ −4
100
+ −2
101
+ 0
102
+ 2
103
+ 4 (σ+)z
104
+ −6 −4 −2
105
+ 0
106
+ 2
107
+ 4
108
+ 6
109
+ x/λ
110
+ −4
111
+ −2
112
+ 0
113
+ 2
114
+ 4
115
+ z/λ
116
+ (σ−)z
117
+ −6 −4 −2
118
+ 0
119
+ 2
120
+ 4
121
+ 6
122
+ x/λ
123
+ −4
124
+ −2
125
+ 0
126
+ 2
127
+ 4 (σ+)z
128
+ Laguerre-Gaussian
129
+ Gaussian
130
+ FIG. 1. Schematic representation of the two-qubit gate. a) We apply
131
+ tweezers propagating along the −y direction on the two ions forming
132
+ the gate. The tweezer intensity can be decomposed into three polar-
133
+ ization components. b) Simplified level scheme of an alkaline-earth
134
+ like ion without nuclear spin showing the encoding of the qubit in
135
+ its Zeeman ground states. The two polarization components of the
136
+ tweezer couple to different states in the P1/2 manifold with detuning
137
+ ∆. This causes the minima of the tweezer potentials to be shifted by
138
+ an amount ±λ depending on the qubit state. Bottom : main polar-
139
+ ization components for a Gaussian and Laguerre-Gaussian (l = 1,
140
+ n = 0) tightly focused tweezer.
141
+ A direct calculation [18] decomposing the field in the focal
142
+ plane into its circular components (σ±)z (and πz) shows that,
143
+ to a good approximation, the circular components are near-
144
+ Gaussian distributions, displaced in opposite directions along
145
+ the x axis. We depict this setup in Fig. 1. Note that the circu-
146
+ lar components rotate in the xy plane, i.e. a plane containing
147
+ the k vector of the light. As shown in Fig. 1, the (σ±)z com-
148
+ ponent is displaced by an amount ±λ ≡ ±λ/2π, with λ the
149
+ arXiv:2301.04668v1 [quant-ph] 11 Jan 2023
150
+
151
+ 2
152
+ tweezer wavelength. As the total field is the superposition
153
+ of two displaced Gaussians, its intensity is slightly elongated
154
+ along x. Hollow tweezers (Gaussian-Laguerre) can be used
155
+ instead of Gaussian ones. This will provide the needed field
156
+ curvature while keeping near-zero intensity at the center of
157
+ the beam, drastically reducing the probability of off-resonant
158
+ scattering that might limit the gate fidelity.
159
+ For simplicity, we first consider ions without nuclear spin,
160
+ such as 40Ca+, 88Sr+, 138Ba+ and 174Yb+. The qubits are
161
+ encoded in the electronic ground states 2S1/2 and |0⟩ = |j =
162
+ 1/2, mj = 1/2⟩ and |1⟩ = |j = 1/2, mj = −1/2⟩ with
163
+ j the total electronic angular momentum and mj its projec-
164
+ tion on the quantization axis. The magnetic field lies along
165
+ the z-direction and the tweezers are polarized along the x-
166
+ direction, such that the ions experience linearly polarized laser
167
+ light. The direction along the x-axis is the long direction of
168
+ the ion trap, with trap frequency ωx. The motion of the ions
169
+ along the x-direction can be described by collective modes of
170
+ harmonic motion with frequencies ωm and mode vectors bi,m,
171
+ with m labeling the mode and i the ion [19].
172
+ We choose the detuning between the tweezers and the D1
173
+ transition to be large enough to avoid photon scattering, but
174
+ much smaller than the spin-orbit coupling splitting of the 2P
175
+ state. In this way, we can neglect coupling to the P3/2 state.
176
+ In what follows we will show that this requirement can be
177
+ satisfied experimentally. Close to the center of the tweezer,
178
+ strong polarization gradients appear and as a result, the two
179
+ qubit states experience slightly different tweezer potentials. In
180
+ particular, as we show in Fig. 1(a), the optical Magnus effect
181
+ causes each qubit state to experience a tweezer potential that
182
+ is offset from the apparent center of the tweezer by ∼ λ [16].
183
+ Hence, we may approximate the tweezer potential as :
184
+ ˆU(x) = −U0 exp
185
+
186
+ −2(ˆx + ˆσzλ)2/w2
187
+ 0
188
+
189
+ (1)
190
+ ≈ − ˜U0 + 1
191
+ 2mω2
192
+ twˆx2 + gx ˆσz
193
+ (2)
194
+ with ωtw =
195
+
196
+ 4 ˜U0(w2
197
+ 0 − 4λ2)/(mw4
198
+ 0), g = 4 ˜U0λ/w2
199
+ 0, and
200
+ ˜U0 = U0 exp(−2λ2/w2
201
+ 0) ≈ U0. Here U0 is the tweezer po-
202
+ tential in the center and the beam waist is w0. Our approxima-
203
+ tion replaces the tweezer potential with a harmonic potential
204
+ and is valid for w0 ≫ lm, with lm =
205
+
206
+ ℏ/2mωm. The last
207
+ term in U(x) is the result of the spin-dependent force g cou-
208
+ pling the internal state of the qubit, ˆσz, to its motion ˆx. Thus,
209
+ the optical Magnus effect allows us to straightforwardly im-
210
+ plement a quantum gate.
211
+ Tweezer Hamiltonian – In the interaction picture with re-
212
+ spect to ˆH0 = ℏωmˆa†
213
+ mˆam the tweezer Hamiltonian on ions i
214
+ and j is:
215
+ ˆH1 = A(t)
216
+ �1
217
+ 2mω2
218
+ tw
219
+
220
+ ˆx2
221
+ i + ˆx2
222
+ j
223
+
224
+ + g
225
+
226
+ ˆσ(i)
227
+ z ˆxi + ˆσ(j)
228
+ z ˆxj
229
+ ��
230
+ .
231
+ (3)
232
+ Here, ˆxi = �
233
+ m lmbim
234
+
235
+ ˆame−iωmt + ˆa†
236
+ meiωmt�
237
+ is the posi-
238
+ tion operator of ion i in the interaction picture, with ˆa†
239
+ m the
240
+ creation operator for the mode m, and 0 ≤ A(t) ≤ 1 speci-
241
+ fies the time-dependence of the tweezer intensity. The qubit-
242
+ state independent terms in ˆH1 do not alter the dynamics of the
243
+ quantum gate. We ignore these terms and arrive at:
244
+ ˆH2 = A(t)g
245
+
246
+ ˆxiˆσ(i)
247
+ z
248
+ + ˆxjˆσ(j)
249
+ z
250
+
251
+ ,
252
+ (4)
253
+ which takes the form of a spin-phonon coupling Hamilto-
254
+ nian reminiscent of the Mølmer-Sørenson scheme for phonon-
255
+ mediated quantum gates in trapped ions [20]. However, at this
256
+ stage we still have various choices available for A(t), depend-
257
+ ing on which type of quantum gate we would like to imple-
258
+ ment. For instance, pulsed A(t) could be used to perform fast
259
+ gates. Here, we choose A(t) to obtain a geometric phase gate.
260
+ For this, we set 2A(t) = 1−cos(νt+φ) where φ = 0 assures
261
+ a smooth ramp of the tweezer intensity and ν = ωc + δ with
262
+ the subscript c denoting the center-of-mass (c.o.m.) mode for
263
+ which ωc = ωx and bi,c = 1/
264
+
265
+ N. We write the operators ˆxi
266
+ and ˆxj in terms of ˆac and ˆa†
267
+ c and perform the rotating wave
268
+ approximation to arrive at:
269
+ ˆH3 =
270
+ glc
271
+ 4
272
+
273
+ N
274
+
275
+ ˆaceiδt + ˆa†
276
+ ce−iδt� �
277
+ ˆσ(i)
278
+ z
279
+ + ˆσ(j)
280
+ z
281
+
282
+ .
283
+ (5)
284
+ To derive the qubit-qubit interactions forming the geomet-
285
+ ric phase gate, we perform a unitary transformation ˆU1 =
286
+ e−iδˆa†
287
+ c ˆact to eliminate the time dependence, followed by a
288
+ Lang-Firsov [21] transformation, ˆU2 = exp
289
+
290
+ ˆα
291
+
292
+ ˆa†
293
+ c − ˆac
294
+ ���
295
+ with ˆα = − ˜g
296
+ δ
297
+
298
+ ˆσ(i)
299
+ z
300
+ + ˆσ(j)
301
+ z
302
+
303
+ . Disregarding qubit-independent
304
+ terms, we obtain
305
+ Heff = 2˜g2
306
+ ℏδ ˆσ(i)
307
+ z ˆσ(j)
308
+ z ,
309
+ (6)
310
+ with ˜g = glc/(4
311
+
312
+ N) = ˜η ˜U0, with the proportionality factor
313
+ ˜η = λlc/(
314
+
315
+ Nw2
316
+ 0). This Hamiltonian generates qubit-qubit
317
+ interactions that can be used to implement a geometric phase
318
+ gate by setting the gate time τ = 2π/δ and ˜g2τ
319
+ ℏ2δ = π/4.
320
+ Characterization of the gate – We analyse the gate dynam-
321
+ ics by performing numerical simulation of the full dynamics
322
+ generated by the Hamiltonian ˆHsim = ˆH0 + ˆU (xi) + ˆU (xj)
323
+ for a two dimensional ion crystal where the tweezers po-
324
+ tentials ˆU (xi;j) on ions i and j have been expanded up to
325
+ fourth-order including spin-independent terms. We use real-
326
+ istic experimental parameters: ∼ 156 µW of tweezer laser
327
+ power focused to a waist of w0 ∼ 0.5 µm and tuned 15 THz
328
+ to the red from the 2S1/2 →
329
+ 2P1/2 transition in 174Yb+
330
+ (λ = 369.5 nm). This results in ˜U0/h ∼ 1.6 MHz, ˜g/h =
331
+ 2.1 kHz/
332
+
333
+ N, and setting δ = 2π × 12.2 kHz/
334
+
335
+ N the gate
336
+ time for the geometric phase gate is τ = 170
337
+
338
+ Nµs. With a
339
+ calculated qubit-state independent tweezer potential of ωtw ∼
340
+ 2π × 37 kHz, the center-of-mass mode frequency (ωc/2π ∼
341
+ 1 MHz) is shifted by ∼ 2ω2
342
+ tw/ωcN ∼ 2π × 710/N Hz.
343
+ This shift can easily be taken into account by correcting δ
344
+ accordingly. In these estimates, we neglected the contribu-
345
+ tion from other dipole allowed transitions, that are detuned by
346
+ ∼ 66 THz (the relatively weak 2S1/2 → 3[3/2]3/2 transition)
347
+ and 115 THz (the strong D2 line) or more.
348
+ We consider the gate unitary with a spin-echo sequence
349
+ given by U(0, τ) = X⊗2U(τ/2, τ)X⊗2U(0, τ/2), where
350
+
351
+ 3
352
+ FIG. 2. We calculate the gate fidelity for a ground state cooled ion
353
+ ¯nc, ¯ns = 0 (blue), sub-Doppler cooled thermal state with ¯nc =
354
+ 0.62, ¯ns = 0.23 (orange) and ¯nc = 15, ¯ns = 0.23 (red, using in
355
+ this case a Fock cutoff nc ≤ 120, ns ≤ 10). (a) Process fidelity
356
+ of the two-qubit Magnus gate for different gate times. (b) Effects of
357
+ misalignment ϵ (orange) and intensity noise Λ1/τ (blue) on the gate
358
+ fidelity. The size of each intensity noise data point represents the
359
+ standard deviation of 20 simulation where we generated a random
360
+ Gaussian noise with σ = Λ1/τ on each of the two pulses. This
361
+ implies a noise on the laser intensity at frequency 1/τ that can not
362
+ be removed by the spin-echo sequence.
363
+ X⊗2 is a qubit flip on both qubits. This spin echo sequence is
364
+ needed in order to remove local rotations on the qubits states
365
+ and possible timing errors. We calculate the unitary time evo-
366
+ lution operator U(0, τ) for a system of two ions with their
367
+ motional c.o.m. and stretch modes and truncate their respec-
368
+ tive Hilbert spaces to nc ≤ 18 and ns ≤ 10. In figure 2 we
369
+ show the process fidelity of the gate assuming the ions are in
370
+ their motional ground state (¯n = 0) as a function of gate time.
371
+ The gate fidelity of F = 0.999988 with nc = ns = 0 rivals
372
+ the current standard approaches. Moreover, the performance
373
+ of our gate is robust to the thermal occupation of the motional
374
+ modes. We characterize the gate performance in presence of
375
+ thermal phonons using the average gate fidelity [18, 22] and
376
+ find that it depends weakly on the motional state of the two
377
+ ions. In fact, using ¯nc = 0.62, ¯ns = 0.23, the fidelity is
378
+ almost unaltered at Fth = 0.999989.
379
+ One of main experimental challenges is perfect tweezer
380
+ alignment. We have studied the resilience of the gate against
381
+ misalignment of the tweezer in the x-direction, which we
382
+ denote by ϵ.
383
+ In the presence of misalignment,
384
+ ˜U0
385
+
386
+ |0⟩
387
+ |1⟩
388
+
389
+ mF
390
+ −1
391
+ 0
392
+ +1
393
+ 171Yb+
394
+ FIG. 3. Relevant energy levels of 171Yb+ for implementing the gate
395
+ on hyperfine qubit splitted by ωq. The coupling can be achieved
396
+ using a pair of Raman beams detuned from the upper state 2P1/2 by
397
+ ∆. In the brackets are the angular contributions to the various dipole
398
+ transition elements.
399
+ TABLE I. Main sources of gate errors. We estimate γph as the prob-
400
+ ability of a off-resonant scattering in for 174Yb+ during the gate time
401
+ (τ = 240 µs) for a Gaussian and Laguerre-Gaussian beams. Other
402
+ typical sources of errors are misalignment (ϵ), tweezer intensity noise
403
+ (Λ1/τ) and timing (∆τ). The values here reported are for laser pa-
404
+ rameters used in our numerical simulations.
405
+ Error source
406
+ γph
407
+ Gaussian
408
+ γph
409
+ Laguerre-Gaussian
410
+ ϵ
411
+ 30 nm
412
+ Λ1/τ
413
+ 0.5%
414
+ ∆τ
415
+ ±5 µs
416
+ 1 − F
417
+ 2 × 10−3
418
+ 10−6
419
+ 1.3 × 10−3 9.3 × 10−5 2.7 × 10−4
420
+ U0 exp−2(ϵ+ˆσzλ)2/ω2
421
+ 0.
422
+ Thus, the misalignment has two ef-
423
+ fects: (i) it changes the tweezer potential at the center of the
424
+ tweezer and therefore the phase accumulation in the phase
425
+ gate, and (ii) it shifts the potential in a qubit-state-dependent
426
+ way. The second contribution is corrected to lowest order by
427
+ a spin-echo sequence. Figure 2(b) shows the infidelity as
428
+ a function of ϵ. Here we assume that the tweezers are mis-
429
+ aligned on both ions in the same way which seems the experi-
430
+ mentally most likely case. The unitary U(0, τ) leads to phase
431
+ space trajectories for ⟨x(t)⟩ and ⟨px(t)⟩ associated with the
432
+ c.o.m. motion[18]. As expected, we find approximately cir-
433
+ cular phase-space orbits for the even parity states |00⟩, |11⟩,
434
+ and very little motion for the odd parity ones. We see that ev-
435
+ ery state combination leads to ion motion, but the difference
436
+ in motion still leads to a high fidelity of ≳ 0.999 as shown in
437
+ Figure 2(b).
438
+ Clock state case – While the calculation was performed
439
+ for the electron spin qubit states in 174Yb+, it should also
440
+ be possible to use the hyperfine clock states |F = mF = 0⟩
441
+ and |F = 1, mF = 0⟩ in 171Yb+. This qubit is insensitive to
442
+ magnetic field noise and coherence times of up to an hour have
443
+ been measured [23]. In this case, the tweezers are formed by a
444
+ bichromatic co-propagating laser field detuned by ∆ from the
445
+ D1 transition at 369.5 nm with overall detuning ∆ ≪ ωFS, the
446
+ fine structure splitting. We set the frequency difference in the
447
+
448
+ 4
449
+ bichromatic tweezer to 12.6 GHz, corresponding to the tran-
450
+ sition between the qubit states [24]. The tweezer laser then
451
+ causes Raman coupling between the qubit states via two dis-
452
+ tinct paths. In the first path, the qubits are coupled via the state
453
+ |P1/2, F = 1, mF = −1⟩ due to the σ− polarization compo-
454
+ nent in the tweezer. In the other, the qubits are coupled via
455
+ the state |P1/2, F = 1, mF = +1⟩ due to the σ+ component
456
+ in the tweezer. We denote the Rabi frequencies of each path
457
+ as Ω±
458
+ 1,2(x). The corresponding Raman couplings of each path
459
+ interfere destructively in the center of the tweezer due to a rel-
460
+ ative minus sign between Ω+
461
+ 1 (x) and Ω+
462
+ 2 (x) in their Clebsch-
463
+ Gordan coefficient, ∝ (Ω−
464
+ 1 (0)Ω−
465
+ 2 (0)+Ω+
466
+ 1 (0)Ω+
467
+ 2 (0))/∆ = 0.
468
+ However, the Magnus effect causes a strong position depen-
469
+ dence of the relative strength of both paths of magnitude
470
+ Ωeff(x) = Ω−
471
+ 1 (x)Ω−
472
+ 2 (x)
473
+
474
+ + Ω+
475
+ 1 (x)Ω+
476
+ 2 (x)
477
+
478
+ ≈ Ω2
479
+
480
+ 4λx
481
+ w2
482
+ 0
483
+ ,
484
+ (7)
485
+ where we assumed x ≪ λ ≪ w0 and |Ω±
486
+ i (0)| = Ω/
487
+
488
+ 2 with
489
+ i = 1, 2, such that both laser frequencies have the same power.
490
+ As a result, a qubit state-dependent force appears as in Eq.
491
+ (4), except that we must now replace ˆσ(i,j)
492
+ z
493
+ → ˆσ(i,j)
494
+ x
495
+ and the
496
+ gate takes the form of the usual Mølmer-Sørensen interaction
497
+ ∝ ˆσ(i)
498
+ x ˆσ(j)
499
+ x
500
+ [20]. Amplitude modulation via A(t) allows again
501
+ for resonant enhancement of the gate.
502
+ In addition to the Raman coupling, we obtain a tweezer po-
503
+ tential (AC Stark shift) for each qubit state of magnitude
504
+ δ|k⟩
505
+ AC(x) =
506
+
507
+ i=1,2
508
+
509
+ j=+,−
510
+ |Ωj
511
+ i(x)|2
512
+ ∆i,|k⟩
513
+ (8)
514
+ with ∆1,|0⟩ = ∆ − ωq, ∆2,|0⟩ = ∆, ∆1,|1⟩ = ∆ and ∆2,|1⟩ =
515
+ ∆ + ωq. This causes an additional trapping potential Φ(x) ≈
516
+ 1
517
+ 2mω2
518
+ twx2 that is independent of the qubit state as before, as
519
+ well as a position-dependent differential Stark shift δAC(x) =
520
+ δ|1⟩
521
+ AC(x) − δ|0⟩
522
+ AC(x). In the limit ωq ≪ |∆|,
523
+ δAC(x) ≈ − ωq
524
+ ∆2
525
+
526
+ i=1,2
527
+
528
+ j=+,−
529
+ |Ωj
530
+ i(x)|2
531
+ (9)
532
+ = −ωq
533
+
534
+ ˜U0(x)
535
+ (10)
536
+ This differential Stark shift is estimated to be small, δAC/2π ≈
537
+ 2.7 kHz for the numbers used in the simulations, and can be
538
+ compensated by a corresponding Raman detuning.
539
+ Photon scattering on the D1 transition can be estimated as
540
+ γph ∼ ˜U0Γ/(ℏ∆) ∼ 13 s−1 with Γ = 1.23 × 108 s−1 in
541
+ Yb+. This adverse effect may be reduced significantly by em-
542
+ ploying hollow tweezers [11, 25, 26] at the expense of added
543
+ complexity. For a hollow beam with a waist w0 = 0.5 µm
544
+ and ∼ 160 µW we obtain a reduction in scattering rate of
545
+ ∼ 10−6 s−1. As long as ωtw ≪ Ωrf, the drive frequency of the
546
+ Paul trap, no parametric excitations can occur and micromo-
547
+ tion of the ions is not a problem. Other errors, such as due to
548
+ intensity noise of the laser, heating of the ions due to electric
549
+ field noise and decoherence due to magnetic field noise have
550
+ the same effect as in other gate implementations. Finally, we
551
+ note that because the tweezers are far detuned from the closest
552
+ transitions, the exact overall frequency of the tweezer laser is
553
+ irrelevant.
554
+ Conclusions In conclusion, we have described a novel
555
+ type of quantum phase gate based on the optical Magnus ef-
556
+ fect using optical tweezers in a linear chain of trapped ions.
557
+ The main benefit is that the gate does not require counter-
558
+ propagating laser fields, greatly simplifying the setup and
559
+ eliminating errors due to phase instabilities between the gate
560
+ laser beams. Furthermore, the state-dependent force gener-
561
+ ated by the Magnus effect allows to perform the gate by cou-
562
+ pling to motional modes on the plane perpendicular to the di-
563
+ rection of propagation of the tweezers allowing novel experi-
564
+ mental implementations. The proposed gate does not require
565
+ ground state cooling and can perform a quantum logic gate
566
+ on any pair of ion qubits by spatial addressing. The expected
567
+ gate fidelity rivals the state of the art also for ions that are not
568
+ cooled to the ground-state of motion.
569
+ ACKNOWLEDGEMENTS
570
+ This work was supported by the Netherlands Organiza-
571
+ tion for Scientific Research (Grant Nos.
572
+ 680.91.120 and
573
+ 680.92.18.05, (R.G.). A.S.N is supported by the Dutch Re-
574
+ search Council (NWO/OCW), as part of the Quantum Soft-
575
+ ware Consortium programme (project number 024.003.037).
576
+ [1] C. Ballance, T. Harty, N. Linke, M. Sepiol, and D. Lucas,
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+ Phys. Rev. Lett. 117, 060504 (2016).
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+ [2] J. Gaebler, T. Tan, Y. Lin, Y. Wan, R. Bowler, A. Keith,
579
+ S. Glancy, K. Coakley, E. Knill, D. Leibfried, and D. Wineland,
580
+ Phys. Rev. Lett. 117, 060505 (2016).
581
+ [3] D. Barredo, S. d. Léséleuc, V. Lienhard, T. Lahaye, and
582
+ A. Browaeys, Science 354, 1021 (2016).
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+ [4] M. Endres, H. Bernien, A. Keesling, H. Levine, E. R. Anschuetz,
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+ A. Krajenbrink, C. Senko, V. Vuletic, M. Greiner, and M. D.
585
+ Lukin, Science 354, 1024 (2016).
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+ [5] M. Norcia, A. Young, and A. Kaufman, Phys. Rev. X 8, 041054
587
+ (2018).
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+ [6] H. Levine, A. Keesling, G. Semeghini, A. Omran, T. T. Wang,
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+ S. Ebadi, H. Bernien, M. Greiner, V. Vuleti´c, H. Pichler, and
590
+ M. D. Lukin, Phys. Rev. Lett. 123, 170503 (2019).
591
+ [7] A. Browaeys and T. Lahaye, Nature Physics 16, 132–142 (2020).
592
+ [8] T. Olsacher, L. Postler, P. Schindler, T. Monz, P. Zoller, and L. M.
593
+ Sieberer, PRX Quantum 1, 020316 (2020).
594
+ [9] Y. H. Teoh, M. Sajjan, Z. Sun, F. Rajabi, and R. Islam,
595
+ Phys. Rev. A 104, 022420 (2021).
596
+ [10] J. D. Arias Espinoza,
597
+ M. Mazzanti,
598
+ K. Fouka,
599
+ R. X.
600
+ Schüssler, Z. Wu, P. Corboz, R. Gerritsma, and A. Safavi-Naini,
601
+ Phys. Rev. A 104, 013302 (2021).
602
+ [11] M. Mazzanti, R. X. Schüssler, J. D. Arias Espinoza, Z. Wu,
603
+ R. Gerritsma, and A. Safavi-Naini, Phys. Rev. Lett. 127, 260502
604
+
605
+ (2021).
606
+ [12] J. I. Cirac and P. Zoller, Nature 404, 579 (2000).
607
+ [13] M. Šašura and A. M. Steane, Phys. Rev. A 67, 062318 (2003).
608
+ [14] T. Calarco, J. I. Cirac, and P. Zoller, Phys. Rev. A 63, 062304
609
+ (2001).
610
+ [15] K.-P. Wang, J. Zhuang, X.-D. He, R.-J. Guo, C. Sheng, P. Xu,
611
+ M. Liu, J. Wang, and M.-S. Zhan, Chinese Phys. Lett. 37, 044209
612
+ (2020).
613
+ [16] R. J. Spreeuw, Phys. Rev. Lett. 125, 233201 (2020).
614
+ [17] R. J. C. Spreeuw, Nanophotonics 11, 633 (2022).
615
+ [18] See supplementary material at link to be inserted by editor for
616
+ definitions, technical details and supporting calculations,.
617
+ [19] D. F. V. James, Appl. Phys. B 66, 181 (1998).
618
+ [20] K. Mølmer and A. Sørensen, Phys. Rev. Lett. 82, 1835 (1999).
619
+ [21] I. G. Lang and Y. A. Firsov, J. Exp. Theor. Phys. 3, 27, 443
620
+ (1968).
621
+ [22] M. A. Nielsen, Physics Letters A 303, 249 (2002).
622
+ [23] P. Wang, C.-Y. Luan, M. Qiao, M. Um, J. Zhang, Y. Wang,
623
+ X. Yuan, M. Gu, J. Zhang, and K. Kim, Nat. Com. 12, 233
624
+ (2021).
625
+ [24] S. Olmschenk, K. C. Younge, D. L. Moehring, D. N. Matsuke-
626
+ vich, P. Maunz, and C. Monroe, Phys. Rev. A 76, 052314 (2007).
627
+ [25] C. T. Schmiegelow, J. Schulz, H. Kaufmann, T. Ruster, U. G.
628
+ Poschinger, and F. Schmidt-Kaler, Nat. Com. 7, 12998 (2016).
629
+ [26] M. Drechsler, S. Wolf, C. T. Schmiegelow, and F. Schmidt-
630
+ Kaler, arXiv:2104.07095 (2021).
631
+
632
+ Supplementary material for :
633
+ Trapped Ion Quantum Computing using Optical Tweezers and the Magnus Effect
634
+ M. Mazzanti,1 R. Gerritsma,1, 2 R. J. C. Spreeuw,1, 2 and A. Safavi-Naini2, 3
635
+ 1Van der Waals-Zeeman Institute, Institute of Physics, University of Amsterdam, 1098 XH Amsterdam, Netherlands
636
+ 2QuSoft, Science Park 123, 1098 XG Amsterdam, the Netherlands
637
+ 3Institute for Theoretical Physics, Institute of Physics, University of Amsterdam, Science Park 904, 1098 XH Amsterdam, the Netherlands
638
+ (Dated: January 13, 2023)
639
+ APPENDIX I : OPTICAL MAGNUS EFFECT
640
+ A key characteristic of a tightly focused beam is the strong
641
+ field curvature near the focus. This not only affects the local
642
+ intensity but also its polarization structure. To calculate this,
643
+ we take a superposition of plane waves labeled by their wave
644
+ vector in spherical coordinates, k = (k, θ, φ). Taking k =
645
+ ω/c as fixed we write
646
+ E(r) ∝
647
+ � 2π
648
+ 0
649
+
650
+ � π
651
+ 0
652
+ dθ sin θ ux(θ, φ) a(θ, φ) eik·r
653
+ with ux(θ, φ) a polarization vector obtained by co-rotating
654
+ the x unit vector when k is rotated from z to (θ, φ), such
655
+ that ux(θ, φ) · k = 0, see also Ref. [S1]. In the calcula-
656
+ tion we center the beam around θ = 0, and the focal plane
657
+ is given by r = (x, y, 0).
658
+ The shape of the beam is de-
659
+ termined by the amplitude function a(θ, φ). For a Gaussian
660
+ beam we set a(θ, φ) = exp(−θ2/w2
661
+ θ); for the lowest or-
662
+ der (l = 1) Laguerre-Gaussian (LG) beam we set a(θ, φ) =
663
+ θ exp(iφ − θ2/w2
664
+ θ). After performing the above integral we
665
+ rotate the results for tweezers propagating along the −y di-
666
+ rection. Finally, the circular field components σ± shown in
667
+ Fig. 1 of the main text are obtained as the projection onto unit
668
+ vectors (x ± iy)/
669
+
670
+ 2. In Figure S-1, all three polarization
671
+ components for a Laguerre-Gaussian beam are shown. Note
672
+ that the σ− and σ+ components have similar intensity while
673
+ the π-polarization is suppressed by a factor ∼ 100.
674
+ −6 −4 −2 0
675
+ 2
676
+ 4
677
+ 6
678
+ x/λ
679
+ −4
680
+ −2
681
+ 0
682
+ 2
683
+ 4
684
+ z/λ
685
+ (σ−)z
686
+ −6 −4 −2 0
687
+ 2
688
+ 4
689
+ 6
690
+ x/λ
691
+ −4
692
+ −2
693
+ 0
694
+ 2
695
+ 4 (π)z
696
+ −6 −4 −2 0
697
+ 2
698
+ 4
699
+ 6
700
+ x/λ
701
+ −4
702
+ −2
703
+ 0
704
+ 2
705
+ 4 (σ+)z
706
+ FIG. S-1. Intensity of the polarization components for a LG beam
707
+ calculated at the focus. The π-polarization component has been en-
708
+ hanced by a factor 100 to make it visible. Here we set wθ = 0.6
709
+ APPENDIX II : PHASE-SPACE DYNAMICS
710
+ We study the phase-space dynamics of the ions by simulat-
711
+ ing the time dependent Hamiltonian using trotterization with
712
+ time-steps of 10−4 τ. At each time-step we evaluate the ex-
713
+ pectation value of the ⟨ˆx⟩ and ⟨ˆp⟩ for the center of mass mode.
714
+ As expected, we find approximately circular phase-space or-
715
+ bits for the even parity states |00⟩, |11⟩, and very little motion
716
+ for the odd parity ones. In Fig. S-2 it is possible to see the evo-
717
+ lution in phase-space for all the four spin states in case of per-
718
+ fectly aligned and slightly misaligned tweezers. As described
719
+ in the main text we simulate numerically the full Hamiltonian
720
+ defined as ˆHsim = ˆH0 + ˆU (xi) + ˆU (xj) where in case of
721
+ misalignment ϵ, ˆU (x) reads as :
722
+ U(x) ≈ −U0 e−2((ˆx−ˆϵ)+ˆσzλ)2/w2
723
+ 0
724
+ ≈ − ˜U0 + 4 ˜U0
725
+ ˆσzλ − ˆϵ
726
+ w2
727
+ 0
728
+ ˆx
729
+ + 1
730
+ 2
731
+ ˜U0
732
+
733
+ 4
734
+
735
+ w2
736
+ 0 − 4λ2�
737
+ w4
738
+ 0
739
+
740
+ ˆx2 − 1
741
+ 2
742
+ ˜U0
743
+
744
+ 16
745
+
746
+ ˆϵ2 − 2ˆσzˆϵλ
747
+
748
+ w4
749
+ 0
750
+
751
+ ˆx2
752
+
753
+
754
+ 8 ˜U0ˆσzλ3w2
755
+ 0 − 4
756
+
757
+ 3ˆϵ2 + λ2�
758
+ 3w6
759
+ 0
760
+
761
+ ˆx3
762
+ +
763
+
764
+ 8 ˜U0ˆϵ3w2
765
+ 0 − 4
766
+
767
+ ˆϵ2 + 3λ2�
768
+ 3w6
769
+ 0
770
+
771
+ ˆx3
772
+
773
+
774
+ 2 ˜U0ˆσzλˆϵ−48w2
775
+ 0 + 64
776
+
777
+ ˆϵ2 + λ2�
778
+ 3w8
779
+ 0
780
+
781
+ ˆx4
782
+ +
783
+
784
+ 2 ˜U0
785
+ 3w4
786
+ 0 − 24w2
787
+ 0
788
+
789
+ ˆϵ2 + λ2�
790
+ + 16
791
+
792
+ ˆϵ4 + 6ˆϵ2λ2 + λ4�
793
+ 3w8
794
+ 0
795
+
796
+ ˆx4.
797
+ with
798
+ ˜U0 = U0e−2(ˆϵ+ˆσzλ)2/w2
799
+ 0
800
+ A small tweezer misalignment ϵ gives rise to new spin-
801
+ dependent terms in the Hamiltonian that shift the trapping po-
802
+ tential in a state dependent way. In Fig.S-2 is shown how the
803
+ dynamics is affected in the case where the tweezers are mis-
804
+ aligned by 30 nm.
805
+ APPENDIX III : GATE FIDELITY
806
+ We characterize the gate by calculating the average process
807
+ fidelity as follows : [S2]:
808
+ ¯F( ˆUid, ˆU ˆ
809
+ Hsim) =
810
+
811
+ j tr
812
+
813
+ ˆUidˆσ†
814
+ j ˆU †
815
+ idˆσj( ˆU ˆ
816
+ Hsim)
817
+
818
+ + d2
819
+ d2 (d + 1)
820
+ ,
821
+
822
+ 2
823
+ −1.4
824
+ −0.7
825
+ 0.0
826
+ 0.7
827
+ 1.4
828
+ ⟨ˆx⟩
829
+ −1.4
830
+ −0.7
831
+ 0.0
832
+ 0.7
833
+ 1.4
834
+ ⟨ˆpx⟩
835
+ ϵ = 0
836
+ −2.1 −1.4 −0.7 0.0
837
+ 0.7
838
+ 1.4
839
+ ⟨ˆx⟩
840
+ −1.4
841
+ −0.7
842
+ 0.0
843
+ 0.7
844
+ 1.4
845
+ ⟨ˆpx⟩
846
+ ϵ = 30 nm
847
+ ψ↑↑
848
+ ψ↓↑
849
+ ψ↑↓
850
+ ψ↓↓
851
+ FIG. S-2. Center of mass mode phase-space dynamics for perfectly
852
+ aligned tweezer (left) and for 30 nm misaligned ones (right). For the
853
+ simulation we used the same parameters as for τ/2 = 120 µs point
854
+ in Figure 1(a) of the main text.
855
+ where ˆUid is the unitary of an ideal geometric phase gate and
856
+ ˆσj( ˆU ˆ
857
+ Hsim) ≡ trFS( ˆU ˆ
858
+ Hsim [|n⟩⟨n| � ˆσj] ˆU †
859
+ ˆ
860
+ Hsim) projects the
861
+ unitary matrix generated by the time evolution of the Hamil-
862
+ tonian used for the simulations ˆU ˆ
863
+ Hsim on the Fock state |n⟩
864
+ and on a d-dimensional representation Pauli matrices.
865
+ [S1] R. J. Spreeuw, Phys. Rev. Lett. 125, 233201 (2020).
866
+ [S2] M. A. Nielsen, Physics Letters A 303, 249 (2002).
867
+
AdE3T4oBgHgl3EQfsgtu/content/tmp_files/load_file.txt ADDED
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+ page_content=' Safavi-Naini2, 3 1Van der Waals-Zeeman Institute, Institute of Physics, University of Amsterdam, 1098 XH Amsterdam, Netherlands 2QuSoft, Science Park 123, 1098 XG Amsterdam, the Netherlands 3Institute for Theoretical Physics, Institute of Physics, University of Amsterdam, Science Park 904, 1098 XH Amsterdam, the Netherlands (Dated: January 13, 2023) We consider the implementation of quantum logic gates in trapped ions using tightly focused optical tweezers.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Strong polarization gradients near the tweezer focus lead to qubit-state dependent forces on the ion.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We show that these may be used to implement quantum logic gates on pairs of ion qubits in a crystal.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
11
+ page_content=' The qubit-state dependent forces generated by this effect live on the plane perpendicular to the direction of propagation of the laser beams opening new ways of coupling to motional modes of an ion crystal.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The proposed gate does not require ground state cooling of the ions and does not rely on the Lamb-Dicke approximation, although the waist of the tightly focused beam needs to be comparable with its wavelength in order to achieve the needed field curvature.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Furthermore, the gate can be performed on both ground state and magnetic field insensitive clock state qubits without the need for counter-propagating laser fields.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This simplifies the setup and eliminates errors due to phase instabilities between the gate laser beams.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Finally, we show that imperfections in the gate execution, in particular pointing errors < 30 nm in the tweezers reduce the gate fidelity from F ≳ 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='99998 to ≳ 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='999.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Trapped ions are one of the most mature platforms for the implementation of quantum computing and quantum logic gates have been implemented with very high fidelity in these systems [1, 2].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Usually, the quantum logic gates in trapped ions rely on state-dependent forces applied to the ions by laser fields or magnetic fields.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The exchange of motional quanta between the ions then leads to effective qubit-qubit in- teractions.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Several recent works have explored how the use of state-of-the-art optical tweezer technology can benefit the trapped ion quantum computer.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Optical tweezers can be used to confine atoms very strongly by inducing a dipole in them and find application in neutral atomic quantum simulators, in which tweezers are used to levitate individual atoms [3–7].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In trapped ions, tweezers may be used to tune the soundwave spectrum in the ion crystal and thereby to program the inter- actions between the qubits [8–10].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Furthermore, in a recent work [11] we have proposed combining state-dependent opti- cal tweezers with oscillating electric fields to build a universal trapped ion quantum computer with extremely long-ranged in- teractions between the qubits.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In this work, we consider another scenario, in which we make use of the strong polarization gradients that occur in op- tical tweezers.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We note that strong gradients in optical po- tentials have been previously investigated to implement two- qubit gates without the need for ground-state cooling [12– 14].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' However, our approach utilizes the state-dependent dis- placement of the tweezer potential due to polarization gradi- ents [15–17].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We propose to use this optical analogue of the Magnus effect to implement quantum logic gates in trapped ions.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Setup – We consider linearly x-polarized, Gaussian tweez- ers, pointing in the −y direction and tightly focused at two qubits between which we wish to implement a quantum logic gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The quantum computing platform here considered is a linear crystal of N alkali-like trapped ions of mass m.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In the focal plane the ions experience a strong polarization gradient along the x direction, such that the polarization is linear (x) in the center and circular (σ±)z in the wings of the Gaussian.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' b) a) ⃗y ⃗x ⃗z mj P1/2 −1/2 +1/2 |0⟩ |1⟩ Ω− S1/2 Ω+ nX+ + + + + + + + −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 z/λ (σ−)z −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 (σ+)z −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 z/λ (σ−)z −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 (σ+)z Laguerre-Gaussian Gaussian FIG.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Schematic representation of the two-qubit gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' a) We apply tweezers propagating along the −y direction on the two ions forming the gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The tweezer intensity can be decomposed into three polar- ization components.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' b) Simplified level scheme of an alkaline-earth like ion without nuclear spin showing the encoding of the qubit in its Zeeman ground states.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The two polarization components of the tweezer couple to different states in the P1/2 manifold with detuning ∆.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This causes the minima of the tweezer potentials to be shifted by an amount ±λ depending on the qubit state.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Bottom : main polar- ization components for a Gaussian and Laguerre-Gaussian (l = 1, n = 0) tightly focused tweezer.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' A direct calculation [18] decomposing the field in the focal plane into its circular components (σ±)z (and πz) shows that, to a good approximation, the circular components are near- Gaussian distributions, displaced in opposite directions along the x axis.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We depict this setup in Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Note that the circu- lar components rotate in the xy plane, i.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='e.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' a plane containing the k vector of the light.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' As shown in Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' 1, the (σ±)z com- ponent is displaced by an amount ±λ ≡ ±λ/2π, with λ the arXiv:2301.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='04668v1 [quant-ph] 11 Jan 2023 2 tweezer wavelength.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' As the total field is the superposition of two displaced Gaussians, its intensity is slightly elongated along x.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Hollow tweezers (Gaussian-Laguerre) can be used instead of Gaussian ones.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This will provide the needed field curvature while keeping near-zero intensity at the center of the beam, drastically reducing the probability of off-resonant scattering that might limit the gate fidelity.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' For simplicity, we first consider ions without nuclear spin, such as 40Ca+, 88Sr+, 138Ba+ and 174Yb+.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The qubits are encoded in the electronic ground states 2S1/2 and |0⟩ = |j = 1/2, mj = 1/2⟩ and |1⟩ = |j = 1/2, mj = −1/2⟩ with j the total electronic angular momentum and mj its projec- tion on the quantization axis.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The magnetic field lies along the z-direction and the tweezers are polarized along the x- direction, such that the ions experience linearly polarized laser light.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The direction along the x-axis is the long direction of the ion trap, with trap frequency ωx.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The motion of the ions along the x-direction can be described by collective modes of harmonic motion with frequencies ωm and mode vectors bi,m, with m labeling the mode and i the ion [19].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We choose the detuning between the tweezers and the D1 transition to be large enough to avoid photon scattering, but much smaller than the spin-orbit coupling splitting of the 2P state.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In this way, we can neglect coupling to the P3/2 state.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In what follows we will show that this requirement can be satisfied experimentally.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Close to the center of the tweezer, strong polarization gradients appear and as a result, the two qubit states experience slightly different tweezer potentials.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In particular, as we show in Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' 1(a), the optical Magnus effect causes each qubit state to experience a tweezer potential that is offset from the apparent center of the tweezer by ∼ λ [16].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Hence, we may approximate the tweezer potential as : ˆU(x) = −U0 exp � −2(ˆx + ˆσzλ)2/w2 0 � (1) ≈ − ˜U0 + 1 2mω2 twˆx2 + gx ˆσz (2) with ωtw = � 4 ˜U0(w2 0 − 4λ2)/(mw4 0), g = 4 ˜U0λ/w2 0, and ˜U0 = U0 exp(−2λ2/w2 0) ≈ U0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Here U0 is the tweezer po- tential in the center and the beam waist is w0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Our approxima- tion replaces the tweezer potential with a harmonic potential and is valid for w0 ≫ lm, with lm = � ℏ/2mωm.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The last term in U(x) is the result of the spin-dependent force g cou- pling the internal state of the qubit, ˆσz, to its motion ˆx.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Thus, the optical Magnus effect allows us to straightforwardly im- plement a quantum gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Tweezer Hamiltonian – In the interaction picture with re- spect to ˆH0 = ℏωmˆa† mˆam the tweezer Hamiltonian on ions i and j is: ˆH1 = A(t) �1 2mω2 tw � ˆx2 i + ˆx2 j � + g � ˆσ(i) z ˆxi + ˆσ(j) z ˆxj �� .' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' (3) Here, ˆxi = � m lmbim � ˆame−iωmt + ˆa† meiωmt� is the posi- tion operator of ion i in the interaction picture, with ˆa† m the creation operator for the mode m, and 0 ≤ A(t) ≤ 1 speci- fies the time-dependence of the tweezer intensity.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The qubit- state independent terms in ˆH1 do not alter the dynamics of the quantum gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We ignore these terms and arrive at: ˆH2 = A(t)g � ˆxiˆσ(i) z + ˆxjˆσ(j) z � , (4) which takes the form of a spin-phonon coupling Hamilto- nian reminiscent of the Mølmer-Sørenson scheme for phonon- mediated quantum gates in trapped ions [20].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' However, at this stage we still have various choices available for A(t), depend- ing on which type of quantum gate we would like to imple- ment.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' For instance, pulsed A(t) could be used to perform fast gates.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Here, we choose A(t) to obtain a geometric phase gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' For this, we set 2A(t) = 1−cos(νt+φ) where φ = 0 assures a smooth ramp of the tweezer intensity and ν = ωc + δ with the subscript c denoting the center-of-mass (c.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='o.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='m.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=') mode for which ωc = ωx and bi,c = 1/ √ N.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We write the operators ˆxi and ˆxj in terms of ˆac and ˆa† c and perform the rotating wave approximation to arrive at: ˆH3 = glc 4 √ N � ˆaceiδt + ˆa† ce−iδt� � ˆσ(i) z + ˆσ(j) z � .' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' (5) To derive the qubit-qubit interactions forming the geomet- ric phase gate, we perform a unitary transformation ˆU1 = e−iδˆa† c ˆact to eliminate the time dependence, followed by a Lang-Firsov [21] transformation, ˆU2 = exp � ˆα � ˆa† c − ˆac �� with ˆα = − ˜g δ � ˆσ(i) z + ˆσ(j) z � .' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Disregarding qubit-independent terms, we obtain Heff = 2˜g2 ℏδ ˆσ(i) z ˆσ(j) z , (6) with ˜g = glc/(4 √ N) = ˜η ˜U0, with the proportionality factor ˜η = λlc/( √ Nw2 0).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This Hamiltonian generates qubit-qubit interactions that can be used to implement a geometric phase gate by setting the gate time τ = 2π/δ and ˜g2τ ℏ2δ = π/4.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Characterization of the gate – We analyse the gate dynam- ics by performing numerical simulation of the full dynamics generated by the Hamiltonian ˆHsim = ˆH0 + ˆU (xi) + ˆU (xj) for a two dimensional ion crystal where the tweezers po- tentials ˆU (xi;' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='j) on ions i and j have been expanded up to fourth-order including spin-independent terms.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We use real- istic experimental parameters: ∼ 156 µW of tweezer laser power focused to a waist of w0 ∼ 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='5 µm and tuned 15 THz to the red from the 2S1/2 → 2P1/2 transition in 174Yb+ (λ = 369.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='5 nm).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This results in ˜U0/h ∼ 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='6 MHz, ˜g/h = 2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='1 kHz/ √ N, and setting δ = 2π × 12.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='2 kHz/ √ N the gate time for the geometric phase gate is τ = 170 √ Nµs.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' With a calculated qubit-state independent tweezer potential of ωtw ∼ 2π × 37 kHz, the center-of-mass mode frequency (ωc/2π ∼ 1 MHz) is shifted by ∼ 2ω2 tw/ωcN ∼ 2π × 710/N Hz.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
94
+ page_content=' This shift can easily be taken into account by correcting δ accordingly.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
95
+ page_content=' In these estimates, we neglected the contribu- tion from other dipole allowed transitions, that are detuned by ∼ 66 THz (the relatively weak 2S1/2 → 3[3/2]3/2 transition) and 115 THz (the strong D2 line) or more.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
96
+ page_content=' We consider the gate unitary with a spin-echo sequence given by U(0, τ) = X⊗2U(τ/2, τ)X⊗2U(0, τ/2), where 3 FIG.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
97
+ page_content=' 2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
98
+ page_content=' We calculate the gate fidelity for a ground state cooled ion ¯nc, ¯ns = 0 (blue), sub-Doppler cooled thermal state with ¯nc = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
99
+ page_content='62, ¯ns = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
100
+ page_content='23 (orange) and ¯nc = 15, ¯ns = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
101
+ page_content='23 (red, using in this case a Fock cutoff nc ≤ 120, ns ≤ 10).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
102
+ page_content=' (a) Process fidelity of the two-qubit Magnus gate for different gate times.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
103
+ page_content=' (b) Effects of misalignment ϵ (orange) and intensity noise Λ1/τ (blue) on the gate fidelity.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
104
+ page_content=' The size of each intensity noise data point represents the standard deviation of 20 simulation where we generated a random Gaussian noise with σ = Λ1/τ on each of the two pulses.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
105
+ page_content=' This implies a noise on the laser intensity at frequency 1/τ that can not be removed by the spin-echo sequence.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
106
+ page_content=' X⊗2 is a qubit flip on both qubits.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
107
+ page_content=' This spin echo sequence is needed in order to remove local rotations on the qubits states and possible timing errors.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
108
+ page_content=' We calculate the unitary time evo- lution operator U(0, τ) for a system of two ions with their motional c.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
109
+ page_content='o.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
110
+ page_content='m.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
111
+ page_content=' and stretch modes and truncate their respec- tive Hilbert spaces to nc ≤ 18 and ns ≤ 10.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
112
+ page_content=' In figure 2 we show the process fidelity of the gate assuming the ions are in their motional ground state (¯n = 0) as a function of gate time.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
113
+ page_content=' The gate fidelity of F = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
114
+ page_content='999988 with nc = ns = 0 rivals the current standard approaches.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
115
+ page_content=' Moreover, the performance of our gate is robust to the thermal occupation of the motional modes.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
116
+ page_content=' We characterize the gate performance in presence of thermal phonons using the average gate fidelity [18, 22] and find that it depends weakly on the motional state of the two ions.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
117
+ page_content=' In fact, using ¯nc = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
118
+ page_content='62, ¯ns = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
119
+ page_content='23, the fidelity is almost unaltered at Fth = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
120
+ page_content='999989.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
121
+ page_content=' One of main experimental challenges is perfect tweezer alignment.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
122
+ page_content=' We have studied the resilience of the gate against misalignment of the tweezer in the x-direction, which we denote by ϵ.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
123
+ page_content=' In the presence of misalignment, ˜U0 → |0⟩ |1⟩ ∆ mF −1 0 +1 171Yb+ FIG.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
124
+ page_content=' 3.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
125
+ page_content=' Relevant energy levels of 171Yb+ for implementing the gate on hyperfine qubit splitted by ωq.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
126
+ page_content=' The coupling can be achieved using a pair of Raman beams detuned from the upper state 2P1/2 by ∆.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
127
+ page_content=' In the brackets are the angular contributions to the various dipole transition elements.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
128
+ page_content=' TABLE I.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
129
+ page_content=' Main sources of gate errors.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
130
+ page_content=' We estimate γph as the prob- ability of a off-resonant scattering in for 174Yb+ during the gate time (τ = 240 µs) for a Gaussian and Laguerre-Gaussian beams.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
131
+ page_content=' Other typical sources of errors are misalignment (ϵ), tweezer intensity noise (Λ1/τ) and timing (∆τ).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
132
+ page_content=' The values here reported are for laser pa- rameters used in our numerical simulations.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
133
+ page_content=' Error source γph Gaussian γph Laguerre-Gaussian ϵ 30 nm Λ1/τ 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
134
+ page_content='5% ∆τ ±5 µs 1 − F 2 × 10−3 10−6 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
135
+ page_content='3 × 10−3 9.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
136
+ page_content='3 × 10−5 2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
137
+ page_content='7 × 10−4 U0 exp−2(ϵ+ˆσzλ)2/ω2 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
138
+ page_content=' Thus, the misalignment has two ef- fects: (i) it changes the tweezer potential at the center of the tweezer and therefore the phase accumulation in the phase gate, and (ii) it shifts the potential in a qubit-state-dependent way.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
139
+ page_content=' The second contribution is corrected to lowest order by a spin-echo sequence.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
140
+ page_content=' Figure 2(b) shows the infidelity as a function of ϵ.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
141
+ page_content=' Here we assume that the tweezers are mis- aligned on both ions in the same way which seems the experi- mentally most likely case.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The unitary U(0, τ) leads to phase space trajectories for ⟨x(t)⟩ and ⟨px(t)⟩ associated with the c.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
143
+ page_content='o.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
144
+ page_content='m.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
145
+ page_content=' motion[18].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' As expected, we find approximately cir- cular phase-space orbits for the even parity states |00⟩, |11⟩, and very little motion for the odd parity ones.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
147
+ page_content=' We see that ev- ery state combination leads to ion motion, but the difference in motion still leads to a high fidelity of ≳ 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='999 as shown in Figure 2(b).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Clock state case – While the calculation was performed for the electron spin qubit states in 174Yb+, it should also be possible to use the hyperfine clock states |F = mF = 0⟩ and |F = 1, mF = 0⟩ in 171Yb+.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This qubit is insensitive to magnetic field noise and coherence times of up to an hour have been measured [23].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
151
+ page_content=' In this case, the tweezers are formed by a bichromatic co-propagating laser field detuned by ∆ from the D1 transition at 369.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
152
+ page_content='5 nm with overall detuning ∆ ≪ ωFS, the fine structure splitting.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
153
+ page_content=' We set the frequency difference in the 4 bichromatic tweezer to 12.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
154
+ page_content='6 GHz, corresponding to the tran- sition between the qubit states [24].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
155
+ page_content=' The tweezer laser then causes Raman coupling between the qubit states via two dis- tinct paths.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In the first path, the qubits are coupled via the state |P1/2, F = 1, mF = −1⟩ due to the σ− polarization compo- nent in the tweezer.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
157
+ page_content=' In the other, the qubits are coupled via the state |P1/2, F = 1, mF = +1⟩ due to the σ+ component in the tweezer.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' We denote the Rabi frequencies of each path as Ω± 1,2(x).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The corresponding Raman couplings of each path interfere destructively in the center of the tweezer due to a rel- ative minus sign between Ω+ 1 (x) and Ω+ 2 (x) in their Clebsch- Gordan coefficient, ∝ (Ω− 1 (0)Ω− 2 (0)+Ω+ 1 (0)Ω+ 2 (0))/∆ = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' However, the Magnus effect causes a strong position depen- dence of the relative strength of both paths of magnitude Ωeff(x) = Ω− 1 (x)Ω− 2 (x) ∆ + Ω+ 1 (x)Ω+ 2 (x) ∆ ≈ Ω2 ∆ 4λx w2 0 , (7) where we assumed x ≪ λ ≪ w0 and |Ω± i (0)| = Ω/ √ 2 with i = 1, 2, such that both laser frequencies have the same power.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' As a result, a qubit state-dependent force appears as in Eq.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
162
+ page_content=' (4), except that we must now replace ˆσ(i,j) z → ˆσ(i,j) x and the gate takes the form of the usual Mølmer-Sørensen interaction ∝ ˆσ(i) x ˆσ(j) x [20].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Amplitude modulation via A(t) allows again for resonant enhancement of the gate.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In addition to the Raman coupling, we obtain a tweezer po- tential (AC Stark shift) for each qubit state of magnitude δ|k⟩ AC(x) = � i=1,2 � j=+,− |Ωj i(x)|2 ∆i,|k⟩ (8) with ∆1,|0⟩ = ∆ − ωq, ∆2,|0⟩ = ∆, ∆1,|1⟩ = ∆ and ∆2,|1⟩ = ∆ + ωq.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This causes an additional trapping potential Φ(x) ≈ 1 2mω2 twx2 that is independent of the qubit state as before, as well as a position-dependent differential Stark shift δAC(x) = δ|1⟩ AC(x) − δ|0⟩ AC(x).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' In the limit ωq ≪ |∆|, δAC(x) ≈ − ωq ∆2 � i=1,2 � j=+,− |Ωj i(x)|2 (9) = −ωq ∆ ˜U0(x) (10) This differential Stark shift is estimated to be small, δAC/2π ≈ 2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
167
+ page_content='7 kHz for the numbers used in the simulations, and can be compensated by a corresponding Raman detuning.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Photon scattering on the D1 transition can be estimated as γph ∼ ˜U0Γ/(ℏ∆) ∼ 13 s−1 with Γ = 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='23 × 108 s−1 in Yb+.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' This adverse effect may be reduced significantly by em- ploying hollow tweezers [11, 25, 26] at the expense of added complexity.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' For a hollow beam with a waist w0 = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content='5 µm and ∼ 160 µW we obtain a reduction in scattering rate of ∼ 10−6 s−1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' As long as ωtw ≪ Ωrf, the drive frequency of the Paul trap, no parametric excitations can occur and micromo- tion of the ions is not a problem.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Other errors, such as due to intensity noise of the laser, heating of the ions due to electric field noise and decoherence due to magnetic field noise have the same effect as in other gate implementations.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Finally, we note that because the tweezers are far detuned from the closest transitions, the exact overall frequency of the tweezer laser is irrelevant.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Conclusions In conclusion, we have described a novel type of quantum phase gate based on the optical Magnus ef- fect using optical tweezers in a linear chain of trapped ions.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The main benefit is that the gate does not require counter- propagating laser fields, greatly simplifying the setup and eliminating errors due to phase instabilities between the gate laser beams.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Furthermore, the state-dependent force gener- ated by the Magnus effect allows to perform the gate by cou- pling to motional modes on the plane perpendicular to the di- rection of propagation of the tweezers allowing novel experi- mental implementations.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The proposed gate does not require ground state cooling and can perform a quantum logic gate on any pair of ion qubits by spatial addressing.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' The expected gate fidelity rivals the state of the art also for ions that are not cooled to the ground-state of motion.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' ACKNOWLEDGEMENTS This work was supported by the Netherlands Organiza- tion for Scientific Research (Grant Nos.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' 680.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
183
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184
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185
+ page_content='92.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
186
+ page_content='18.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
187
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188
+ page_content='G.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
189
+ page_content=').' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
190
+ page_content=' A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
191
+ page_content='S.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
192
+ page_content='N is supported by the Dutch Re- search Council (NWO/OCW), as part of the Quantum Soft- ware Consortium programme (project number 024.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
193
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194
+ page_content='037).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
195
+ page_content=' [1] C.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
196
+ page_content=' Ballance, T.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
197
+ page_content=' Harty, N.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
198
+ page_content=' Linke, M.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
199
+ page_content=' Sepiol, and D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
200
+ page_content=' Lucas, Phys.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
201
+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
202
+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
203
+ page_content=' 117, 060504 (2016).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
204
+ page_content=' [2] J.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
205
+ page_content=' Gaebler, T.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
206
+ page_content=' Tan, Y.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
207
+ page_content=' Lin, Y.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
208
+ page_content=' Wan, R.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
209
+ page_content=' Bowler, A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
210
+ page_content=' Keith, S.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
211
+ page_content=' Glancy, K.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
212
+ page_content=' Coakley, E.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
213
+ page_content=' Knill, D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
214
+ page_content=' Leibfried, and D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
215
+ page_content=' Wineland, Phys.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
216
+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
217
+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
218
+ page_content=' 117, 060505 (2016).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
219
+ page_content=' [3] D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
220
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221
+ page_content=' d.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
222
+ page_content=' Léséleuc, V.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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224
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228
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229
+ page_content=' Keesling, H.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
230
+ page_content=' Levine, E.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
231
+ page_content=' R.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
232
+ page_content=' Anschuetz, A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
233
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234
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235
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236
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237
+ page_content=' D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
238
+ page_content=' Lukin, Science 354, 1024 (2016).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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241
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242
+ page_content=' Kaufman, Phys.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
243
+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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247
+ page_content=' Keesling, G.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
248
+ page_content=' Semeghini, A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
249
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250
+ page_content=' T.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
251
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253
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254
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255
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+ page_content=' D.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
258
+ page_content=' Lukin, Phys.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
259
+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
260
+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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264
+ page_content=' Lahaye, Nature Physics 16, 132–142 (2020).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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267
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269
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+ page_content=' M.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Sieberer, PRX Quantum 1, 020316 (2020).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' H.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
275
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277
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278
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280
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284
+ page_content=' Arias Espinoza, M.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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288
+ page_content=' Schüssler, Z.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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291
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298
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299
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300
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+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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+ page_content=' J.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
423
+ page_content=' C.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
424
+ page_content=' Spreeuw,1, 2 and A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
425
+ page_content=' Safavi-Naini2, 3 1Van der Waals-Zeeman Institute, Institute of Physics, University of Amsterdam, 1098 XH Amsterdam, Netherlands 2QuSoft, Science Park 123, 1098 XG Amsterdam, the Netherlands 3Institute for Theoretical Physics, Institute of Physics, University of Amsterdam, Science Park 904, 1098 XH Amsterdam, the Netherlands (Dated: January 13, 2023) APPENDIX I : OPTICAL MAGNUS EFFECT A key characteristic of a tightly focused beam is the strong field curvature near the focus.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
426
+ page_content=' This not only affects the local intensity but also its polarization structure.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
427
+ page_content=' To calculate this, we take a superposition of plane waves labeled by their wave vector in spherical coordinates, k = (k, θ, φ).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
428
+ page_content=' Taking k = ω/c as fixed we write E(r) ∝ � 2π 0 dφ � π 0 dθ sin θ ux(θ, φ) a(θ, φ) eik·r with ux(θ, φ) a polarization vector obtained by co-rotating the x unit vector when k is rotated from z to (θ, φ), such that ux(θ, φ) �� k = 0, see also Ref.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
429
+ page_content=' [S1].' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
430
+ page_content=' In the calcula- tion we center the beam around θ = 0, and the focal plane is given by r = (x, y, 0).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
431
+ page_content=' The shape of the beam is de- termined by the amplitude function a(θ, φ).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
432
+ page_content=' For a Gaussian beam we set a(θ, φ) = exp(−θ2/w2 θ);' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
433
+ page_content=' for the lowest or- der (l = 1) Laguerre-Gaussian (LG) beam we set a(θ, φ) = θ exp(iφ − θ2/w2 θ).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
434
+ page_content=' After performing the above integral we rotate the results for tweezers propagating along the −y di- rection.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
435
+ page_content=' Finally, the circular field components σ± shown in Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
436
+ page_content=' 1 of the main text are obtained as the projection onto unit vectors (x ± iy)/ √ 2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
437
+ page_content=' In Figure S-1, all three polarization components for a Laguerre-Gaussian beam are shown.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
438
+ page_content=' Note that the σ− and σ+ components have similar intensity while the π-polarization is suppressed by a factor ∼ 100.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
439
+ page_content=' −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 z/λ (σ−)z −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 (π)z −6 −4 −2 0 2 4 6 x/λ −4 −2 0 2 4 (σ+)z FIG.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
440
+ page_content=' S-1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
441
+ page_content=' Intensity of the polarization components for a LG beam calculated at the focus.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
442
+ page_content=' The π-polarization component has been en- hanced by a factor 100 to make it visible.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
443
+ page_content=' Here we set wθ = 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
444
+ page_content='6 APPENDIX II : PHASE-SPACE DYNAMICS We study the phase-space dynamics of the ions by simulat- ing the time dependent Hamiltonian using trotterization with time-steps of 10−4 τ.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
445
+ page_content=' At each time-step we evaluate the ex- pectation value of the ⟨ˆx⟩ and ⟨ˆp⟩ for the center of mass mode.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
446
+ page_content=' As expected, we find approximately circular phase-space or- bits for the even parity states |00⟩, |11⟩, and very little motion for the odd parity ones.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
447
+ page_content=' In Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
448
+ page_content=' S-2 it is possible to see the evo- lution in phase-space for all the four spin states in case of per- fectly aligned and slightly misaligned tweezers.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
449
+ page_content=' As described in the main text we simulate numerically the full Hamiltonian defined as ˆHsim = ˆH0 + ˆU (xi) + ˆU (xj) where in case of misalignment ϵ,' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
450
+ page_content=' ˆU (x) reads as : U(x) ≈ −U0 e−2((ˆx−ˆϵ)+ˆσzλ)2/w2 0 ≈ − ˜U0 + 4 ˜U0 ˆσzλ − ˆϵ w2 0 ˆx + 1 2 ˜U0 � 4 � w2 0 − 4λ2� w4 0 � ˆx2 − 1 2 ˜U0 � 16 � ˆϵ2 − 2ˆσzˆϵλ � w4 0 � ˆx2 − � 8 ˜U0ˆσzλ3w2 0 − 4 � 3ˆϵ2 + λ2� 3w6 0 � ˆx3 + � 8 ˜U0ˆϵ3w2 0 − 4 � ˆϵ2 + 3λ2� 3w6 0 � ˆx3 − � 2 ˜U0ˆσzλˆϵ−48w2 0 + 64 � ˆϵ2 + λ2� 3w8 0 � ˆx4 + � 2 ˜U0 3w4 0 − 24w2 0 � ˆϵ2 + λ2� + 16 � ˆϵ4 + 6ˆϵ2λ2 + λ4� 3w8 0 � ˆx4.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
451
+ page_content=' with ˜U0 = U0e−2(ˆϵ+ˆσzλ)2/w2 0 A small tweezer misalignment ϵ gives rise to new spin- dependent terms in the Hamiltonian that shift the trapping po- tential in a state dependent way.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
452
+ page_content=' In Fig.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
453
+ page_content='S-2 is shown how the dynamics is affected in the case where the tweezers are mis- aligned by 30 nm.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
454
+ page_content=' APPENDIX III : GATE FIDELITY We characterize the gate by calculating the average process fidelity as follows : [S2]: ¯F( ˆUid, ˆU ˆ Hsim) = � j tr � ˆUidˆσ† j ˆU † idˆσj( ˆU ˆ Hsim) � + d2 d2 (d + 1) , 2 −1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
455
+ page_content='4 −0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
456
+ page_content='7 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
457
+ page_content='0 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
458
+ page_content='7 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
459
+ page_content='4 ⟨ˆx⟩ −1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
460
+ page_content='4 −0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
461
+ page_content='7 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
462
+ page_content='0 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
463
+ page_content='7 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
464
+ page_content='4 ⟨ˆpx⟩ ϵ = 0 −2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
465
+ page_content='1 −1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
466
+ page_content='4 −0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
467
+ page_content='7 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
468
+ page_content='0 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
469
+ page_content='7 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
470
+ page_content='4 ⟨ˆx⟩ −1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
471
+ page_content='4 −0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
472
+ page_content='7 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
473
+ page_content='0 0.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
474
+ page_content='7 1.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
475
+ page_content='4 ⟨ˆpx⟩ ϵ = 30 nm ψ↑↑ ψ↓↑ ψ↑↓ ψ↓↓ FIG.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
476
+ page_content=' S-2.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
477
+ page_content=' Center of mass mode phase-space dynamics for perfectly aligned tweezer (left) and for 30 nm misaligned ones (right).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
478
+ page_content=' For the simulation we used the same parameters as for τ/2 = 120 µs point in Figure 1(a) of the main text.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
479
+ page_content=' where ˆUid is the unitary of an ideal geometric phase gate and ˆσj( ˆU ˆ Hsim) ≡ trFS( ˆU ˆ Hsim [|n⟩⟨n| � ˆσj] ˆU † ˆ Hsim) projects the unitary matrix generated by the time evolution of the Hamil- tonian used for the simulations ˆU ˆ Hsim on the Fock state |n⟩ and on a d-dimensional representation Pauli matrices.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
480
+ page_content=' [S1] R.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
481
+ page_content=' J.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
482
+ page_content=' Spreeuw, Phys.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
483
+ page_content=' Rev.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
484
+ page_content=' Lett.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
485
+ page_content=' 125, 233201 (2020).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
486
+ page_content=' [S2] M.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
487
+ page_content=' A.' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
488
+ page_content=' Nielsen, Physics Letters A 303, 249 (2002).' metadata={'source': '/home/zjlab/wf/langchain-ChatGLM/knowledge_base/AdE3T4oBgHgl3EQfsgtu/content/2301.04668v1.pdf'}
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1
+ Cinematic Techniques in Narrative Visualization
2
+ Matthew Conlen
3
+ Our World in Data
4
5
+ Jeffrey Heer
6
+ University of Washington
7
8
+ Hillary Mushkin
9
+ California Institute of Technology
10
11
+ Scott Davidoff
12
+ Jet Propulsion Laboratory
13
+ California Institute of Technology
14
15
+ ABSTRACT
16
+ The many genres of narrative visualization (e.g. data comics, data
17
+ videos) each offer a unique set of affordances and constraints. To
18
+ better understand a genre that we call cinematic visualizations—3D
19
+ visualizations that make highly deliberate use of a camera to convey
20
+ a narrative—we gathered 50 examples and analyzed their traditional
21
+ cinematic aspects to identify the benefits and limitations of the form.
22
+ While the cinematic visualization approach can violate traditional
23
+ rules of visualization, we find that through careful control of the
24
+ camera, cinematic visualizations enable immersion in data-driven,
25
+ anthropocentric environments, and can naturally incorporate in-
26
+ situ narrators, concrete scales, and visual analogies. Our analysis
27
+ guides our design of a series of cinematic visualizations, created for
28
+ NASA’s Earth Science Communications team. We present one as a
29
+ case study to convey design guidelines covering cinematography,
30
+ lighting, set design, and sound, and discuss challenges in creating
31
+ cinematic visualizations.
32
+ 1
33
+ INTRODUCTION
34
+ Within narrative visualization [57], researchers have identified gen-
35
+ res (such as data comics [3] and data videos [1]) that help better
36
+ unpack and situate their specific application and the features that
37
+ they employ. cinematic visualizations embed data into a three-
38
+ dimensional, time varying scene, utilizing one or more cameras to
39
+ direct the relationship between a viewer and the scene to tell a dra-
40
+ matic data-driven story. This cinematic approach is different from
41
+ the one typically used in information visualization, where graph-
42
+ ics are reduced to a minimal form, incorporating only essential
43
+ elements like axes and data-driven marks [64]. Cinematic visual-
44
+ izations are more maximal: non-data marks are not compressed or
45
+ reduced, instead entire digital worlds are built up around data points
46
+ and included in the visible frame. This technique allows viewers
47
+ to feel present in locations augmented with data-bound objects,
48
+ known as data visceralizations [41]. Narrative documentary visual-
49
+ izations [10] can be produced through the careful editorial direction
50
+ of the cinematography, editing, mise-en-scène, and sound [5].
51
+ Through an analysis of 50 existing cinematic visualizations, we
52
+ identified four salient techniques (in-situ narrators, resolution of
53
+ scale, anthropocentric perspective, and story-driven cameras) that
54
+ cinematic visualizations employ to dramatically engage their au-
55
+ dience through emotionally resonant data-stories. We show how
56
+ these techniques are used throughout the examples analyzed, dis-
57
+ cuss constraints associated with them, and reason about why cine-
58
+ matic visualizations may be effective despite the known pitfalls of
59
+ 3D visualization.
60
+ Using the lessons learned from this formal analysis, we produced
61
+ a web-based article containing a series of cinematic visualizations
62
+ relating to climate change, which was published by NASA’s Earth
63
+ Science Communications team 1. We contribute the design process
64
+ for one of these visualizations as a case study, presenting design
65
+ artifacts that were created during our process (both successful
66
+ and unsuccessful), and provide concrete guidelines for designers
67
+ of cinematic visualizations. Our analysis and design artifacts are
68
+ available at https://cinematic-visualization.github.io/.
69
+ 2
70
+ RELATED WORK
71
+ Narrative visualizations are used to improve memorability [7, 8],
72
+ to instill empathy or emotion [9], to frame a message [33], and to
73
+ improve engagement [19, 28]. Segel & Heer [57] provided an ini-
74
+ tial characterization of the design space of narrative visualizations,
75
+ which was later elaborated to include additional techniques [60].
76
+ Hullman et al. [34] focused on the role of sequence in narrative
77
+ visualization, characterizing a set of transition types and other high
78
+ level strategies for sequencing visualizations. Tools have been cre-
79
+ ated to support narrative visualization authoring [2, 11, 18, 56], and
80
+ a small number of empirical evaluations of narrative visualizations
81
+ have been conducted [9, 19, 46, 69]. Further work has investigated
82
+ specific genres of narrative visualization such as data comics [3],
83
+ and new genres have emerged beyond Segel & Heer’s initial set,
84
+ such as “scrollytelling.” Here we add to the ongoing conversation
85
+ around narrative visualization by identifying another such genre:
86
+ cinematic visualization. Kosara & McKinley [39] identified the op-
87
+ portunity for narrative visualization researchers to learn from other
88
+ disciplines that engaged heavily with storytelling and multimedia,
89
+ this paper draws on film art scholarship, incorporates a formal
90
+ system of cinematic style into our analysis, discussion, and design
91
+ of cinematic visualizations.
92
+ 2.1
93
+ Data Videos & VR
94
+ Data videos were included in the initial set of genres put forth by
95
+ Segel & Heer [57] and first studied closely by Amini et al. [1]. Not
96
+ all data videos are cinematic visualizations (for example, we do
97
+ not consider a video consisting of a sequence of two-dimensional
98
+ infographics to be cinematic), and not all cinematic visualizations
99
+ 1https://climate.nasa.gov/news/2933/visualizing-the-quantities-of-climate-change/
100
+ arXiv:2301.03109v1 [cs.HC] 8 Jan 2023
101
+
102
+ , ,
103
+ Conlen, et al.
104
+ Figure 1: The Dangers of Storm Surge (CV42) is a mixed reality video produced by the Weather Channel. The video opens with
105
+ a close up shot of a news anchor wearing a rain jacket, standing in front of a house (1A). There are audible sounds of rain
106
+ under the anchor’s voice and water dripping down the windows of the house. The camera pulls back revealing that the live
107
+ anchor is being composited into a 3D scene of a suburban neighborhood during a storm surge (1B). There are very few data
108
+ points actually encoded as visual elements. The piece simply shows water rising from zero, to three, to six, to nine feet (1C-D)
109
+ as the anchor narrates with details in reference to the danger of storm surge associated with hurricanes.
110
+ are data videos (for example one in which the visualization is deeply
111
+ tied to the text of an interactive news article). While Amini et al.
112
+ were primarily concerned with the narrative structure and attention
113
+ cues of data videos, we additionally consider the visual and auditory
114
+ style of cinematic visualizations in detail. Under our formal style
115
+ system, our analysis of editing is most closely related to Amini’s
116
+ work, however that is only one of four dimensions we consider.
117
+ Bradbury & Guadagno [10] studied viewer preferences in docu-
118
+ mentary narrative visualization (a subgenre of data videos in which
119
+ data is presented using the techniques of documentary film), and
120
+ found that audiences may prefer when documentary data videos
121
+ include voice-over narration and on-screen narrators. We build on
122
+ their analysis of the use of narrators and narration, in particular
123
+ during our discussions of in-situ narrators that interact with data-
124
+ bound objects digitally rendered into the space around them, and
125
+ of the use of sound in cinematic visualizations. Video producers
126
+ have extended the traditional documentary visualization format to
127
+ enable interactivity such as user selected paths through the content
128
+ and manipulable graphics [29, 63].
129
+ Immersive data stories [35] have been discussed within the
130
+ emerging field of immersive analytics [44] and have been shown
131
+ to allow viewers to examine data at multiple scales, support im-
132
+ mersive exploration, and create affective personal experiences with
133
+ data [36]. Lee et al. [41] introduced data visceralizations, where
134
+ physical quantities are visualized in 3D virtual reality scenes. This
135
+ paper helps to bridge the gap between data visceralization and nar-
136
+ rative visualization by showing how cinematic techniques can be
137
+ used to create author-guided narrative visualizations using data vis-
138
+ ceralizations. Cinematic visualizations similarly attempt to immerse
139
+ viewers and create emotionally resonant experiences, although in
140
+ contrast to immersive visualizations they are typically viewed on a
141
+ standard 2D screen with limited (or no) user control of the camera.
142
+ There are several toolkits for creating immersive data visualizations
143
+ and data stories on augmented reality devices [21, 55, 59].
144
+ 2.2
145
+ 3D Computer Graphics
146
+ Animation [62] has been a partner discipline with visualization for
147
+ some time. Classic principles of animation [61] have been adapted
148
+ for digital usage [40] and subsequently for information visualiza-
149
+ tion [30]. With realistic camera models [38] and improving render-
150
+ ing capabilities [20] digital animation became a tool to create Holly-
151
+ wood films [31]. While 3D graphics have been used in visualization
152
+ to limited success, e.g., to display hierarchical information [17], the
153
+ use of 3D graphics in information visualization is often avoided.
154
+ A broad body of research documents potential pitfalls, including
155
+ that volume is not a perceptually effective encoding channel [16],
156
+ and that 3D projections introduce distortion and occlusion [67].
157
+ We find that designers of cinematic visualizations may intention-
158
+ ally use suboptimal encodings in support of more visceral [41] and
159
+ emotionally resonant [28] graphics.
160
+ The use of 3D does find more regular application in scientific visu-
161
+ alization [4, 65], including its use in storytelling [22, 43]. Borkiewicz
162
+ used the term cinematic scientific visualization [6] to refer to a class
163
+ of narrative data videos that focus on scientific data. Here we use
164
+ cinematic visualization in a similar way but do not restrict the data
165
+ to be strictly scientific or inherently spatial. Unlike Borkiewicz,
166
+ our description encapsulates visualizations which are not embed-
167
+ ded in films, but may be, for example, displayed as an animation
168
+ accompanying a news article.
169
+ 2.3
170
+ Film Art
171
+ Bordwell and Thompson [5] define narrative and style as the two
172
+ major formal systems of film. While prior work has examined se-
173
+ quence [34] and narrative structure & attention cues [1] in data
174
+ videos, we observe that cinematic style has far less visibility in the
175
+ critical vocabulary of data visualization. Style plays a crucial roll
176
+ in filmmaking, enabling directors to “confirm our expectations, or
177
+ modify them, or cheat, or challenge them. [...] A director directs
178
+ not only the cast and crew. A director also directs us, directs our
179
+ attention, shapes our reaction.” [5] This paper brings Bordwell and
180
+ Thompson’s formal system of cinematic style into the world of data
181
+ visualization, and uses it to examine how narrative visualizations
182
+ borrow techniques from cinema while departing from many of the
183
+ traditional practices advocated by visualization research.
184
+ Style consists of four features, which together make up a film’s
185
+ style, each now briefly described. Mise-en-scène refers to every-
186
+ thing that is seen in the frame, including lighting, actors, objects,
187
+ backdrops, and so on [27]. Cinematography refers to the use of the
188
+
189
+ Cinematic Techniques in Narrative Visualization
190
+ , ,
191
+ Figure 2: (A) In [REALISTIC] Elephant rocket fuel - Saturn V (CV29), a model Saturn V rocket takes off, however, instead of
192
+ flames exiting the bottom of the spacecraft, elephants are expelled, the number of elephants represents the corresponding
193
+ mass of fuel. This video may not make for a particularly effective visualization in terms of conveying precise quantities, but
194
+ the style successfully uses humor in order to call attention to the fact that rocket launches use a quantity of fuel so great
195
+ it is appropriate to measure it in terms of dozens of elephants. (B) In Here are 120 million Monopoly pieces, roughly one for
196
+ every household in the United States (CV6) by the New York Times the pile of Monopoly pieces is first seen from a far, before
197
+ the reader scrolls down the page to trigger the camera zooming in to the very top of the pile, dramatically revealing what a
198
+ disproportionately small portion of families provide most political funding.
199
+ camera, how shots are composed and framed [26]. By placing ele-
200
+ ments at specific locations within the frame, they can be perceived
201
+ either as the subject or the background of the image [25]. Editing
202
+ is the composition of multiple pieces of footage in time or space,
203
+ creating transitions between perspectives and scenes [54]. Sound
204
+ is the audio used, whether it be music, voice over, or sounds from
205
+ characters or objects on screen [32]. Our analysis of cinematic visu-
206
+ alization identified techniques along these dimensions of style that
207
+ designers can use to enhance their presentation of data narratives.
208
+ 3
209
+ CINEMATIC VISUALIZATION SURVEY
210
+ We collected cinematic visualization to analyze by surveying liter-
211
+ ature on narrative visualization [1, 6, 34, 35, 43, 57, 60], browsing
212
+ the information visualization awards website Information is Beau-
213
+ tiful [45] and the PacificVIS storytelling contest [50], and searching
214
+ for news articles, blog posts, conference talks, and videos which
215
+ were described using combinations of the keywords cinematic, data,
216
+ data video, dataviz, datavis, visualization, news, newsgames, immer-
217
+ sive, mixed reality, 3d, and video. We searched the portfolios of the
218
+ creators of the visualizations found initially and their collaborators.
219
+ A full list of the cinematic visualizations can be seen in Figure 7 in
220
+ the appendix of this paper; we refer to these studies by identifiers
221
+ throughout the paper (e.g., CV4 refers to the fourth example in the
222
+ table). Our analysis considered 50 cinematic visualizations. While
223
+ the corpus is not exhaustive, the examples expose the variety of
224
+ media (interactive news articles, YouTube videos, and TV segments)
225
+ which cinematic visualizations occupy and the messages that they
226
+ deliver. The examples visualized a broad range of data types, in-
227
+ cluding datasets both with and without physical and geographic
228
+ dimensions.
229
+ Rather than empirically evaluate specific design patterns utilized
230
+ in the visualizations, we turn to the means of understanding plot
231
+ devices [57], sequencing [1], and film style [5]. We analyzed the
232
+ style of each example along the dimensions of mise-en-scène, cine-
233
+ matography, editing, and sound using the 4-step analysis process
234
+ described by Bordwell and Thompson [5], a canonical method of
235
+ film analysis. For each example we first identified the main com-
236
+ municative goals of the visualizations, and then studied the salient
237
+ techniques applied within the mise-en-scène, cinematography, edit-
238
+ ing, and sound which supported these narrative goals. We then used
239
+ iterative coding to categorize the salient techniques used across
240
+ the examples. Usage of these techniques are shown in Figure 7, for
241
+ example we recorded many ways in which a viewer’s attention
242
+ is guided (through color, light, annotations, and narrators in the
243
+ mise-en-scène) and use of cinematographic techniques like point-
244
+ of-view perspective and user-controlled cameras. The table shows
245
+ that the medium of the cinematic visualization has some impact on
246
+ the techniques used, for example cinematic visualizations embed-
247
+ ded in online articles rarely use sound, but often utilize user-paced
248
+ segments, while those presented as videos make heavy use of sound.
249
+
250
+ A
251
+ B
252
+ Here are 120 million
253
+ Monopoly pieces, roughly
254
+ one for every household
255
+ in the United States.
256
+ Just 158 families have
257
+ provided nearly half of the
258
+ early money for efforts to
259
+ capture the White House., ,
260
+ Conlen, et al.
261
+ Figure 3: VFX Artist Reveals the True Scale of the Universe fea-
262
+ tures a live-action narrator alongside scaled-down 3D mod-
263
+ els of celestial bodies.
264
+ 3.1
265
+ Design Techniques
266
+ Through this analysis we identified salient recurring techniques that
267
+ were frequently applied to support the communicative goals of the
268
+ visualization, including the use of in-situ narrators, anthropocentric
269
+ perspective, resolution of scale, and story-driven cameras.
270
+ In-situ narrators mediate interactions with diegetic data.
271
+ Perhaps the most novel technique that we identified in cinematic
272
+ visualizations is the use of in-situ narrators, in which the mise-en-
273
+ scène contains a character that interacts directly with on-screen,
274
+ diegetic data.2 In contrast to traditional documentary visualization
275
+ narrators who might participate from off-screen (“voice of god”) or
276
+ refer to data visualizations rendered as two-dimensional holograms
277
+ or composited over top the video [10], in-situ narrators are under-
278
+ stood by the viewer to be able to see and interact with the diegetic
279
+ data either through the use of superimposed data visceralizations
280
+ 2Something which is diegetic exists in the same universe as the characters on screen; we
281
+ use the phrase diegetic data to refer to data-driven elements which are part of—rather
282
+ than composited over—the scene shown in the frame.
283
+ (CV35, 40, 42, 43) or, in one case, data physicalization [37] (CV41).
284
+ This (typically) mixed reality environment serves an important
285
+ role for narrative visualization, allowing the on-screen narrator to
286
+ mediate interactions between the audience and the graphics, letting
287
+ them provide additional context and push the storyline forward.
288
+ These narrators, essential components of the mise-en-scène, can
289
+ also help concretize a visualization’s anthropocentric perspective,
290
+ reinforcing the idea that data is being displayed at a human scale.
291
+ In The Dangers of Storm Surge (CV42), one exemplar of this
292
+ technique (Figure 1) produced by the Weather Channel, a news
293
+ anchor wearing a blue jacket explains the dangers associated with
294
+ flooding due to storm surge. The graphics are coordinated with
295
+ the narrator’s script and appear to respond to his dialogue, the
296
+ composition of the frame inviting comparison between the man and
297
+ the height of the water. The narrator is the primary subject from the
298
+ start of the clip, positioned centrally in frame and maintaining focus
299
+ due to visual cues like his bright blue coat, the circular platform
300
+ upon which he stands, and the shot composition. To call attention
301
+ to the water’s height at certain key moments, a brightly colored
302
+ annotation is projected onto the crest of the surge.
303
+ An anthropocentric perspective transports viewers and
304
+ enables drama. One notable aspect of cinema is how the camera is
305
+ able to transport the audience into the scene: people watching sus-
306
+ pend disbelief [24] to allow themselves to wholeheartedly imagine,
307
+ or “believe”, that they are in the scene, seeing things through the
308
+ camera lens. That is, the camera’s perspective becomes the viewer’s
309
+ point of view, they are one and the same. The height, angle, and
310
+ distance of a camera in relation to objects in the scene all play a role
311
+ in how a viewer will interpret and respond to the frame that they
312
+ ultimately see [5]. When a camera is placed high above a setting,
313
+ the viewer feels like they are also high above it. When a camera
314
+ is placed at eye level, a viewer feels as if they are standing there
315
+ watching the subject. For example, both CV1 and CV26 utilize unit
316
+ visualizations and concrete scales to visualize quantities in relation
317
+ to the size of Manhattan, but each uses perspective to impact the
318
+ viewer’s experience in a different way. In CV1 the data being dis-
319
+ played (plastic bottle usage) is not directly related to the locations
320
+ being used as concrete scale referents, and an overview shot is
321
+ used, letting the viewer absorb the scale of the data rather than
322
+ the details and textures of the city itself. In contrast, CV26 begins
323
+ with a shot from a camera placed at eye-level, looking at several
324
+ of the city’s ubiquitous yellow taxis, transporting viewers to the
325
+ city at street level, and forcing them to reckon with the data being
326
+ displayed (New York City’s annual green house gas emissions) in a
327
+ much more visceral way [41].
328
+ Some cinematic visualizations place the camera perspective
329
+ somewhere that is humanly impossible. However, if the audience
330
+ suspends disbelief, the camera can carry the viewer through these
331
+ otherwise inaccessible spaces, for example, CV12 shows an anima-
332
+ tion of the Cassini spacecraft as it orbited and eventually crashed
333
+ into Saturn. Choice and Chance (CV11), visualizes the events of the
334
+ 2016 Pulse night club shooting in Tampa Bay, positions a camera
335
+ looking “through” the roof of a nightclub. Because the scene is
336
+ shot using a digital model instead of a real location, the roof of the
337
+ club can simply be removed and problems of occlusion go away.
338
+ Changing perspectives can also shift the subject of the scene or
339
+ add emotional content, for example, when the camera moves to
340
+
341
+ A
342
+ SUBSCRIBE
343
+ B
344
+ c
345
+ Rige!Cinematic Techniques in Narrative Visualization
346
+ , ,
347
+ Figure 4: New York City’s greenhouse gas emissions as one-ton spheres of carbon dioxide gas, a cinematic visualization produced
348
+ by Carbon Visuals and released online. The cinematic visualization uses a variety of different camera views, along with stark
349
+ colors to guide viewers through an explanation of the scale of the city’s greenhouse gas emissions. The number of instances
350
+ of the blue sphere is driven by the rate of emissions. As this number grows the city buildings serve as a concrete scale.
351
+ reveal something that wasn’t already in the frame, the audience
352
+ experiences seeing it for the first time. In Choice and Chance the
353
+ camera moves to different vantage points throughout the model as
354
+ the story progresses. The camera remains in an overview shot for
355
+ the majority of the article, but moves to ground level at the climax,
356
+ elevating the intensity of the shot by placing the viewer into the
357
+ perspective of a bystander.
358
+ Author-defined camera trajectories can be played, paused,
359
+ and (lightly) modified by viewers. The cinematic visualizations
360
+ that we analyzed tended to use author-driven narrative structures [57],
361
+ with most user interactions consisting of the user clicking or scrolling
362
+ to trigger the visualization to continue to the next stage (e.g., CV2,
363
+ 5-17, 21-22). Operationally, this requires animating the position
364
+ and orientation of a digital camera model along a track specified
365
+ by the author, and has been used heavily by cinematic visualiza-
366
+ tions embedded in articles (16 out of 22). The other way in which
367
+ (constrained) interactivity was employed was allowing the manipu-
368
+ lation of 3D models. In most cases this means the user can position
369
+ the camera at a particular location around the model (see CV17 for a
370
+ stereotypical example). These models might be scientific (CV13,17)
371
+ or cultural (CV5) objects that would be otherwise inaccessible to
372
+ the audience viewing the visualization. It is common for orbital
373
+ cameras to be used, constraining the camera’s focus to remain on
374
+ a particular object of interest while allowing the user to exercise
375
+ control over viewing angle and zoom level (Fig. 7D). Cinematic
376
+ visualizations that support these interactions must be rendered in
377
+ real-time, limiting the fidelity at which the models may be rendered.
378
+ Visualization techniques are combined toward resolution
379
+ of scale. While we traditionally think of 3D graphics as ineffective
380
+ for encoding quantities [16], a recurring theme in our examples is
381
+ the use of 3D graphics to visualize and communicate quantities of
382
+ a massive scale (e.g., CV1, 6, 8, 26-28). Quantities at a scale beyond
383
+ what we experience in daily life (i.e. hyperobjects [47]), like amount
384
+ of carbon dioxide emitted from NYC annually (CV26), may be es-
385
+ pecially difficult for people to picture because we rarely, if ever,
386
+ interact with quantities of such a size. Cinematic visualizations can
387
+ convey a quantity of scale in a concrete and affecting way by using
388
+ cinematography to establish the viewer’s point of view from the
389
+ ground, a position which often serves as the implicit zero point
390
+ of a y-axis. We observed that several visualization techniques are
391
+ naturally expressed in cinematic visualizations, including data vis-
392
+ ceralizations [41], unit visualization [51] and concrete scales [14].
393
+ For example, in CV27 the viewer sees a city park, including trees,
394
+ people standing in a grassy field, and a ten meter tall blue sphere
395
+ representing the actual size of one metric ton of CO2 (data vis-
396
+ ceralization). As the scene progresses, many more spheres appear,
397
+ each representing one metric ton of CO2 (unit visualization), until
398
+ so many appear that the camera must zoom out, above the park,
399
+ observing the growing pile of spheres in comparison to the city
400
+ buildings (concrete scale).
401
+ Objects which are used as backdrops—for example a city skyline
402
+ (CV11) or parked car (CV42, Fig. 1)—may serve double duty as
403
+ concrete scale referents and contextual elements. The use of 3D
404
+ graphics affords designers the ability to use concrete scales (CV1,
405
+ 26) and visual analogies (CV29, 36) to (re-)contextualize the size of
406
+ objects, and digital sets are constructed to facilitate comparisons
407
+ that are impossible to make directly in the physical world (CV1,
408
+ 27) and use point-of-view perspective to impart a visceral sense of
409
+ magnitude. The visual medium is rich with possibilities for analogy.
410
+ For example, in [REALISTIC] Elephant rocket fuel - Saturn V (CV29,
411
+ Fig. 2), designer Maxim Sachs renders the launch of the Saturn V
412
+ rocket, except that the rocket expels elephants behind it as it travels,
413
+ rather than exhaust. The elephants represent the mass of fuel that
414
+ is being expended. By juxtaposing these images, Sachs is able to re-
415
+ frame an abstract quantity of rocket fuel in terms that people may
416
+ have more familiarity with, and do it with a sense of humor that
417
+ may make the visualization overall more memorable or engaging
418
+ for its audience [8]. In a more typical case, the narrator of CV40
419
+ asks the audience to imagine if Earth were the size of a tennis ball,
420
+ and then, using this new scale, shows the relative size of different
421
+ planets, moons, and stars. These planets are compared against one
422
+ another, rendered into real-world footage including a narrator who
423
+ provides guidance and relevant facts about the celestial objects.
424
+
425
+ , ,
426
+ Conlen, et al.
427
+ Figure 5: How Much is a Gigatonne? shows one gigatonne of ice in Central Park, New York. A digital set (A) is designed including
428
+ multiple cameras, lighting, and data-driven and contextual elements. Footage from the various cameras is composed to create
429
+ the final sequence (B-E). This was one of several videos that we developed for an article published on NASA’s climate website.
430
+ View the full videos at https://cinematic-visualization.github.io/.
431
+ They are shown embedded into several settings, for example an
432
+ office, a Los Angeles street, and the New York City skyline.
433
+ 3.2
434
+ Constraints
435
+ The time-based format does not support a high data density.
436
+ Traditional information graphics often present a data-dense display
437
+ with minimal “non-data ink” [64] to remove possible distractions
438
+ and optimize the display for tasks such as value look-up and com-
439
+ parison. In some cases, designers may choose to add additional
440
+ illustrative features to increase the memorability of the visualiza-
441
+ tion [7]. In contrast, cinematic visualizations utilize diegetic data,
442
+ embedded in a three dimensional scene with other elements which
443
+ contextualize the scene (see CV35 for a striking example). In cine-
444
+ matic visualizations (e.g. CV40,42) the elements surrounding the
445
+ data fulfill a dual role as both data and non-data ink; they add
446
+ spatial presence to the visualization [12], supporting a sense of
447
+ transportation to the virtual world for viewers, while simultane-
448
+ ously serving as guides and axes, points of reference for concrete
449
+ scales [14]. Rather than densely packing data, we see that cinematic
450
+ visualizations often only show one or a few data points in the frame,
451
+ favoring to include additional contextual elements that help add
452
+ emotional resonance to the data-story being told.
453
+ Designers trade-off between perceptual effectiveness and
454
+ dramatic narrative. Visualizations that employ 3D graphics are
455
+ often ineffective perceptually. These graphics may use sub-optimal
456
+ encoding channels like volume and can further bias judgement
457
+ through distortion and occlusion. Cinematic visualizations are not
458
+ appropriate when the task is centered around value judgements.
459
+ Instead, we see cinematic visualizations effectively used when a
460
+ rough estimate of values is sufficient and the precise value is not
461
+ of central importance (e.g. CV29). Many of the cinematic visual-
462
+ izations that we analyzed use a volume encoding to display data
463
+ (CV1,6,26,27,35). Volume is a less effective encoding channel com-
464
+ pared to position and may cause the audience to misestimate the
465
+ true quantity. This trade-off may be acceptable depending on the
466
+ data being presented and the precision with which the author hopes
467
+ it will be apprehended.
468
+ 4
469
+ CASE STUDY: HOW MUCH IS A
470
+ GIGATONNE?
471
+ We collected and studied the aforementioned cinematic visualiza-
472
+ tions while exploring designs to support the communication ob-
473
+ jectives of NASA’s Earth Science Communications Team. Climate
474
+ change is a complex, multi-faceted issue of global importance [49]
475
+ and the team is tasked with maintaining climate.nasa.gov, a website
476
+ that tracks vital statistics about Earth’s climate, and delivers up-
477
+ dates about global warming to a diverse global audience of millions
478
+ of readers. The team uses traditional information graphics [48], as
479
+ well as narrative visualizations (e.g., [53]), to highlight how scien-
480
+ tists know that anthropogenic global warming is truly happening,
481
+ what changes have taken place in Earth’s climate so far, and why it
482
+ is an important topic for readers to understand even if it does not
483
+ seem to be affecting them. However, the team sought data-driven
484
+ stories that more viscerally engaged their audience and connect
485
+
486
+ Digital set design
487
+ Cam1 (God's eye view)
488
+ D
489
+ Cam2 (bird's eye view)
490
+ Lighting: Global Illumination
491
+ Data-driven element
492
+ Geographic elements
493
+ Cam3 (point-of-view)
494
+ Texture from satellite images
495
+ A
496
+ Rendered output
497
+ B
498
+ Central Park
499
+ D
500
+ C
501
+ ewYorkCit
502
+ God's eye view (Establishing shot)
503
+ Point-of-view (Establishing)
504
+ Point-of-view (Initial action)
505
+ Medium-long shot (Peak)Cinematic Techniques in Narrative Visualization
506
+ , ,
507
+ Figure 6: We explored many different designs, these were left on the cutting room floor. The designs were dropped for reasons
508
+ including poor perceptual effectiveness (A-C), locations too small for the scale of the data (D-F), and designs too illustrative
509
+ and not physically accurate enough (G-H). It was particularly difficult to identify locations that were broadly recognizable
510
+ from a 3D reconstruction but also suitable to server as a concrete scale referent.
511
+ the planetary scale data of climate change to a human scale that
512
+ readers can readily understand.
513
+ Within the domain of climate change communication is a range
514
+ of research investigating how to effectively communicate the latest
515
+ science to a broad audience. High level principles of climate change
516
+ communication have been synthesized by the Center for Research
517
+ on Environmental Decisions [58]. We think cinematic visualizations
518
+ are well suited to satisfy principles “Get Your Audience’s Attention“
519
+ and “Translate Scientific Data Into Concrete Experience.” Here
520
+ we describe how our work creates connections between ongoing
521
+ investigations in narrative visualization, computer graphics, and
522
+ film art to achieve this.
523
+ Guided by editorial priorities set by NASA’s Earth Science Com-
524
+ munication team, we produced an article consisting of a several
525
+ cinematic visualizations to communicate massive quantities related
526
+ to climate change. We endeavoured to make them interpretable and
527
+ meaningful to a broad public audience. These visualizations were
528
+ eventually published to an audience of millions. Here we describe
529
+ our design process to create cinematic visualizations, identifying a
530
+ general workflow of use to practitioners who wish to create this
531
+ type of visualization themselves, and to tool-builders who wish to
532
+ provide better support for authoring cinematic visualizations in
533
+ the future. As with visualization production in general, these steps
534
+ are not necessarily linear; rather, the process is iterative and error
535
+ prone, and may require going back to earlier steps if it becomes
536
+ apparent that a design is not working. We experienced many failed
537
+ attempts (see Figure 6) before arriving at our final designs.
538
+ 4.1
539
+ Pre-Production
540
+ Narrative. Quantities of ice loss are measured in gigatonnes, a
541
+ unit of mass corresponding to one million metric tons. Statistics
542
+ about ice loss are often reported using this unit, for example Earth’s
543
+ polar ice caps are losing about 426 gigatonnes of ice per year, at
544
+ the time of writing. The scale of the unit here hides the fact that
545
+ 426 gigatonnes is a massive amount of ice. Our goal was to provide
546
+ a visualization that would allow our audience to better interpret
547
+ these statistics going forward. We collected statistics on ice loss in
548
+ Greenland and Antarctica (the two ice sheets) over the course of
549
+ significant periods, such as the amount of ice lost between 2002-
550
+ 2017 when NASA’s Grace satellite was actively observing the polar
551
+ ice caps, or since the start of the 20th century (5,000 and 49,000
552
+ gigatonnes, respectively).
553
+ We settled on cinematic visualization because it is a natural fit
554
+ for the use of concrete scales, we wanted to draw people’s attention,
555
+ there is a relatively small amount of data that we are showing, and
556
+ we wanted to display the data in a context that conveyed corporeal
557
+ urgency. Given the affordances identified in Section 3, a cinematic
558
+ visualization was an appropriate choice for our task of visualizing
559
+ quantities related to climate change in a way that would capture
560
+ the attention of our audience and allow them to comprehend the
561
+ data in a concrete way. We ultimately chose the form factor for our
562
+ visualization to be an interactive article containing a series of short
563
+ cinematic visualizations. The visualizations were embedded as pre-
564
+ rendered videos, which could be loaded dynamically, allowing for
565
+ a certain amount of interactivity. Depending on the use case, one
566
+ must determine whether real-time rendering is needed or not. Using
567
+ real-time rendering limits the level of photorealism [52], but enables
568
+ another level of interactivity, letting the user control the camera
569
+ and interact with elements in the scene (Fig. 7D). We intended
570
+ the narrative structure of our visualization to be largely author-
571
+ driven [57], and decided that real-time rendering was not required.
572
+ After determining that a cinematic visualization was appropri-
573
+ ate, we began outlining possible scripts and creating storyboards
574
+ in which we sketched ideas for locations, cinematography, and se-
575
+ quencing of shots. We first sought to identify locations that would
576
+ serve as effective backdrops, allowing people to gain a concrete
577
+ understanding of the size of data in familiar locations. We consid-
578
+ ered natural locations like the Grand Canyon, Monument Valley,
579
+ Mt. Everest, and Uluru, urban environments like Houston, New
580
+ York City, San Francisco, and St. Louis, and other man-made sites
581
+ like football stadiums and the Hoover Dam. Within each of these
582
+ environments we created sketches to help determine the camera
583
+ placement, mise-en-scène, data, and annotations that the visualiza-
584
+ tions would require, and wrote rough scripts to define the narrative
585
+ structure.
586
+ While we wanted to place data in a variety of different envi-
587
+ ronments so that our diverse audience would be able to connect,
588
+
589
+ 2000
590
+ 1979
591
+ 2009
592
+ Carbon
593
+ Emissions
594
+ 7021
595
+ M, ,
596
+ Conlen, et al.
597
+ ultimately many of these locations were not used. See Figure 6 for
598
+ examples of some of the locations that were not able to support
599
+ both focus and context at an anthropocentric perspective. The final
600
+ article consisted of videos visualizing one, then 5,000, then 49,000
601
+ gigatonnes of ice. The videos were embedded throughout the text
602
+ of an article which provided context. In the first and last videos the
603
+ user could click to choose to play videos displaying the relevant
604
+ quantity of ice in different locations. Here we look closely at the
605
+ design process for the first video, showing one gigatonne of ice in
606
+ Central Park, New York City.
607
+ 4.2
608
+ Principal Photography
609
+ With the storyboards and scripts ready, the source footage that
610
+ would make up the final video needed to be created. We chose to
611
+ use Blender for this process, which provides both an interactive
612
+ GUI-based interface as well as a Python API that allowed us to
613
+ load, transform, and bind data to objects in a 3D scene. We created
614
+ renders for many different scenes, although ultimately ended up
615
+ using a small number of them in our published pieces.
616
+ Mise-en-scène. The elements that constitute the mise-en-scène
617
+ of a cinematic visualization need to be created and arranged. Be-
618
+ cause many of our scenes take place in real-world locations, we
619
+ were able to utilize existing open data sets to import geographic
620
+ data, including 3D models of buildings and terrain data. In addition
621
+ to elements derived from real-world locations, we added elements
622
+ which would be parameterized by data, for example the large block
623
+ of ice placed in Central Park (Figure 5). After the models have been
624
+ created, they need to be assigned a material, which (along with
625
+ lighting) will determine how they appear in final renders. We chose
626
+ to use a flat shading for the buildings and other environmental
627
+ elements. This gave these elements less visual weight while still al-
628
+ lowing them to be easily identifiable. We considered using a similar
629
+ flat style for the data elements, but ultimately decided to add a more
630
+ photorealistic ice material which would allow the data to stand out
631
+ against the buildings and reinforce the idea that we were showing
632
+ a concrete amount of ice. While many of the examples that we saw
633
+ utilize a studio lighting setup to control shadows and reflection, we
634
+ opted to use simple global illumination to emulate the sun shining
635
+ in our outdoor scene. This meant our lighting was realistic for the
636
+ location and the setup was quite simple, but we were limited in our
637
+ ability to use lighting as a tool to guide attention, as we saw it used
638
+ (for example) in CV15.
639
+ With the scene constructed, the next step was to bind the data.
640
+ This was the point at which we realized that many of the set lo-
641
+ cations were not going to work with the data we were hoping to
642
+ visualize (“data changes everything” [66]). For example, a gigatonne
643
+ of ice placed in a football stadium (Fig. 6D) would extend over 200
644
+ kilometers into the sky, making it difficult to view both the diegetic
645
+ data and the stadium itself simultaneously. For our visualizations
646
+ we were simply assigning the dimensions of a primitive 3D object
647
+ based on calculations related to the mass of ice melt over specific
648
+ periods, along with the density of ice, in order to create blocks of
649
+ ice which were physically representative of the quantity lost.
650
+ Cinematography. After we incorporated our data into the scene
651
+ it was time to add animation and cinematography. Blender supports
652
+ a keyframe-based animation system which made it simple to add
653
+ basic animations to the size and locations of elements in the scene,
654
+ as well as the position and perspective of cameras. Working off of
655
+ the storyboards that we had created, we placed cameras (shown
656
+ in Figure 5) that would be physically realistic and familiar: we use
657
+ three cameras, one a human point-of-view, one a bird’s eye view
658
+ (as if it were taken from a helicopter circling the city), and one a
659
+ "god’s eye view" taken from the perspective of a satellite overhead.
660
+ The satellite camera allowed us to create an initial establishing shot,
661
+ while the other cameras provided views that supported a ground-
662
+ level view as well as an overview. When sequenced together, these
663
+ camera perspectives allow us to present focus plus context [13] to
664
+ the viewer, and support our narrative goals [1].
665
+ 4.3
666
+ Post-Production
667
+ Once the source material was created, we needed to edit it to form
668
+ a coherent narrative, for example by combining multiple videos in
669
+ sequence, adding annotations on top of the video to add context,
670
+ and adding sound to add presence, guide attention, and provide
671
+ details. Any visual effects must be added at this stage. For example,
672
+ in the case of embedding digital data objects into physical footage
673
+ of a narrator, a “match moving” process to align the digital and
674
+ physical scenes would need to be performed [23].
675
+ Editing. We combined footage from multiple cameras, compos-
676
+ ing shots into a narrative structure, starting with establishing shots,
677
+ then initial action, peak, and finally release [1]. The sequence of
678
+ images is important to advance the role of narrative, pacing, and
679
+ mood. Narrative visualizations often include annotations to provide
680
+ additional context and explain to viewers what it is they are seeing.
681
+ In the case of cinematic visualizations these annotations can be
682
+ composited over the source footage using standard video editing
683
+ software. Some examples that we saw embed annotations directly
684
+ into the 3D scene itself, which requires them to be embedded in the
685
+ source footage directly. We chose to composite annotations rather
686
+ than include them “in-situ” as it facilitated more rapid iteration dur-
687
+ ing the editing process, allowing us to change the timing, location,
688
+ and content of annotations, without needing to re-render any of
689
+ the source footage — a potentially time-consuming process.
690
+ Sound. In our work we ultimately did not use audio, instead
691
+ opting to embed the videos in a larger text article, which would
692
+ serve to provide viewers with context for the visualization. This is
693
+ a limitation and something to be explored more in future work, as
694
+ audio can be a useful tool in cinematic visualization to set tone and
695
+ drive narrative.
696
+ 4.4
697
+ Publication
698
+ Once the article was completed and approved for publication, it
699
+ was posted to NASA’s climate website. We did not collect detailed
700
+ metrics on how readers interacted with the videos on the article
701
+ itself, but can see how users responded to posts on the NASA
702
+ Climate Facebook, Instagram, and Twitter pages. These posts—
703
+ which contained a link to the article and (in some cases) directly
704
+ embedded the video set in New York City—were collectively viewed
705
+ tens of thousands of times, received thousands of engagements
706
+ (likes, comments, shares), and the article was subsequently shared
707
+ by other organizations such as the United States Department of
708
+
709
+ Cinematic Techniques in Narrative Visualization
710
+ , ,
711
+ Agriculture and the World Meteorological Organization, as well as
712
+ by individual scientists and meteorologists.
713
+ Across all of the social platforms users left 94 direct comments,
714
+ with topics ranging from positive (for example, some explicitly
715
+ expressing that they like this type of visualization “We need more
716
+ of these types of comparisons in the media”, “This is an amazing
717
+ visualization. Thanks NASA!”, or asking for similar visualizations
718
+ of different quantities “It would be very interesting to see this illus-
719
+ tration but with the predicted sea level after all the ice in Greenland
720
+ and Antarctica melt. Can you show that?”) to concern about the
721
+ data being visualized (“Oh my God. Come to our aid.”, “Thanks for
722
+ helping us comprehend the enormity of this sad news!”, a GIF of
723
+ a cartoon rodent crying) to climate change denial (“Where’s your
724
+ proof”, “Wow, as much as 2 millimetres. Measured by satellite too”).
725
+ The comments were distributed roughly uniformly across the three
726
+ types (positive attitude toward visualization, concern about climate
727
+ change, and climate change denial), but varied heavily across plat-
728
+ forms, with users on Facebook expressing concern or denying that
729
+ there is a climate problem, users on Instagram leaving both positive
730
+ and concerned comments, and users on Twitter expressing a range
731
+ of concern, denial, and a positive attitude toward the graphic.
732
+ 5
733
+ DISCUSSION
734
+ Cinematic visualizations can engage viewers with dramatic and
735
+ visceral presentations of data, highlighting particularly important
736
+ data points, and presenting an author-guided tour through data
737
+ embedded in a relevant context. On the other hand, they may be
738
+ poor choices for communicating large amounts of data and are
739
+ not optimal in terms of perceptual effectiveness. If a cinematic
740
+ visualization is appropriate, it will require a broad range of skills —
741
+ such as cinematography, narrative, 3D modeling, video editing, and
742
+ possibly acting — and a time-consuming iterative design process.
743
+ 5.1
744
+ Challenges of Creating Cinematic
745
+ Visualizations
746
+ While cinematic visualizations can capture the attention of their
747
+ audience and help viewers relate to the data in a concrete way,
748
+ they can be challenging and time-consuming to produce. Here we
749
+ discuss some of the challenges inherent in creating an effective
750
+ cinematic visualization.
751
+ One of the most apparent difficulties of cinematic visualization
752
+ is the potentially overwhelming size of the design space. Works
753
+ in this genre typically use three visual dimensions, plus time and
754
+ sound. The methods that allow us to analyze and critique cinematic
755
+ visualizations (e.g., [5]) do not necessarily help us to create them.
756
+ That is, they are difficult to use generatively. While information
757
+ designers are familiar with the attention to detail that is required
758
+ when placing objects in a frame in order to achieve an effective
759
+ visual hierarchy, in cinematic visualizations there are also objects
760
+ outside of the frame that affect the style and tone of the visualization.
761
+ For example, the placement of the camera in relation to the subjects,
762
+ the focal length of the camera, and the placement and strength of
763
+ light sources are all instrumental in creating a shot which can easily
764
+ be decoded by viewers.
765
+ There is a diversity of tasks that need to be completed in order
766
+ to create a cinematic visualization, each requiring a separate set of
767
+ skills. For example, in addition to skills required for traditional visu-
768
+ alization (data analysis, transformation, and visualization) and nar-
769
+ rative visualization (understanding audience, storytelling, graphic
770
+ design), cinematic visualization will often make use of animation,
771
+ cinematography, lighting, motion graphics, 3D modeling, sound
772
+ design, video editing, and (sometimes) acting. The skills that make
773
+ one a good 3D modeler are not necessarily the same skills that make
774
+ one a good storyteller, and so graphics of this type often require
775
+ a diverse team to create. Furthermore, for ray-tracing renderers,
776
+ there is a large gap between prototypes and final rendered output,
777
+ challenging the iterative design process.
778
+ 5.2
779
+ Considerations for Cinematic Visualization
780
+ Creators
781
+ While cinematic visualizations share many of the same design goals
782
+ of more traditional narrative visualization (e.g., guide the viewers’
783
+ attention), the way in which these goals are operationalized differ.
784
+ Here we highlight ways that these design goals were operational-
785
+ ized across the four dimensions of style, both in our own work and
786
+ in the examples analyzed. For a full breakdown of the techniques
787
+ used in each example, see Figure 7.
788
+ Mise-en-scène. Objects’ sizes, colors, shapes, textures, and place-
789
+ ment in relation to one another can all be used create an effective
790
+ visual hierarchy. For example, to guide a user’s attention in a cin-
791
+ ematic visualization, a designer might choose to use lighting to
792
+ cast a glow around an object (CV11), or change the object’s color
793
+ (CV2, CV13) so that it stands out. In How Much is a Gigatonne,
794
+ the ice’s large size, color, and shine draw a viewers attention to
795
+ it in contrast with the surrounding buildings, which are smaller,
796
+ grayscale, and matte. The mise-en-scène is designed both to com-
797
+ municate information—including using narrators (CV42), diegetic
798
+ data (CV35), and visual analogies (CV6)—and to add dramatic affect
799
+ (e.g. CV11, CV40).
800
+ Cinematography. Perspective can be used both to drive narra-
801
+ tive and to set tone, as well as to provide focus plus context. The
802
+ position (CV26), angle (CV28), or focus (CV2) of a camera can be
803
+ modified so that the object becomes the focal point of the frame.
804
+ To help narrow the large space of possible cinematic visualizations,
805
+ and make effective use of the frame, designers of cinematic visual-
806
+ ization may study how shots are composed and sequenced in films.
807
+ In How Much is a Gigatonne?, we rendered footage from multiple
808
+ cameras in order to create close-up, medium, and wide shots. Some
809
+ cinematic visualizations enable limited user-control of the camera,
810
+ for example letting the user trigger the next stage of animation
811
+ (CV9) or rotate their perspective (CV13). Often the camera needs
812
+ to track a particular object in the scene (CV12). If this object is in
813
+ motion you may need to set your camera to track it. Planning the
814
+ path of the camera so that the object of interest is not occluded by
815
+ other objects and so that motion is smooth and visually pleasing
816
+ can be difficult. This may be done algorithmically [15, 68] or by
817
+ hand.
818
+ Editing. Putting the footage into a particular order progressively
819
+ reveals information to convey the authors’ intended message. Edi-
820
+ tors may use footage from one camera at one location (CV29), or
821
+ multiple cameras at multiple locations (CV40). The editing tech-
822
+ niques used in data videos—particularly the use of establishing,
823
+
824
+ , ,
825
+ Conlen, et al.
826
+ initial, peak, and release shots—has been studied in more depth by
827
+ Amini et al. [1]. Similar to movie makers, creators of cinematic visu-
828
+ alizations may use the technique of storyboarding to prototype and
829
+ communicate their scenes in a lo-fidelity form before endeavouring
830
+ on the time intensive task of 3D modeling and rendering. In How
831
+ Much is a Gigatonne we use establishing shots to situate the viewer
832
+ before initiating action from the perspective of the ground level (an
833
+ anthropocentric perspective), before cutting to the vantage point
834
+ of a helicopter, using the city skyline as a concrete scale.
835
+ Sound. Audio can set tone (CV25), cue attention (CV28), and
836
+ impart additional details through narration on (CV40) or off-screen
837
+ (CV45). Music (CV29) and ambient sound (CV26) can affect the tone
838
+ of the visualization and add presence to the scene, for example
839
+ CV29 uses combines techno music and a visual analogy of of the
840
+ weight of rocket fuel (measured in elephants) to create a humorous
841
+ juxtaposition which may make the visualization more approachable
842
+ and less dry. CV26 uses diegetic sound (taxi cabs honking) to rein-
843
+ force the anthropocentric perspective. In How Much is a Gigatonne
844
+ we did not use sound (neither did most of the other visualizations
845
+ that we analyzed which used an “article” format), but effective use
846
+ of both the visual and auditory channels has been shown to lead to
847
+ improved outcomes in multimedia learning contexts [42].
848
+ 5.3
849
+ Implications for Authoring Tools
850
+ As cinematic visualization is a newly emerging genre, there is rel-
851
+ atively little tool support to facilitate authoring of this type of
852
+ visualization. Instead, creators turn to general purpose 3D software
853
+ that was designed to support a breadth of use cases such as architec-
854
+ tural design, modeling, and narrative animation. These tools, while
855
+ powerful and expressive, may overwhelm users with complexity
856
+ that is incidental to the task of creating a cinematic visualization.
857
+ For example, objects are assigned materials which are powered by
858
+ low-level shader code. One can not choose, e.g., between “realistic”
859
+ or “cartoon” aesthetics but instead must compose low level shader
860
+ components to achieve the desired look.
861
+ These tools do not support the basic building blocks of visualiza-
862
+ tion, such as easily ingesting data and binding data values to objects
863
+ in a scene. Instead, users must write custom scripts to handle any
864
+ such task. The interfaces in general are multi-modal: most 3D mod-
865
+ eling work is done directly through a GUI, but data-driven work
866
+ needs to be done in code; shaders are described using a directed
867
+ graph. Authors are forced to context switch between drastically
868
+ different environments, arguably making it harder to iterate.
869
+ The task of 3D rendering can be computationally intensive. De-
870
+ pending on the output resolution, complexity of the scene, and
871
+ computing power available, a short (30 seconds) animation could
872
+ take several hours to render. There is a large gap between the
873
+ fidelity of the final renders and what a designer sees while con-
874
+ structing the scene. This setup makes it important to create test
875
+ renders frequently, but makes it hard to have a rapid feedback loop.
876
+ 5.4
877
+ Limitations of our Work
878
+ Our survey was limited to 50 examples, taken from a limited set of
879
+ sources. While not exhaustive, the examples implement a range of
880
+ design techniques across a variety of applications. We do not pro-
881
+ vide an empirical evaluation of the work surveyed, instead choosing
882
+ to use techniques of film criticism in order to analyze patterns used
883
+ and identify the communication intentions of their producers. We
884
+ similarly did not empirically evaluate our own work, and instead
885
+ provide an account of our design process and detail our reasoning
886
+ for important decisions that were made along the way. Our work
887
+ does not fully utilize the design space of cinematic visualizations
888
+ that we identified; for example, we did not use sound at all, and all
889
+ narration was done through written text with a few small overlays
890
+ in the video. The experience might be improved by incorporating
891
+ narration either on-screen or off [10].
892
+ 6
893
+ CONCLUSION
894
+ We presented cinematic visualization, a genre of narrative visu-
895
+ alization that uses techniques from cinema in order to enhance the
896
+ presentation of data-driven stories. A central contribution of this
897
+ work is to identify a new genre of narrative visualization that we
898
+ then analyze in depth. The importance of genre is clear in other art
899
+ forms like literature and cinema; however, it is invoked less often
900
+ in the context of visualization research. We believe that this type of
901
+ work is crucial for understanding the design of narrative visualiza-
902
+ tions, and thinking rigorously about how they can be constructed
903
+ and deployed. While past work on narrative visualization looked
904
+ specifically at the narrative structure, here we look at both narra-
905
+ tive and style as formal systems that contribute to the dramatic
906
+ experience of watching a cinematic visualization. To do this, we
907
+ turned to theory from another form of art, film, in order to provide
908
+ grounding in the features of style, and used analysis techniques
909
+ established in that domain to deconstruct our case studies.
910
+ We analyzed a variety of examples of cinematic visualization and
911
+ the techniques that they employ towards certain narrative applica-
912
+ tions. Many of these visualizations show a relatively small amount
913
+ of data (e.g., focusing on a single rate or quantity) as opposed to
914
+ being data-dense. The non-data elements of the scene play an im-
915
+ portant role: they are used to set the location in which the shot is
916
+ taking place and provide cues to viewers about where they are, what
917
+ they are looking at, and why it is relevant. This approach is quite
918
+ different from typical information visualizations, where data may
919
+ be reduced to a minimal form, such as a line or a bar. Cinematic
920
+ visualization instead tends to be more maximal in its approach,
921
+ such that the non-data ink is not reduced or omitted, but rather
922
+ used to build up entire digital worlds around data points. This style
923
+ encourages viewers to feel present in locations augmented with
924
+ data objects, or to viscerally experience events that happened in
925
+ the past, or are happening far away in the universe.
926
+ Rendering data in 3D is a fraught endeavor, as the values being
927
+ rendered can be obscured by humans’ relatively poor ability to
928
+ estimate and compare volume, and because the 3D projection can
929
+ introduce distortion when trying to read values. Why would the cre-
930
+ ators choose to follow a cinematic path over one that more clearly
931
+ and directly communicates the underlying data with precision?
932
+ We argue that in choosing to treat a visualization as a cinematic
933
+ experience, its authors might be looking beyond the immediate
934
+ data, in order to viscerally ground that data in meaningful context.
935
+ In other words, analytic precision is only one of several objectives
936
+ that a visualization might help accomplish. In choosing 3D, we
937
+ might diminish precision in service of other objectives.
938
+
939
+ Cinematic Techniques in Narrative Visualization
940
+ , ,
941
+ ACKNOWLEDGEMENTS
942
+ We would like to thank Susan Callery, Holly Shaftel, Randal Jackson,
943
+ Daniel Bailey, Michael Gunson, Josh Willis, Joe Witte, and the
944
+ Earth Science Communications Team at NASA’s Jet Propulsion
945
+ Laboratory for their support of this work. A portion of this research
946
+ was carried out at the Jet Propulsion Laboratory, California Institute
947
+ of Technology, under a contract with the National Aeronautics and
948
+ Space Administration (80NM0018D0004).
949
+ REFERENCES
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+
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+ Cinematic Techniques in Narrative Visualization
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+ , ,
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+ Figure 7: We analyzed the style of 50 cinematic visualizations using the features of mise-en-scène, cinematography, editing, and
1148
+ sound. An HTML version of this table including URLs for each row can be found at https://cinematic-visualization.github.io/.
1149
+
1150
+ Cinematography
1151
+ Mise-en-scene
1152
+ Editing
1153
+ Audio
1154
+ rative Text
1155
+ Composited Annotations
1156
+ Jser-controlled camera
1157
+ Realistic Background
1158
+ - Opacity
1159
+ mera
1160
+ er-triggered steps
1161
+ 3617 - L
1162
+ n-Situ Annotations
1163
+ Composited Narra
1164
+ Point-of-view can
1165
+ nera
1166
+ Visual Analogy
1167
+ rator
1168
+ it Visualizatiol
1169
+ Scale
1170
+ punos oeba
1171
+ Reality
1172
+ n-situ Narra
1173
+ notation
1174
+ Annotation
1175
+ Annotation
1176
+ dded
1177
+ ncrete
1178
+ erview
1179
+ pax
1180
+ ISIC
1181
+ 0
1182
+ Author
1183
+ Publishel
1184
+ Titte
1185
+ cV1
1186
+ Drowning in plastic
1187
+ Simon Scarr, et al.
1188
+ Reuters
1189
+ CV2
1190
+ Is This the Neighborhood New York Deserves?
1191
+ Michael Kimmelman
1192
+ NYT
1193
+ CV3
1194
+ Krigsskipet som krasjet og sank
1195
+ B
1196
+ Stangvik, et al.
1197
+ VG
1198
+ CV4
1199
+ How China Turned a City Into a Prison
1200
+ Chris Buckley, et al.
1201
+ NYT
1202
+ CV5
1203
+ The Forbidden City's unique architecture
1204
+ Marco Hernandez
1205
+ South China Morning Post
1206
+ CV6
1207
+ Here are 120 million Monopoly pieces, roughly one.
1208
+ Confessore, et al.
1209
+ NYT
1210
+ CV7
1211
+ Building Katie's New Face
1212
+ Jason Treat
1213
+ NatGeo
1214
+ CV8
1215
+ Mass Exodus: The scale of the Rohingya crisis
1216
+ Christian Inton
1217
+ Reuters
1218
+ This 3-D Simulation Shows Why Social Distancing.
1219
+ CV9
1220
+ Parshina-Kottas, et al.
1221
+ NYT
1222
+ CV10 Tracking China's Muslim Gulag
1223
+ Simon Scarr
1224
+ Reuters
1225
+ CV11
1226
+ Choice and Chance
1227
+ Staff
1228
+ Tampa Bay Times
1229
+ cV12 Cassini's Grand Tour
1230
+ Nadia Drake, et al.
1231
+ NatGeo
1232
+ CV13 Resurecting a Dragon
1233
+ Brian T Jacobs
1234
+ NatGeo
1235
+ CV14Want to fireproof your house? Here's where to start
1236
+ Kyle Kim, et al.
1237
+ LATimes
1238
+ CV15Apoll 11 -As They Shot It
1239
+ Jonathan Corum, et al. NYT
1240
+ CV16 The Atlas of Moons
1241
+ NatGeo Staff
1242
+ NatGeo
1243
+ CV17 Explore a Toad's Digital Clone
1244
+ Brian T. Jacobs
1245
+ NatGeo
1246
+ CV18 THE THOMAS FIRE: 40 DAYS OF DEVASTATION
1247
+ Joe Fox
1248
+ LATimes
1249
+ D.
1250
+ CV19 Is the Nasdag in Another Bubble?
1251
+ Roger Kenny, et al.
1252
+ Wall Street Journal
1253
+ CV20 A 3-D View of a Chart That Predicts The Econom...
1254
+ Gregor Aisch, et al.
1255
+ NYT
1256
+ CV21
1257
+ Inside the Taser
1258
+ Simon Scarr
1259
+ Reuters
1260
+ CV22 Seeing Earth from Outer Space
1261
+ Matthew Conlen
1262
+ The Pudding
1263
+ C.
1264
+ CV23 Of Catastrophes and Rescues: Making the Invisib..
1265
+ Peter Mindek, et al.
1266
+ PacificVis
1267
+ CV24A Visualization of Two-stage Autoignition of n-dod..
1268
+ Yucong Ye, et al.
1269
+ PacificVis
1270
+ CV25 How Mariano Rivera Dominates Hitters
1271
+ Graham Roberts, et al. NYTimes
1272
+ Real World Visuals
1273
+ Real World Visuals
1274
+ CV27 CCS:A2 degree solution
1275
+ Real World Visuals
1276
+ Real world Visuals
1277
+ CV28CARS
1278
+ Real World Visuals
1279
+ Real world Visuals
1280
+ CV29[REALISTIC] Elephant rocket fuel - Saturn V
1281
+ Maxim Sachs
1282
+ YOUTUBE
1283
+ CV30 University of Exeter greenhouse gas emissions in R..
1284
+ Real World Visuals
1285
+ Real world Visuals
1286
+ CV31if The World Were 100 People
1287
+ Gabriel Reilich, et al.
1288
+ Good Magazine
1289
+ CV32 Up - and down - from Ground Zero
1290
+ Graham Roberts, et al. NYT
1291
+ CV33 The Birth of a Virtual Cell
1292
+ Peter Mindek, et al.
1293
+ PacificVis
1294
+ CV34
1295
+ The Nuclear Threat - The Shadow Peace
1296
+ Neil Halloran
1297
+ Youtube
1298
+ CV35What f Carbon Left Your Tailpipe as Solid Chunks?
1299
+ Sukee Bennett
1300
+ PBS Nova
1301
+ CV36Stay Home, Flatten the Curve
1302
+ keta
1303
+ Youtube
1304
+ CV37 Chart Party: We decided to erase the three-pointer
1305
+ Jon Bois
1306
+ Youtube
1307
+ cV38 200 Countries, 200 Years, 4 Minutes
1308
+ Hans Rosling
1309
+ Youtube
1310
+ CV39 The best stats you've ever seen
1311
+ Hans Rosling
1312
+ TED
1313
+ CV40 VFX Artist Reveals the True Scale of the Universe
1314
+ Wren Weichman
1315
+ Corridor Crew
1316
+ CV41
1317
+ Helge Ingstad
1318
+ Hallvard Sandberg
1319
+ NRKbeta
1320
+ CV42The dangers of storm surge
1321
+ The Weather Channel
1322
+ The Weather Channel
1323
+ CV43 Survive the Tornado
1324
+ The Weather Channel
1325
+ The Weather Channel
1326
+ CV44
1327
+ Television Elections Coverage
1328
+ KING5 TV
1329
+ KING5
1330
+ CV45 Powers of Ten
1331
+ Eames & Eames
1332
+ IBM
1333
+ CV46 Strange things happen when you rotate in 4 dimen...
1334
+ Hamish Todd
1335
+ Youtube
1336
+ CV47 Discovering Gale Crater
1337
+ Armand Emamdjomeh LATimes
1338
+ A
1339
+ CV48 Taiwan earthquake: Survivors found in rubble of Ta..
1340
+ Malachy Brown,
1341
+ SketchFab / Australian
1342
+ cV49 Four of the Best Olympians, as You've Never Seen...
1343
+ John Branch
1344
+ NYT
1345
+ CV50 How We Created a Virtual Crime Scene to Investig.
1346
+ Malachy Brown,
1347
+ NYT
1348
+ CV13
1349
+ CV40
1350
+ CV26
1351
+ CV35
1352
+ D. Author-Guided
1353
+ A. In-situ Narrator
1354
+ B. Anthropocentric Perspective
1355
+ C. Resolving Scale
1356
+ Interactive Camera
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1
+ Do entangled states correspond to entangled measurements under local transformations?
2
+ Florian Pimpel,1, ∗ Martin J. Renner,2, 3, ∗ and Armin Tavakoli4
3
+ 1Atominstitut, Technische Universität Wien, Stadionallee 2, 1020 Vienna, Austria
4
+ 2University of Vienna, Faculty of Physics, Vienna Center for Quantum Science and Technology (VCQ), Boltzmanngasse 5, 1090 Vienna, Austria
5
+ 3Institute for Quantum Optics and Quantum Information - IQOQI Vienna,
6
+ Austrian Academy of Sciences, Boltzmanngasse 3, 1090 Vienna, Austria
7
+ 4Physics Department, Lund University, Box 118, 22100 Lund, Sweden
8
+ We investigate whether pure entangled states can be associated to a measurement basis in which all vectors are
9
+ local unitary transformations of the original state. We prove that for bipartite states with a local dimension that is
10
+ either 2, 4 or 8, every state corresponds to a basis. Via numerics we strongly evidence the same conclusion also
11
+ for two qutrits and three qubits. However, for some states of four qubits we are unable to find a basis, leading
12
+ us to conjecture that not all quantum states admit a corresponding measurement. Furthermore, we investigate
13
+ whether there can exist a set of local unitaries that transform any state into a basis. While we show that such a
14
+ state-independent construction cannot exist for general quantum states, we prove that it does exist for real-valued
15
+ n-qubit states if and only if n = 2, 3, and that such constructions are impossible for any multipartite system
16
+ of an odd local dimension. Our results suggest a rich relationship between entangled states and iso-entangled
17
+ measurements with a strong dependence on both particle numbers and dimension.
18
+ Entanglement is a fundamental, broadly useful and an in-
19
+ tensely studied feature of quantum mechanics.
20
+ However,
21
+ in spite being of arguably similar foundational significance,
22
+ much less is known about the entanglement of joint quan-
23
+ tum measurements than the entanglement of quantum states.
24
+ Entangled measurements are crucial for seminal quantum in-
25
+ formation protocols such as teleportation [1], dense coding
26
+ [2] and entanglement swapping [3], which are instrumen-
27
+ tal for various quantum technologies.
28
+ Typically, they are
29
+ based on the paradigmatic Bell basis, which is composed of
30
+ the four maximally entangled states (|00⟩ ± |11⟩)/
31
+
32
+ 2 and
33
+ (|01⟩ ± |10⟩)/
34
+
35
+ 2. In the same way that the Bell basis may
36
+ be thought of as the measurement corresponding to the max-
37
+ imally entangled state, it is natural to ask whether entangled
38
+ states in general can be associated with a corresponding en-
39
+ tangled measurement. Studying the relationship between en-
40
+ tangled states and entangled measurements is not only inter-
41
+ esting for understanding quantum mechanics. It is also an
42
+ invitation to explore, in the context of quantum information
43
+ applications, the largely uncharted terrain of entangled mea-
44
+ surements beyond the Bell basis and its immediate general-
45
+ isations. Most notably, entangled measurements beyond the
46
+ Bell basis are also increasingly interesting for topics such as
47
+ network nonlocality [4] and entanglement-assisted quantum
48
+ communication [5, 6].
49
+ Consider that we are given a pure quantum state |ψ⟩ com-
50
+ prised of n subsystems, each of dimension d. Is it possible
51
+ to find a measurement, namely an orthonormal basis of the
52
+ global dn-dimensional Hilbert space, in which all basis states
53
+ have the same degree of entanglement as |ψ⟩? Specifically, we
54
+ want to decide the existence of dn strings, {Vj}dn
55
+ j=1, of local
56
+ unitary transformations,
57
+ Vj =
58
+ n
59
+
60
+ k=1
61
+ U (j)
62
+ k
63
+ (1)
64
+ ∗ These authors contributed equally.
65
+ where U (j)
66
+ k
67
+ is a d-dimensional unitary operator, such that the
68
+ set of states |ψj⟩ ≡ Vj |ψ⟩ form a basis, i.e. | ⟨ψj|ψj′⟩ | =
69
+ δjj′. If affirmative, we say that |ψ⟩ admits a basis and we call
70
+ the set of basis vectors {|ψj⟩}dn
71
+ j=1 a |ψ⟩-basis.
72
+ Known examples of entangled measurements can be ac-
73
+ commodated in this picture. For example, the Bell basis can
74
+ be obtained from operating on |ψ⟩ = (|00⟩ + |11⟩)/
75
+
76
+ 2 with
77
+ the four strings of local unitaries {Vj}4
78
+ j=1 = {11 ⊗ 11, 11 ⊗
79
+ X, Z ⊗ 11, Z ⊗ X}, where X and Z are bit-flip and phase-
80
+ flip Pauli operators. A well-known generalisation of the Bell
81
+ basis to n systems of dimension d can be thought of as a
82
+ |GHZn,d⟩-measurement where the relevant state is the higher-
83
+ dimensional GHZ state |GHZn,d⟩ =
84
+ 1
85
+
86
+ d
87
+ �d−1
88
+ k=0 |k⟩⊗n. The
89
+ corresponding strings of local unitaries are Vj = Zj1
90
+ d ⊗Xj2
91
+ d ⊗
92
+ . . . ⊗ Xjn
93
+ d |GHZn,d⟩ where j = j1 . . . jn ∈ {0, . . . , d − 1}n
94
+ and where Zd = �d−1
95
+ l=0 e
96
+ 2πi
97
+ d l |l⟩⟨l| and Xd = �d−1
98
+ l=0 |l + 1⟩⟨l|
99
+ are generalised Pauli operators. More generally, any state that
100
+ is locally maximally entanglable (for example graph states)
101
+ is known to admit a basis via suitable unitaries of the form
102
+ Vj = U j1
103
+ 1 ⊗ . . . ⊗ U jn
104
+ n
105
+ [7]. These states are characterised
106
+ by the property that if each qubit is supplemented with a
107
+ qubit ancilla and controlled unitary gates are performed on
108
+ the state-ancilla pairs, then a maximally entangled bipartite
109
+ state can be constructed between the collection of state-qubits
110
+ and the collection of ancilla-qubits.
111
+ However, this is far
112
+ from a complete characterisation of the states that admit a
113
+ basis, which is seen already in the restrictive form of the
114
+ strings of unitaries. For example, the three-qubit W-state,
115
+ |W3⟩ = (|001⟩+|010⟩+|100⟩)/
116
+
117
+ 3, is not locally maximally
118
+ entanglable but is neverthelss known to admit a basis [8]. In
119
+ what follows, we set out to systematically explore whether
120
+ entangled states admit a corresponding basis and then, as we
121
+ will introduce later, whether such bases can be constructed
122
+ even without prior knowledge of the state.
123
+ Let us begin with considering the simplest situation, namely
124
+ when |ψ⟩ is a state of two qubits. We constructively show that
125
+ every such state admits a basis. To this end, we first apply
126
+ the state-dependent local unitaries W A
127
+ ψ ⊗ W B
128
+ ψ that map |ψ⟩,
129
+ arXiv:2301.13285v1 [quant-ph] 30 Jan 2023
130
+
131
+ 2
132
+ via a Schmidt decomposition, into the computational basis,
133
+ |ψS⟩ = λ |00⟩+
134
+
135
+ 1 − λ2 |11⟩ for some coefficient 0 ≤ λ ≤ 1.
136
+ Then, we consider the action of the following four strings of
137
+ local unitaries
138
+
139
+
140
+
141
+
142
+
143
+ 11 ⊗ 11
144
+ 11 ⊗ XZ
145
+ XZ ⊗ Z
146
+ XZ ⊗ X
147
+
148
+
149
+
150
+
151
+
152
+ .
153
+ (2)
154
+ One can verify that this transforms |ψS⟩ into a |ψ⟩-basis. No-
155
+ tice that once the state has been rotated into the Schmidt form
156
+ |ψS⟩, the subsequent unitaries (2) do not depend on λ. This
157
+ construction can be extended to bipartite (n = 2) states of
158
+ local dimension d = 4 and d = 8. Again via Schmidt de-
159
+ composition, we can find state-dependent local unitaries that
160
+ transform |ψ⟩ into |ψS⟩ = �d−1
161
+ l=0 λl |ll⟩ for some Schmidt co-
162
+ efficients �
163
+ l λ2
164
+ l = 1. In Appendix A, we show that there is a
165
+ set of local unitaries that indeed leads to a |ψ⟩-basis indepen-
166
+ dently of the specific Schmidt coefficients.
167
+ It is natural to consider also the simplest case that is not
168
+ of the above convenient form, namely that of two qutrits,
169
+ (n, d) = (2, 3). This appears to be considerably different be-
170
+ cause we fail to find strings of local unitaries that bring the
171
+ Schmidt decomposition |ψS⟩ into a basis without explicit de-
172
+ pendence on the Schmidt coefficients. Nevertheless, a basis
173
+ might still be possible to construct by taking the Schmidt co-
174
+ efficients into account when choosing the local unitaries. Ac-
175
+ tually, this seems to always be possible. To arrive at this, we
176
+ have used a numerical method. Let {|φj⟩}m
177
+ j=1 be a set of states
178
+ in a given Hilbert space. These states are pairwise orthogonal
179
+ if and only if they realise the global minimum (zero) of the
180
+ following objective function
181
+ f({φj}) ≡
182
+
183
+ j̸=j′
184
+ | ⟨φj|φj′⟩ |2.
185
+ (3)
186
+ For a given state |ψ⟩, we numerically minimise f({ψj}) over
187
+ all possible strings {Vj}dn
188
+ j=1 of local unitaries. To this end,
189
+ we parameterise the local unitaries U (j)
190
+ k
191
+ using the scheme of
192
+ Ref. [9]. For the two-qutrit case, we have randomly chosen
193
+ 1000 pairs of Schmidt coefficients (λ1, λ2) which (up to local
194
+ unitaries) fully specifies the state. In each case we numerically
195
+ minimise f({ψj}). Without exception, we find strings of lo-
196
+ cal unitaries that yield a result below our selected precision
197
+ threshold of f ≤ 10−6.
198
+ Furthermore, we have also numerically investigated the
199
+ case of three qubits, (n, d) = (3, 2). This scenario requires
200
+ a different approach than the previous cases since multipar-
201
+ tite states have no Schmidt decomposition. Instead, for any
202
+ given three-qubit state |ψ⟩, there exists local unitary transfor-
203
+ mations that map it onto the canonical form a |000⟩+b |011⟩+
204
+ c |101⟩ + d |110⟩ + e |111⟩ where (b, c, d, e) are real num-
205
+ bers and a is a complex number [10, 11]. Hence, up to lo-
206
+ cal unitaries, the state space (after normalisation) is charac-
207
+ terised by five real numbers. Later, we will provide an analyt-
208
+ ical construction of a |ψ⟩-basis for the four-parameter family
209
+ corresponding to restricting a to be real. However, we have
210
+ not found an analytical basis construction for general three-
211
+ qubit states, but we nevertheless conjecture that it exists. To
212
+ evidence this, we have employed the previously introduced
213
+ numerical search method. Again, we have randomly chosen
214
+ 1000 normalised sets of coefficients (a, b, c, d, e) and searched
215
+ for the minimal value of f over all the strings of local qubit
216
+ unitaries. In all cases, we find that f vanishes up to our se-
217
+ lected precision of f ≤ 10−6.
218
+ Given the above case studies, one might suspect that ev-
219
+ ery pure quantum state admits a basis.
220
+ Interestingly, this
221
+ seems not to be true.
222
+ While some states of four qubits,
223
+ (n, d) = (4, 2), are found to admit a basis, for example
224
+ a W state and doubly-excited Dicke state [23], it appears
225
+ that most four-qubit states do not admit a basis. We have
226
+ sampled many different four-qubit states and repeatingly at-
227
+ tempted to numerically find a basis via the minimisation of
228
+ (3), also using several different search algorithms. It was reg-
229
+ ularly found that the estimated minimum is multiple orders
230
+ of magnitude above our given precision threshold for a basis.
231
+ For example, we searched for the minimum of f for the state
232
+ 2
233
+
234
+ 6 |W⟩ +
235
+
236
+ 2
237
+
238
+ 6 |GHZ4,2⟩, with 100 randomised initial points,
239
+ and never reached below f = 10−1, five orders of magnitude
240
+ above our precision threshold. We have attempted to prove
241
+ that no basis exists by employing semidefinite outer relax-
242
+ ations of f over the set of dimensionally-restricted quantum
243
+ correlations [12] combined with a modified sampling of the
244
+ state and measurement space [13] and symmetrisation tech-
245
+ niques [14] to efficiently treat the large number of single-qubit
246
+ unitaries featured in this problem. However, the conjecture
247
+ has resisted our efforts. A guiding intuition for the impossi-
248
+ bility of a basis is to note that the number of free parameters is
249
+ 3n(2n − 1) whereas the number of orthogonality constraints
250
+ (counting both the real and imaginary part) is 22n − 2n, and
251
+ the latter is larger than the former only when n ≥ 4.
252
+ Furthermore, if an n-qubit state |ψ⟩ does not admit a ba-
253
+ sis, then the (n + 1)-qubit state |ψ′⟩ = |ψ⟩ ⊗ |0⟩ also does
254
+ not admit a basis. By contradiction, suppose there are 2n+1
255
+ unitaries V ′
256
+ j = Vj ⊗ U (j)
257
+ n+1 such that |⟨ψ′|(V ′
258
+ j )†V ′
259
+ k|ψ′⟩| =
260
+ δjk ∀j, k ∈ {1, ..., 2n+1}. Divide the 2n+1 states U (j)
261
+ n+1 |0⟩
262
+ into two sets such that two orthogonal vectors are not in
263
+ the same set (e.g. the northern and southern hemisphere
264
+ of the Bloch ball).
265
+ Consider the set that contains at least
266
+ as many elements as the other one, hence, at least 2n el-
267
+ ements.
268
+ By construction, these states cannot be distin-
269
+ guished on the last qubit, |⟨0|U (j)†
270
+ n+1U (k)
271
+ n+1|0⟩| ̸= 0.
272
+ Since
273
+ |⟨ψ′|(V ′
274
+ j )†V ′
275
+ k|ψ′⟩| = |⟨ψ|V †
276
+ j Vk|ψ⟩| · |⟨0|U (j)†
277
+ n+1U (k)
278
+ n+1|0⟩|, we
279
+ must have |⟨ψ|V †
280
+ j Vk|ψ⟩| = δjk for all of those pairs, which
281
+ contradicts that |ψ⟩ does not admit a basis. By induction, this
282
+ argument shows that if our above conjecture holds, namely
283
+ that some four-qubit states do not admit a basis, then the same
284
+ holds for any number of qubits.
285
+ Since not all pure quantum states admit a basis, and this
286
+ seems to be typical rather than exceptional for four qubits, it
287
+ is interesting to ask whether some distinguished families of
288
+ n-qubit states can nevertheless admit a basis. This is well-
289
+ known to be the case for n-qubit GHZ-states and graph-states
290
+
291
+ 3
292
+ since they are locally maximally entanglable. More interest-
293
+ ingly, a positive answer is also possible for states that are not
294
+ of this kind: we construct a basis for the n-qubit W-state,
295
+ |Wn⟩ =
296
+ 1
297
+ √n
298
+
299
+ σ σ(|0⟩⊗n−1 |1⟩) where σ runs over all permu-
300
+ tations of the position of “1”. Note that |W1⟩ = |1⟩ and that a
301
+ |W1⟩-basis is obtained from the unitaries {11, X}. Now we ap-
302
+ ply induction. Consider that the strings {V (n)
303
+ j
304
+ }2n
305
+ j=1 generate a
306
+ |Wn⟩-basis. One can then construct a basis for n+1 qubits as
307
+ follows. For half of the basis elements, namely j = 1, . . . , 2n,
308
+ define V (n+1)
309
+ j
310
+ = V (n)
311
+ j
312
+ ⊗ 11 and for the other half, namely j =
313
+ 2n +1, . . . , 2n+1, define V (n+1)
314
+ j
315
+ = �n
316
+ k=1 U (j)
317
+ k Z ⊗X. As we
318
+ detail in Appendix B, one can verify that {V (n+1)
319
+ j
320
+ |Wn+1⟩}j
321
+ is a W-basis. We note that for the purpose of entanglement
322
+ distillation, a different construction of a W-basis was given in
323
+ Ref. [8].
324
+ So far, we have considered whether a specific state can be
325
+ associated to a specific measurement. In other words, the uni-
326
+ tary constructions have been state-dependent. We now go fur-
327
+ ther and introduce a complementary concept, namely whether
328
+ there exist strings of local unitaries {Vj} that can transform
329
+ any state in a space of states S into a basis, i.e. strings of local
330
+ unitaries that satisfy
331
+ ∀ψ ∈ S,
332
+ |⟨ψ|V †
333
+ j Vj′|ψ⟩| = δjj′.
334
+ (4)
335
+ Naturally, this state-independent notion of basis construc-
336
+ tion is much stronger than the previously considered state-
337
+ dependent notion.
338
+ In the most ambitious case, when we
339
+ choose the space S to be the entire Hilbert space of n sub-
340
+ systems of dimension d, i.e. S ≃ (Cd)⊗n, then a state-
341
+ independent construction cannot exist. In fact, not even two
342
+ orthogonal vectors can be state-independently constructed for
343
+ the full quantum state space. To show this, we can w. l. g. set
344
+ V1 = 11 and assume that there exists local unitaries {Uk}
345
+ such that |ψ1⟩ = |ψ⟩ and |ψ2⟩ = �n
346
+ k=1 Uk |ψ⟩ are orthog-
347
+ onal for all |ψ⟩. Focus now on the particular state |ψ⟩ =
348
+ �n
349
+ k=1 |µk⟩ where |µk⟩ is some eigenvector of the unitary Uk.
350
+ Since the eigenvalues of a unitary are complex phases, writ-
351
+ ten eiϕk for Uk and |µk⟩, we obtain |ψ1⟩ = �n
352
+ k=1 |µk⟩ and
353
+ |ψ2⟩ = ei �n
354
+ k=1 ϕk �n
355
+ k=1 |µk⟩. These two states are evidently
356
+ not orthogonal and hence we have a contradiction.
357
+ Interestingly, the situation changes radically if we limit our
358
+ state-independent investigation to all quantum states in a real-
359
+ valued Hilbert space. That is, S ≃ (Rd)⊗n. Such real quan-
360
+ tum systems have also been contrasted in the literature with
361
+ their complex counterparts [15–17]. Let us momentarily ig-
362
+ nore the n-partition structure of our Hilbert space and sim-
363
+ ply consider two real states |ψ1⟩ = |ψ⟩ and |ψ2⟩ = U |ψ⟩
364
+ obtained from a given real target state |ψ⟩ and a fixed (ψ-
365
+ independent) unitary U.
366
+ It holds that ψ1 and ψ2 are or-
367
+ thogonal if and only if U is skew-symmetric.
368
+ To prove
369
+ this, assume first the skew-symmetry property U = −U T .
370
+ Since for real states ⟨ψ1|ψ2⟩ = ⟨ψ2|ψ1⟩∗ is equivalent to
371
+ ⟨ψ|U|ψ⟩ = ⟨ψ|U †|ψ⟩∗ = ⟨ψ|U T |ψ⟩, skew-symmetry im-
372
+ plies that ⟨ψ1|ψ2⟩ = 0. Conversely, assume that ⟨ψ|U|ψ⟩ = 0
373
+ for all real-valued ψ. Choosing in particular |ψ⟩ = |k⟩ for
374
+ k = 0, . . . , d − 1, it follows that all diagonal elements of U
375
+ must vanish. Then, choose |ψ⟩ =
376
+ 1
377
+
378
+ 2(|i⟩ + |j⟩) for any pair
379
+ i ̸= j. This yield Uii+Ujj+Uij+Uji = 0, but since we know
380
+ that the diagonals vanish we are left with just Uij = −Uji
381
+ which defines a skew-symmetric operator.
382
+ Returning to our n-partitioned real Hilbert space, and still
383
+ w. l. g. taking V1 = 11, the above result demands that we find
384
+ local unitaries such that
385
+ U1 ⊗ . . . ⊗ Un = −U T
386
+ 1 ⊗ . . . ⊗ U T
387
+ n .
388
+ (5)
389
+ This is only possible if U T
390
+ k = ±Uk. Hence, all local unitaries
391
+ must be either symmetric or skew-symmetric, and the number
392
+ of the latter must be odd. When extended from two orthogonal
393
+ states to a whole basis, we require that this property holds for
394
+ every pair of distinct labels (j, j′) in the basis. In other words,
395
+ we require that every string (Vj)†Vj′ with j ̸= j′ is skew-
396
+ symmetric.
397
+ The question becomes whether the above condition can
398
+ be satisfied for a given scenario. Consider it first for qubit
399
+ systems (d = 2). In Appendix C we show that the set of
400
+ complex qubit unitaries that are either symmetric or skew-
401
+ symmetric and whose products are again either symmetric
402
+ or skew-symmetric, must obey a simple structure; they are
403
+ essentially equivalent to the four Pauli-type operators P ≡
404
+ {11, X, Z, XZ}. Thus, if a state-independent construction ex-
405
+ ists, we can restrict to selecting one of these four operators for
406
+ each of our local unitaries U (j)
407
+ k . Interestingly, for the case of
408
+ two qubits, (n, d) = (2, 2), a state-independent construction
409
+ is possible. It is in fact given by Eq. (2). One can straightfor-
410
+ wardly verify that the above criterion is satisfied, i.e. all local
411
+ unitaries are selected from P and all pairs of products of uni-
412
+ tary strings in (2) are skew-symmetric. Alternatively, one can
413
+ easily verify that (2) maps every state �
414
+ i,j=0,1 αij |ij⟩ into a
415
+ basis, for any real coefficients αij. Furthermore, by the same
416
+ token, a state-independent basis is also possible for every real
417
+ state of three qubits, (n, d) = (3, 2). One explicit construc-
418
+ tion that satisfies our necessary and sufficient criterion is the
419
+ following set of eight strings of local unitaries
420
+
421
+
422
+
423
+
424
+
425
+
426
+
427
+
428
+
429
+
430
+
431
+
432
+
433
+
434
+
435
+
436
+
437
+
438
+
439
+
440
+
441
+ 11 ⊗ 11 ⊗ 11
442
+ Z ⊗ Z ⊗ XZ
443
+ Z ⊗ XZ ⊗ 11
444
+ XZ ⊗ 11 ⊗ 11
445
+ Z ⊗ X ⊗ XZ
446
+ X ⊗ 11 ⊗ XZ
447
+ X ⊗ XZ ⊗ Z
448
+ X ⊗ XZ ⊗ X
449
+
450
+
451
+
452
+
453
+
454
+
455
+
456
+
457
+
458
+
459
+
460
+
461
+
462
+
463
+
464
+
465
+
466
+
467
+
468
+
469
+
470
+ .
471
+ Again,
472
+ one
473
+ may
474
+ easily
475
+ verify
476
+ that
477
+ every
478
+ real
479
+ state
480
+
481
+ i,j,k=0,1 αijk |ijk⟩ is mapped into a basis.
482
+ Two- and three-qubits are interesting cases because they
483
+ are exceptional.
484
+ As we now show, there exists no state-
485
+ independent construction for real states of four or more qubits.
486
+ We first prove this for n = 4 and then show that this im-
487
+ plies impossibility also for n > 4. The four-qubit case con-
488
+ tains 16 strings of unitaries and we know that each local uni-
489
+ tary can w. l. g. be selected from P. Since we seek a state-
490
+ independent construction, we can momentarily consider only
491
+ the state |0000⟩. In order for it to be mapped into a basis, we
492
+
493
+ 4
494
+ (2,2,R) (2,2,C) (3,2,R) (3,2,C) (4,2,R) (2,3,C) (2,4 or 8,C) (n, 2m + 1,R)
495
+ State-dependent
496
+ construction
497
+ 
498
+ 
499
+ 
500
+ ()
501
+ ()
502
+ ()
503
+ 
504
+ − − −
505
+ State-independent
506
+ construction
507
+ 
508
+ 
509
+ 
510
+ 
511
+ 
512
+ 
513
+ 
514
+ 
515
+ TABLE I: Overview of results. The first row indicates the scenario: (n, d, S) gives particle number, dimension and the type of state space
516
+ respectively. The symbol indicates the existence of a basis under local unitaries. The symbol indicates that there in general can be no basis
517
+ under local unitaries, i.e. at least one state admits no basis. Paranthesis indicates that the result is obtained from numerical search. The
518
+ symbol − − − indicates that no investigation was made.
519
+ see that Z acts trivially on every register and therefore each
520
+ one of the 16 combinations of bit-flip or identity operators,
521
+ {Xc1 ⊗ Xc2 ⊗ Xc3 ⊗ Xc4} for c1, c2, c3, c4 ∈ {0, 1}, must
522
+ be featured in exactly one of the 16 unitary strings {Vj}16
523
+ j=1.
524
+ Let us now look only at six of these strings, namely those
525
+ corresponding to having zero bit-flips (1 case), one bit-flip (4
526
+ cases) and four bit-flips (1 case). W. l. g. fixing V1 = 11 (zero
527
+ bit-flips), the strings take the form
528
+ V1
529
+ 11
530
+
531
+ 11
532
+
533
+ 11
534
+
535
+ 11
536
+ V2
537
+ XZr11 ⊗
538
+ Zr12
539
+
540
+ Zr13
541
+
542
+ Zr14
543
+ V3
544
+ Zr21
545
+ ⊗ XZr22 ⊗
546
+ Zr23
547
+
548
+ Zr24
549
+ V4
550
+ Zr31
551
+
552
+ Zr32
553
+ ⊗ XZr33 ⊗
554
+ Zr34
555
+ V5
556
+ Zr41
557
+
558
+ Zr42
559
+
560
+ Zr43
561
+ ⊗ XZr44
562
+ V6
563
+ XZr51 ⊗ XZr52 ⊗ XZr53 ⊗ XZr54
564
+ ,
565
+ (6)
566
+ where rij
567
+ ∈ {0, 1} represent our freedom to insert a Z
568
+ operator and thus realise the two relevant elements of P.
569
+ Since every row must be skew-symmetric and the only skew-
570
+ symmetric element in P is XZ, we must have r11 = r22 =
571
+ r33 = r44 = 1 and r51 + r52 + r53 + r54 = 1 where ad-
572
+ dition is modulo two. Moreover, every product of two rows
573
+ must be skew-symmetric, i.e. the product must have an odd
574
+ number of XZ operations. For the four middle rows, this im-
575
+ plies rij + rji = 1 for distinct indices i, j ∈ {1, 2, 3, 4}. For
576
+ the products V †
577
+ 6 Vj for j = 2, 3, 4, 5, the conditions for skew-
578
+ symmetry respectively become
579
+ r12 + r13 + r14 + r52 + r53 + r54 = 1
580
+ r21 + r23 + r24 + r51 + r53 + r54 = 1
581
+ r31 + r32 + r34 + r51 + r52 + r54 = 1
582
+ r41 + r42 + r43 + r51 + r52 + r53 = 1.
583
+ (7)
584
+ Summing these four equations and using the previously es-
585
+ tablished skew-symmetry conditions, one can cancel out all
586
+ degrees of freedom rij and arrive at the contradiction 1 = 0.
587
+ Hence, we conclude that the state-independent basis construc-
588
+ tion for four qubits is impossible.
589
+ For the case of five qubits, we can again assume w. l. g. that
590
+ the 32 combinations of bit-flip or identity operators, {Xc1 ⊗
591
+ Xc2⊗Xc3⊗Xc4⊗Xc5} for c1, c2, c3, c4, c5 ∈ {0, 1} must be
592
+ featured in exactly one of the 32 unitary strings since the state
593
+ |00000⟩ has to be mapped into an orthonormal basis. Suppose
594
+ there is a state-independent construction that maps every real-
595
+ valued five-qubit state into a basis, in especially any state of
596
+ the form |ψ⟩ ⊗ |0⟩, where |ψ⟩ is an arbitrary real-valued four
597
+ qubit state. Now consider the 16 strings where c5 = 0. Since
598
+ the fifth qubit is always mapped to itself, it has to hold that the
599
+ first four qubits are pairwise distinguishable. However, this
600
+ implies a state-independent construction for four qubits which
601
+ is in contradiction to the above. By induction, this implies that
602
+ no state-independent construction can exist whenever n ≥ 4.
603
+ The possibility of state-independent constructions for real-
604
+ valued bi- and tri-partite systems draws heavily on the sim-
605
+ ple structure of skew-symmetric qubit unitaries. If we con-
606
+ sider real-valued systems of dimension d > 2, the situa-
607
+ tion changes considerably.
608
+ Using our necessary and suffi-
609
+ cient condition, it follows immediately that state-independent
610
+ constructions are impossible in all odd dimensions, i.e. when
611
+ (n, d) = (n, 2m+1). This stems from the fact that there exists
612
+ no skew-symmetric unitary matrix in odd dimensions. To see
613
+ that, simply note that if A is skew-symmetric then det(A) =
614
+ det
615
+
616
+ AT �
617
+ = det(−A) = (−1)2m+1 det(A) = − det(A) and
618
+ hence det(A) = 0, but that contradicts unitarity because the
619
+ determinant of a unitary has unit modulus.
620
+ In summary, we have investigated the correspondence be-
621
+ tween entangled states and entangled measurements under lo-
622
+ cal unitary transformations, both when the local transforma-
623
+ tion can and cannot explicitly depend on the target state. Per-
624
+ haps surprisingly, we have found that this problem is not so
625
+ straightforward and has a strong dependence on both the num-
626
+ ber of subsystems involved and their dimension. Our analyt-
627
+ ical and numerical results and conjectures are summarised in
628
+ Table I.
629
+ The conspicuous open problem left by our work is to prove
630
+ our conjecture that there exists states that do not admit a ba-
631
+ sis under local unitaries. An interesting related question is if
632
+ one can bound the relative volume of four-qubit states that do
633
+ not admit a basis. Our numerical investigations suggest that
634
+ nearly all four-qubit states should belong to this class. Fur-
635
+ thermore, it would be useful to find analytical solutions for
636
+ the three-qubit and two-qutrit state-dependent cases. More-
637
+ over, for the state-independent considerations, we focused on
638
+ real Hilbert spaces. A natural question is whether there ex-
639
+ ists state-independent basis constructions for other interest-
640
+ ing spaces. For example, if one restricts to bipartite states
641
+ of a known entanglement entropy, can one construct a state-
642
+ independent basis? The answer is clearly positive for the lim-
643
+ iting cases of product states and maximally entangled states.
644
+ Another interesting space to consider is the symmetric sub-
645
+ space of n-qubit Hilbert space.
646
+
647
+ 5
648
+ Our results may also have prospects in quantum informa-
649
+ tion as one may now construct entangled measurements asso-
650
+ ciated to entangled states. Recently there has been proposals
651
+ of two-qubit entangled projections; the so-called Elegant Joint
652
+ Measurements [18, 19] which have also been realised in vari-
653
+ ous experiments [20? , 21]. The Elegant Joint Measurements
654
+ can be seen as a particular type of |ψ⟩-basis where |ψ⟩ is a
655
+ partially entangled two-qubit state. However, the basis addi-
656
+ tionally has the feature that the collections of reduced states
657
+ form a tetrahedron. This requirement goes beyond our prob-
658
+ lem formulation, as we do not impose any structure on the
659
+ reduced states of our bases. However, it suggests an avenue
660
+ to identifying interesting and highly symmetric measurements
661
+ by finding the particular |ψ⟩-basis that maximises the Hilbert
662
+ space volume spanned its collection of reduced states.
663
+ Finally, one of the notable shortcommings of traditional,
664
+ GHZ based, multiqubit entanglement swapping protocols is
665
+ that the loss of one particle renders the measurement separa-
666
+ ble. However, some other states that are inequivalent to GHZ
667
+ under LOCC can preserve their entanglement under reduc-
668
+ tions. The existence of an iso-entangled basis composed of
669
+ such states may constitute an avenue to more noise-resiliant
670
+ entanglement swapping protocols which have natural quan-
671
+ tum information applications.
672
+ Note added.— During the late stage of our work, we be-
673
+ came aware of the previous work [23] where i. a. bases are
674
+ found for some Dicke states.
675
+ ACKNOWLEDGMENTS
676
+ We thank Hayata Yamasaki,
677
+ Marcus Huber,
678
+ Jakub
679
+ Czartowski and Karol ˙Zyczkowski for discussions. A. T. ac-
680
+ knowledges support from the Wenner-Gren Foundation and
681
+ from the Wallenberg Centre for Quantum Technology. M. J.
682
+ R. acknowledges financial support from the Austrian Science
683
+ Fund (FWF) through BeyondC (F7103-N38), the Project No.
684
+ I-2906, as well as support by the John Templeton Founda-
685
+ tion through Grant 61466, The Quantum Information Struc-
686
+ ture of Spacetime (qiss.fr), the Foundational Questions Insti-
687
+ tute (FQXi) and the research platform TURIS. The opinions
688
+ expressed in this publication are those of the authors and do
689
+ not necessarily reflect the views of the John Templeton Foun-
690
+ dation.
691
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734
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+ schmidt
737
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739
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+ Tanaka,
786
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787
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788
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789
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790
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791
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792
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793
+ of
794
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795
+ information
796
+ onto
797
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798
+ states,
799
+ Journal
800
+ of
801
+ Modern
802
+ Optics
803
+ 54,
804
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805
+ (2007),
806
+ https://doi.org/10.1080/09500340701403301.
807
+ Appendix A: Basis construction for every bipartite state of local dimension d = 4 and d = 8
808
+ Let the local dimension be a power of two, d = 2m, and index the d2 basis elements as (˜j, j) where ˜j = 0, 1, . . . , d − 1
809
+ and j = 1, 2, . . . , d. Let W A
810
+ ψ ⊗ W B
811
+ ψ be the state-dependent local unitaries that transform the general state |ψ⟩ into the Schmidt
812
+ basis, i.e. |ψS⟩ ≡ W A
813
+ ψ ⊗ W B
814
+ ψ |ψ⟩ = �d−1
815
+ l=0 λl |l, l⟩, with the Schmidt coefficients λl ∈ R satisfying �
816
+ l λ2
817
+ l = 1. We now
818
+ further decompose the individual d-dimensional registers as a string of m qubits, writing |l⟩ = |l1 . . . lm⟩. Thus, the Schmidt
819
+ decomposed state reads
820
+ |ψS⟩ =
821
+
822
+ l1,...,lm=0,1
823
+ λl |l1 . . . lm, l1 . . . lm⟩ .
824
+ (A1)
825
+ Once the state has been put in the form (A1), we apply a set of local unitaries that is independent of the Schmidt coefficients.
826
+ For d = 4 and ˜j = 0, the two sets of unitaries read as follows:
827
+ ˜j j
828
+ U (˜j,j)
829
+ 1
830
+ U (˜j,j)
831
+ 2
832
+ U (˜j,j)
833
+ 1
834
+ ⊗ U (˜j,j)
835
+ 2
836
+ |ψS⟩
837
+ 0 1
838
+ 11 ⊗ 11
839
+ 11 ⊗ 11
840
+ λ00 |00, 00⟩ + λ01 |01, 01⟩ + λ10 |10, 10⟩ + λ11 |11, 11⟩
841
+ 0 2
842
+ 11 ⊗ X
843
+ 11 ⊗ XZ
844
+ λ00 |01, 01⟩ − λ01 |00, 00⟩ + λ10 |11, 11⟩ − λ11 |10, 10⟩
845
+ 0 3
846
+ X ⊗ 11
847
+ XZ ⊗ Z
848
+ λ00 |10, 10⟩ − λ01 |11, 11⟩ − λ10 |00, 00⟩ + λ11 |01, 01⟩
849
+ 0 4
850
+ X ⊗ X XZ ⊗ X
851
+ λ00 |11, 11⟩ + λ01 |10, 10⟩ − λ10 |01, 01⟩ − λ11 |00, 00⟩
852
+ (A2)
853
+ In addition, we define U (˜j,j)
854
+ 1
855
+ := X
856
+ ˜j
857
+ 4 U (˜j=0,j)
858
+ 1
859
+ and U (˜j,j)
860
+ 2
861
+ := U (˜j=0,j)
862
+ 2
863
+ , where Xd is the d-dimensional shift-operator Xd =
864
+ �d−1
865
+ l=0 |l + 1⟩⟨l|. Note that, the unitaries U (˜j,j)
866
+ 2
867
+ coincide with the state-independent set for two qubits given in Eq. (2) and
868
+ do not depend on ˜j. At the same time, U (˜j=0,j)
869
+ 1
870
+ are the same as U (˜j,j)
871
+ 2
872
+ where the Z gates are left out. We now show that
873
+ {U (˜j,j)
874
+ 1
875
+ ⊗ U (˜j,j)
876
+ 2
877
+ |ψS⟩}˜j,j is a basis of the bipartite Hilbert space. One can check directly that the four states with ˜j = 0 stated in
878
+ Eq. (A2) above are pairwise orthogonal. We want to mention that we are exploiting the fact that U (˜j=0,j)
879
+ 2
880
+ are the elements of a
881
+ state-independent construction. To see the connection, note that the calculation for the state-independent two-qubit construction
882
+ reads as follows:
883
+ (11 ⊗ 11)(λ00 |00⟩ + λ01 |01⟩ + λ10 |10⟩ + λ11 |11⟩) = λ00 |00⟩ + λ01 |01⟩ + λ10 |10⟩ + λ11 |11⟩ ,
884
+ (A3)
885
+ (11 ⊗ XZ)(λ00 |00⟩ + λ01 |01⟩ + λ10 |10⟩ + λ11 |11⟩) = λ00 |01⟩ − λ01 |00⟩ + λ10 |11⟩ − λ11 |10⟩ ,
886
+ (A4)
887
+ (XZ ⊗ Z)(λ00 |00⟩ + λ01 |01⟩ + λ10 |10⟩ + λ11 |11⟩) = λ00 |10⟩ − λ01 |11⟩ − λ10 |00⟩ + λ11 |01⟩ ,
888
+ (A5)
889
+ (XZ ⊗ X)(λ00 |00⟩ + λ01 |01⟩ + λ10 |10⟩ + λ11 |11⟩) = λ00 |11⟩ + λ01 |10⟩ − λ10 |01⟩ − λ11 |00⟩ .
890
+ (A6)
891
+ Since these states are pairwise orthogonal for arbitrary real coefficients λl1l2, the same holds true for the states in Eq. (A2).
892
+ In addition, all of the states where ˜j = 0 are elements of the subspace spanned by |00, 00⟩, |01, 01⟩, |10, 10⟩ and |11, 11⟩.
893
+ Hence, they form a basis of this four-dimensional subspace.
894
+ By shifting now the first system we obtain a basis for the
895
+ remaining orthogonal subspaces.
896
+ More precisely, since we defined U (˜j,j)
897
+ 1
898
+ = X
899
+ ˜j
900
+ 4 U (˜j=0,j)
901
+ 1
902
+ the states where ˜j = 1 are
903
+ esentially the same states as the ones in Eq. (A2) but with the first system shifted by one l → l ⊕ 1 (mod 4). For example,
904
+ λ00 |11, 10⟩ − λ01 |00, 11⟩ − λ10 |01, 00⟩ + λ11 |10, 01⟩ is the state that corresponds to ˜j = 1 and j = 3. In this way, the
905
+ four states where ˜j = 1 form a basis of the subspace spanned by |01, 00⟩, |10, 01⟩, |11, 10⟩ and |00, 11⟩ (or all states where
906
+ |l + 1, l⟩). Analogously, the four states where ˜j = 2 (˜j = 3) form a basis of the subspaces spanned by the vectors with |l + 2, l⟩
907
+ (|l + 3, l⟩). Altogether, the sixteen states {U (˜j,j)
908
+ 1
909
+ ⊗ U (˜j,j)
910
+ 2
911
+ |ψS⟩}˜j,j form a basis of the entire sixteen dimensional Hilbert space.
912
+ A similar construction can be found for d = 8 by using the state-independent construction of three qubits. Similar as above,
913
+
914
+ 7
915
+ the set for ˜j = 0 reads as follows:
916
+ ˜j j
917
+ U (˜j,j)
918
+ 1
919
+ U (˜j,j)
920
+ 2
921
+ U (˜j,j)
922
+ 1
923
+ ⊗ U (˜j,j)
924
+ 2
925
+ |ψS⟩
926
+ 0 1
927
+ 11 ⊗ 11 ⊗ 11
928
+ 11 ⊗ 11 ⊗ 11
929
+ +λ000 |000, 000⟩ + λ001 |001, 001⟩ + λ010 |010, 010⟩ + λ011 |011, 011⟩
930
+ +λ100 |100, 100⟩ + λ101 |101, 101⟩ + λ110 |110, 110⟩ + λ111 |111, 111⟩
931
+ 0 2
932
+ 11 ⊗ 11 ⊗ X
933
+ Z ⊗ Z ⊗ XZ
934
+ +λ000 |001, 001⟩ − λ001 |000, 000⟩ − λ010 |011, 011⟩ + λ011 |010, 010⟩
935
+ −λ100 |101, 101⟩ + λ101 |100, 100⟩ + λ110 |111, 111⟩ − λ111 |110, 110⟩
936
+ 0 3
937
+ 11 ⊗ X ⊗ 11
938
+ Z ⊗ XZ ⊗ 11
939
+ +λ000 |010, 010⟩ + λ001 |011, 011⟩ − λ010 |000, 000⟩ − λ011 |001, 001⟩
940
+ −λ100 |110, 110⟩ − λ101 |111, 111⟩ + λ110 |100, 100⟩ + λ111 |101, 101⟩
941
+ 0 4
942
+ X ⊗ 11 ⊗ 11
943
+ XZ ⊗ 11 ⊗ 11
944
+ (...)
945
+ 0 5
946
+ 11 ⊗ X ⊗ X
947
+ Z ⊗ X ⊗ XZ
948
+ (...)
949
+ 0 6
950
+ X ⊗ 11 ⊗ X
951
+ X ⊗ 11 ⊗ XZ
952
+ (...)
953
+ 0 7
954
+ X ⊗ X ⊗ 11
955
+ X ⊗ XZ ⊗ Z
956
+ (...)
957
+ 0 8
958
+ X ⊗ X ⊗ X X ⊗ XZ ⊗ X
959
+ (...)
960
+ (A7)
961
+ Again, we define U (˜j,j)
962
+ 1
963
+ = X
964
+ ˜j
965
+ 8 U (˜j=0,j)
966
+ 1
967
+ and U (˜j,j)
968
+ 2
969
+ = U (˜j=0,j)
970
+ 2
971
+ . The proof that this forms a basis of the 64-dimension Hilbert
972
+ space is completely analogous to the case of d = 4 before. The eight states for ˜j = 0 form a basis of the eight-dimensional
973
+ subspace spanned by |l1l2l3, l1l2l3⟩ (for li = 0, 1). Applying the shift operator X8 to the first system, one obtains bases of the
974
+ other eight-dimensional orthogonal subspaces spanned by the vectors with
975
+ ��l + ˜j, l
976
+
977
+ . This approach cannot (immediately) be
978
+ generalized to higher dimensions d = 2n, due to the lack of state-independent constructions for n ≥ 4 qubits. However, there is
979
+ in principle no reason to restrict the unitaries on the second system to tensor products of single qubit Pauli gates as we do here.
980
+ In principle, we could also consider general permutations with suitably chosen signs such that all terms cancel in this pairwise
981
+ sense as above. Even when considering this larger class of possibilities, we made an exhaustive search and could not find any
982
+ additional construction. Due to this, it seems unlikely that a construction exists in which the unitaries do not depend on the
983
+ Schmidt coefficients.
984
+ Appendix B: An n-qubit basis of W-states
985
+ We define the n-qubit W-state as
986
+ |W1⟩ ≡ |1⟩
987
+ |W2⟩ ≡
988
+ 1
989
+
990
+ 2 (|01⟩ + |10⟩)
991
+ |W3⟩ ≡
992
+ 1
993
+
994
+ 3 (|001⟩ + |010⟩ + |100⟩)
995
+ |W4⟩ ≡ 1
996
+ 2 (|0001⟩ + |0010⟩ + |0100⟩ + |1000⟩)
997
+ ...
998
+ (B1)
999
+ Note that for one and two qubits, the definition is only introduced for sake of convenience. In general, we write
1000
+ |Wn⟩ ≡
1001
+ 1
1002
+ √n
1003
+
1004
+ σ
1005
+ σ(|0⟩⊗n−1 |1⟩),
1006
+ (B2)
1007
+ where σ runs over all permutations of the position of “1”. It is also useful to write the state recursively as
1008
+ |Wn+1⟩ =
1009
+
1010
+ n
1011
+ n + 1 |Wn⟩ ⊗ |0⟩ +
1012
+ 1
1013
+ √n + 1 |0⟩n ⊗ |1⟩
1014
+ (B3)
1015
+ Clearly, if we apply the local unitaries U (1)
1016
+ 1
1017
+ = 11 and U (2)
1018
+ 1
1019
+ = X to |W1⟩ we generate the trivial one-qubit W-basis {|0⟩ , |1⟩}.
1020
+ Assume now that the local unitaries {U (j)
1021
+ k } for k = 1, . . . n and j = 1, . . . , 2n yield a |Wn⟩-basis. We will now show that under
1022
+ this assumption we can construct a basis for |Wn+1⟩ and hence it follows from induction that a W-basis exists for any number
1023
+ of qubits.
1024
+
1025
+ 8
1026
+ We illustrate the induction step as follows,
1027
+ U (1)
1028
+ 1
1029
+
1030
+ U (1)
1031
+ 2
1032
+ ⊗ . . . ⊗
1033
+ U (1)
1034
+ n
1035
+
1036
+ 11
1037
+ U (2)
1038
+ 1
1039
+
1040
+ U (2)
1041
+ 2
1042
+ ⊗ . . . ⊗
1043
+ U (2)
1044
+ n
1045
+
1046
+ 11
1047
+ ...
1048
+ ...
1049
+ ...
1050
+ U (2n)
1051
+ 1
1052
+
1053
+ U (2n)
1054
+ 2
1055
+ ⊗ . . . ⊗
1056
+ U (2n)
1057
+ n
1058
+
1059
+ 11
1060
+ U (1)
1061
+ 1 Z
1062
+
1063
+ U (1)
1064
+ 2 Z
1065
+ ⊗ . . . ⊗
1066
+ U (1)
1067
+ n Z
1068
+ ⊗ X
1069
+ U (2)
1070
+ 1 Z
1071
+
1072
+ U (2)
1073
+ 2 Z
1074
+ ⊗ . . . ⊗
1075
+ U (2)
1076
+ n Z
1077
+ ⊗ X
1078
+ ...
1079
+ ...
1080
+ ...
1081
+ U (2n)
1082
+ 1
1083
+ Z ⊗ U (2n)
1084
+ 2
1085
+ Z ⊗ . . . ⊗ U (2n)
1086
+ n
1087
+ Z ⊗ X
1088
+ .
1089
+ (B4)
1090
+ We see that for the first 2n basis elements, we extend the unitaries for n qubits by tensoring with 11 for qubit number n + 1.
1091
+ For the latter 2n basis elements, we extend the unitaries for n qubits by multiplying all of them from the right by Z and finally
1092
+ tensoring with X for qubit number n + 1. As usual, we now write the string of unitaries associated to each row as V (n+1)
1093
+ j
1094
+ for
1095
+ n = 1, . . . , 2n+1. We similarly use V (n)
1096
+ j
1097
+ for the unitary strings for the case of n qubits.
1098
+ To see that this yields a basis, we first show that the first 2n basis elements (upper block of table, j = 1, . . . , 2n) are orthogonal.
1099
+ For this purpose, we use the recursion formula (B3) to write for j ̸= j′
1100
+ ⟨Wn+1|(V (n+1)
1101
+ j′
1102
+ )†V (n+1)
1103
+ j
1104
+ |Wn+1⟩ =
1105
+ n
1106
+ n + 1⟨Wn0|(V (n)
1107
+ j′
1108
+ )†V (n)
1109
+ j
1110
+ ⊗ 11|Wn0⟩ +
1111
+ 1
1112
+ n + 1⟨0 . . . 01|(V (n)
1113
+ j′
1114
+ )†V (n)
1115
+ j
1116
+ ⊗ 11|0 . . . 01⟩
1117
+ +
1118
+ √n
1119
+ n + 1⟨Wn0|(V (n)
1120
+ j′
1121
+ )†V (n)
1122
+ j
1123
+ ⊗ 11|0 . . . 01⟩ +
1124
+ √n
1125
+ n + 1⟨0 . . . 01|(V (n)
1126
+ j′
1127
+ )†V (n)
1128
+ j
1129
+ ⊗ 11|Wn0⟩ = 0
1130
+ The first term is zero for all j′ ̸= j due to the induction hypothesis. The third and fourth terms are zero due to orthogonality in
1131
+ the last qubit register. The second term is zero for every j′ ̸= j there exists at least one qubit register k for which U (j′)
1132
+ k
1133
+ and U (j)
1134
+ k
1135
+ are composed of different numbers of bit-flips (X). The latter follows from the initial condition of using {11, X} to construct the
1136
+ |W1⟩-basis.
1137
+ The same procedure will analogously show that the latter 2n basis elements (lower block of the table, j = 2n + 1, . . . , 2n+1)
1138
+ are orthogonal. We are left with showing that every overlap between the upper and lower block, i.e. with any j′ = 1, . . . , 2n and
1139
+ any j = 2n + 1, . . . , 2n+1, also vanishes. For this we have
1140
+ ⟨Wn+1|(V (n+1)
1141
+ j′
1142
+ )†V (n+1)
1143
+ j
1144
+ |Wn+1⟩ =
1145
+ n
1146
+ n + 1⟨Wn0|
1147
+
1148
+ (V (n)
1149
+ j′
1150
+ )†V (n)
1151
+ j
1152
+ ⊗ X
1153
+
1154
+ n
1155
+
1156
+ k=1
1157
+ Z ⊗ 11|Wn0⟩
1158
+ +
1159
+ 1
1160
+ n + 1⟨0 . . . 01|
1161
+
1162
+ (V (n)
1163
+ j′
1164
+ )†V (n)
1165
+ j
1166
+ ⊗ X
1167
+
1168
+ n
1169
+
1170
+ k=1
1171
+ Z ⊗ 11|0 . . . 01⟩
1172
+ +
1173
+ √n
1174
+ n + 1⟨Wn0|
1175
+
1176
+ (V (n)
1177
+ j′
1178
+ )†V (n)
1179
+ j
1180
+ ⊗ X
1181
+
1182
+ n
1183
+
1184
+ k=1
1185
+ Z ⊗ 11|0 . . . 01⟩
1186
+ +
1187
+ √n
1188
+ n + 1⟨0 . . . 01|
1189
+
1190
+ (V (n)
1191
+ j′
1192
+ )†V (n)
1193
+ j
1194
+ ⊗ X
1195
+
1196
+ n
1197
+
1198
+ k=1
1199
+ Z ⊗ 11|Wn0⟩
1200
+ Note that �n
1201
+ k=1 Z ⊗ 11 |Wn0⟩ = − |Wn0⟩ and �n
1202
+ k=1 Z ⊗ 11 |0 . . . 01⟩ = |0 . . . 01⟩. The first and second terms are both zero due
1203
+ to orthogonality in the final qubit register. We thus have
1204
+ ⟨Wn+1|(V (n+1)
1205
+ j′
1206
+ )†V (n+1)
1207
+ j
1208
+ |Wn+1⟩ =
1209
+ √n
1210
+ n + 1⟨Wn|(V (n)
1211
+ j′
1212
+ )†V (n)
1213
+ j
1214
+ |0 . . . 0⟩ −
1215
+ √n
1216
+ n + 1⟨0 . . . 0|(V (n)
1217
+ j′
1218
+ )†V (n)
1219
+ j
1220
+ |Wn⟩
1221
+ =
1222
+ √n
1223
+ n + 1⟨Wn|(V (n)
1224
+ j′
1225
+ )†V (n)
1226
+ j
1227
+ − (V (n)
1228
+ j
1229
+ )†V (n)
1230
+ j′
1231
+ |0 . . . 0⟩ = 0.
1232
+ (B5)
1233
+ The last equality follows from the fact that it is sufficient, for given (j, j′), that there exist some register index k such that
1234
+ (U (j′))†
1235
+ kU (j)
1236
+ k
1237
+ − (U (j))†
1238
+ kU (j′)
1239
+ k
1240
+ = 0 in order for the overlap to vanish. This is always the case because due to our construction (see
1241
+ initial condition and the table), for every two unitaries there is at least one register k where the single-qubit unitaries differ by
1242
+ X, meaning that either (U (j)
1243
+ k , U (j′)
1244
+ k
1245
+ ) = (11, X)/(Z, XZ), or the same with j ↔ j′ is true. The condition above is satisfied by
1246
+ all of these combinations. Hence we conclude that the proposed construction satisfies
1247
+ ⟨Wn+1|(V (n+1)
1248
+ j
1249
+ )†V (n+1)
1250
+ j′
1251
+ |Wn+1⟩ = δjj′
1252
+ (B6)
1253
+
1254
+ 9
1255
+ and therefore yields a W-state basis for any number of qubits.
1256
+ Appendix C: The Pauli structure for state-independent qubit unitary constructions
1257
+ We consider the set of local unitaries P that are applied to the i-th qubit in the state-independent construction and show that
1258
+ without loss of generality, the set can be chosen to be the Pauli-type gates P ≡ {11, X, Z, XZ}. First, note that the set is finite
1259
+ since there are exactly 2n basis states. Next, we observe that the identity 11 has to be within the set P since we demand that
1260
+ V1 = 11. Furthermore, we can argue that the gate
1261
+ XZ =
1262
+
1263
+ 0 −1
1264
+ 1
1265
+ 0
1266
+
1267
+ has to be within the set as well, since it is the only gate that maps every real qubit state to its orthogonal state. More precisely,
1268
+ if it is not used on the i-th qubit at least once, one can choose a real qubit state |φi⟩ such that none of the gates in P map
1269
+ |φi⟩ to its orthogonal vector. Hence if we apply the state-independent construction to the real-valued product state |φ⟩ =
1270
+ |0⟩1 ⊗ . . . |0⟩i−1 ⊗ |φi⟩ ⊗ |0⟩i+1 ⊗ . . . ⊗ |0⟩n none of the resulting 2n states are distinguishable on the i-th qubit, which is
1271
+ impossible if these states should form a basis of product states. Therefore, the gate XZ has to be within the set P. Apart from
1272
+ the gates 11 and XZ we can constrain which other qubit unitaries can be in the set P. We know that if we demand V1 = 11, every
1273
+ string of local unitaries (Vj) and their products (Vj)†Vj′ with j ̸= j′ have to be skew-symmetric. As a result, the local unitaries
1274
+ on each subsystem (hence, the unitaries in the set P) and also all their products have to be either symmetric or skew-symmetric.
1275
+ By neglecting a global phase, the general form of a unitary operator can be written as:
1276
+ U =
1277
+
1278
+ cos (θ)eiα
1279
+ sin (θ)eiβ
1280
+ − sin (θ)e−iβ cos (θ)e−iα
1281
+
1282
+ .
1283
+ (C1)
1284
+ The only skew-symmetric 2×2 unitary is, up to an irrelevant global phase, the Pauli-type operator XZ, which we already found
1285
+ to be necessarily in the set P. All the symmetric matrices of this form can be written as:
1286
+ U =
1287
+
1288
+ cos (θ)eiα
1289
+ i sin (θ)
1290
+ i sin (θ) cos (θ)e−iα
1291
+
1292
+ .
1293
+ (C2)
1294
+ If the gate U is in P, it is at some point multiplied with the gate XZ since the operator XZ is used at least once on the i-th qubit.
1295
+ Since we know that the result of this product has to be again either symmetric or skew-symmetric, we obtain that α = π/2, 3π/2
1296
+ due to:
1297
+ (XZ)†U =
1298
+
1299
+ 0 1
1300
+ −1 0
1301
+ � �
1302
+ cos (θ)eiα
1303
+ i sin (θ)
1304
+ i sin (θ) cos (θ)e−iα
1305
+
1306
+ =
1307
+
1308
+ i sin (θ) cos (θ)e−iα
1309
+ − cos (θ)eiα
1310
+ −i sin (θ)
1311
+
1312
+ .
1313
+ (C3)
1314
+ The two possibilities for α = π/2, 3π/2 correspond to the two solutions
1315
+ U1 =
1316
+
1317
+ cos (θ)
1318
+ sin (θ)
1319
+ sin (θ) − cos (θ)
1320
+
1321
+ ,
1322
+ U2 =
1323
+
1324
+ sin (θ) − cos (θ)
1325
+ − cos (θ) − sin (θ)
1326
+
1327
+ .
1328
+ (C4)
1329
+ We left the irrelevant global factor i for simplicity. Considering the additional degree of freedom of θ, we can restrict to the first
1330
+ class of solutions U1 since the second class U2 can be obtained by shifting θ by π/2. Hence, if we add a gate U to the set P, it
1331
+ has to be of the form given by U1 above. Now if we add two such gates to the set P, the product of U1 with another valid matrix
1332
+ U ′
1333
+ 1 is
1334
+ U †
1335
+ 1U ′
1336
+ 1 =
1337
+
1338
+ cos (θ)
1339
+ sin (θ)
1340
+ sin (θ) − cos (θ)
1341
+ � �
1342
+ cos (θ′)
1343
+ sin (θ′)
1344
+ sin (θ′) − cos (θ′)
1345
+
1346
+ =
1347
+ =
1348
+
1349
+ cos (θ) cos (θ′) + sin (θ) sin (θ′)
1350
+ cos (θ) sin (θ′) − sin (θ) cos (θ′)
1351
+ sin (θ) cos (θ′) − cos (θ) sin (θ′)
1352
+ cos (θ) cos (θ′) + sin (θ) sin (θ′)
1353
+
1354
+ =
1355
+
1356
+ cos (θ − θ′)
1357
+ − sin (θ − θ′)
1358
+ sin (θ − θ′)
1359
+ cos (θ − θ′)
1360
+
1361
+ If both, U1 and U ′
1362
+ 1, are in P, this product has to be again either symmetric, which is true if θ = θ′ or skew-symmetric, which is
1363
+ true if θ = θ′ + π/2. (Note that, also θ = θ′ + π and θ = θ′ + 3π/2 are possible solutions but we do not have to consider them
1364
+
1365
+ 10
1366
+ since they just differ by an irrelevant global factor of (−1) in one of the two unitaries.) Hence, U ′
1367
+ 1 is either U1 or the unitary U2
1368
+ stated above. Hence, for each single-qubit subsystem, we can only use a set of operators P ≡ {11, U1, U2, XZ} for our basis
1369
+ construction.
1370
+ In a final step, we can show that we can restrict also θ. To see this, suppose a state-independent construction exists where we
1371
+ use the gates from the set P ≡ {11, U1, U2, XZ}. Now consider the construction where each gate U1 is replaced with W †U1W,
1372
+ each gate U2 with W †U2W, each gate XZ with W †XZW and each gate 11 with W †11W, where:
1373
+ W =
1374
+
1375
+ cos (α) − sin (α)
1376
+ sin (α)
1377
+ cos (α)
1378
+
1379
+ (C5)
1380
+ for some freely chosen parameter α. This also has to be a state-independent construction for any state with real coefficients,
1381
+ since W is a map from real states to real states, and all inner products between the basis states remain the same under this
1382
+ local transformation. Hence, if a state-independent construction exists with the gate set P ≡ {11, U1, U2, XZ}, another state-
1383
+ independent construction with the gate set P′ ≡ {W †11W, W †U1W, W †U2W, W †XZW} has to exist as well. Choosing
1384
+ α = θ/2, the set P′ ≡ {W †11W, W †U1W, W †U2W, W †XZW} becomes exactly P′ ≡ {11, X, Z, XZ}, which concludes the
1385
+ proof.
1386
+
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1
+ arXiv:2301.01268v1 [math.CV] 3 Jan 2023
2
+ Proper holomorphic maps in Euclidean spaces
3
+ avoiding unbounded convex sets
4
+ Barbara Drinovec Drnovˇsek and Franc Forstneriˇc
5
+ Abstract We show that if E is a closed convex set in Cn (n > 1) contained in a closed halfspace H such
6
+ that E ∩ bH is nonempty and bounded, then the concave domain Ω = Cn \ E contains images of proper
7
+ holomorphic maps f : X → Cn from any Stein manifold X of dimension < n, with approximation of
8
+ a given map on closed compact subsets of X. If in addition 2 dim X + 1 ≤ n then f can be chosen an
9
+ embedding, and if 2 dim X = n then it can be chosen an immersion. Under a stronger condition on E
10
+ we also obtain the interpolation property for such maps on closed complex subvarieties.
11
+ Keywords Stein manifold, holomorphic embedding, Oka manifold, minimal surface, convexity
12
+ MSC (2010): 32H02, 32Q56; 52A20, 53A10
13
+ Date: 3 January 2023
14
+ In memoriam Nessim Sibony
15
+ 1. Introduction
16
+ Let X be a Stein manifold. Denote by O(X, Cn) the Frechet space of holomorphic maps
17
+ X → Cn endowed with the compact-open topology and write O(X, C) = O(X). A theorem of
18
+ Remmert [36] (1956), Narasimhan [35] (1960), and Bishop [7] (1961) states that almost proper
19
+ maps are residual in O(X, Cn) if dim X = n, proper maps are dense if dim X < n, proper
20
+ immersions are dense if 2 dim X ≤ n, and proper embeddings are dense if 2 dim X < n. A
21
+ proof is also given in the monograph [29] by Gunning and Rossi.
22
+ It is natural to ask how much space proper maps need. We pose the following question.
23
+ Problem 1.1. For which domains Ω ⊂ Cn are proper holomorphic maps (immersions,
24
+ embeddings) X → Cn as above, with images contained in Ω, dense in O(X, Ω)?
25
+ It is evident that Ω cannot be contained in a halfspace of Cn since every holomorphic map
26
+ from C to a halfspace lies in a complex hyperplane. In this paper we give an affirmative answer
27
+ for concave domains whose complement E = Cn \ Ω satisfies the following condition.
28
+ Definition 1.2. A closed convex set E in a real or complex Euclidean space V has bounded
29
+ convex exhaustion hulls (BCEH) if for every compact convex set K in V
30
+ (1.1)
31
+ the set h(E, K) = Conv(E ∪ K) \ E is bounded.
32
+ Here, Conv denotes the convex hull. The following is our first main result.
33
+ Theorem 1.3. Let E be an unbounded closed convex set in Cn (n > 1) with bounded convex
34
+ exhaustion hulls. Given a Stein manifold X with dim X < n, a compact O(X)-convex set K in
35
+ X, and a holomorphic map f0 : K → Cn with f0(bK) ⊂ Ω = Cn \ E, we can approximate f0
36
+ uniformly on K by proper holomorphic maps f : X → Cn satisfying f(X \ ˚
37
+ K) ⊂ Ω. The map
38
+ f can be chosen an embedding if 2 dim X < n and an immersion if 2 dim X ≤ n.
39
+
40
+ 2
41
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
42
+ In this paper, a map f : K → Cn from a compact set K is said to be holomorphic if it is the
43
+ restriction to K of a holomorphic map on an open neighbourhood of K.
44
+ In particular, if f0(K) ⊂ Ω then the theorem gives uniform approximation of f0 by proper
45
+ holomorphic maps f : X → Cn with f(X) ⊂ Ω. If bE is of class C 1 and strictly convex
46
+ near infinity, we obtain an analogue of Theorem 1.3 with additional interpolation on a closed
47
+ complex subvariety X′ of X such that f0 : X′ → Cn is proper holomorphic; see Theorem 4.2.
48
+ Without the condition on the range, interpolation of proper holomorphic embeddings X ֒→ Cn
49
+ on a closed complex subvariety was obtained by Acquistapace et al. [1] in 1975.
50
+ The analogue of the BCEH condition for unbounded closed sets in Stein manifolds, with the
51
+ convex hull replaced by the holomorphically convex hull, is used in holomorphic approximation
52
+ theory of Arakelyan and Carleman type; see the survey in [18].
53
+ It is evident that a closed convex set E ⊂ Rn has BCEH if and only if there is an increasing
54
+ sequence K1 ⊂ K2 ⊂ · · · of compact convex sets exhausting Rn such that the set h(E, Kj) (see
55
+ (1.1)) is bounded for every j = 1, 2, . . .. In particular, BCEH is a condition at infinity which is
56
+ invariant under perturbations supported on a compact subset. For compact convex sets E ⊂ Cn,
57
+ Theorem 1.3 was proved in [24]; in this case BCEH trivially holds.
58
+ We show in Section 3 that a closed convex set E in Rn has BCEH if and only if E is
59
+ continuous in the sense of Gale and Klee [26]; see Proposition 3.3. If E has BCEH then
60
+ Conv(E ∪ K) is closed for any compact convex set K ⊂ Rn (see [26, Theorem 1.5]). If such E
61
+ is unbounded, which is the main case of interest, there are affine coordinates (x, y) ∈ Rn−1 × R
62
+ such that E = Eφ = {(x, y) ∈ Rn : y ≥ φ(x)} is the epigraph of a convex function
63
+ φ : Rn−1 → R+ = [0, +∞) growing at least linearly near infinity (see Proposition 3.4). In
64
+ particular, an unbounded closed convex set E ⊂ Cn with BCEH is of the form
65
+ (1.2)
66
+ E = Eφ = {z = (z′, zn) ∈ Cn : ℑzn ≥ φ(z′, ℜzn)}
67
+ in some affine complex coordinates z = (z′, zn) on Cn, with φ as above. (Here, ℜ and ℑ denote
68
+ the real and the imaginary part.) For a convex function φ of class C 1 we give a differential
69
+ characterization of the BCEH condition on its epigraph Eφ; see Proposition 3.8. The BCEH
70
+ property holds if the radial derivative of φ tends to infinity; see Corollary 3.9. On the other hand,
71
+ there are convex functions of linear growth whose epigraphs have BCEH; see Example 3.10. By
72
+ Proposition 3.11, a convex function φ with at least linear growth at infinity can be approximated
73
+ uniformly on compacts by functions ψ ≤ φ of the same kind whose epigraphs Eψ have BCEH.
74
+ This allows us to extend Theorem 1.3 as follows; see Section 4 for the proof.
75
+ Corollary 1.4. The conclusion of Theorem 1.3 holds for any convex epigraph Eφ of the form
76
+ (1.2) such that φ ≥ 0 and the set {φ = 0} is nonempty and compact.
77
+ A closed convex set E ⊂ Cn with BCEH does not contain any affine real line (see Proposition
78
+ 3.4), and for n > 1 its complement Ω = Cn \ E is an Oka domain according to Wold and the
79
+ second named author; see [25, Theorem 1.8]. This fact plays an important role in our proof
80
+ of Theorem 1.3, given in Section 4. (The precise result from Oka theory which we shall use
81
+ is stated as Theorem 4.1.) Among closed convex epigraphs (1.2), the class of sets with Oka
82
+ complement is strictly bigger than the class of sets with BCEH. In particular, the former class
83
+ contains many sets containing boundary lines, which is impossible for a set with BCEH.
84
+ Problem 1.5. Is there a (not necessarily convex) set Eφ ⊂ Cn of the form (1.2) with φ ≥ 0 of
85
+ sublinear growth for which Theorem 1.3 holds? Is there a set of this kind in C2 such that C2\Eφ
86
+ contains the image of a proper holomorphic disc D = {z ∈ C : |z| < 1} → C2?
87
+
88
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
89
+ 3
90
+ Theorem 1.3 is the first general result in the literature providing proper holomorphic maps
91
+ X → Cn from any Stein manifold of dimension < n whose images avoid large convex sets in
92
+ Cn close to a halfspace, and with approximation of a given map on a compact holomorphically
93
+ convex set in X. Without the approximation condition and assuming that dim X ≤ n − 2, there
94
+ are proper holomorphic maps of X into a complex hyperplane in Cn \ E.
95
+ On the other hand, there are many known results concerning proper holomorphic maps in
96
+ Euclidean spaces and in more general Stein manifolds whose images avoid certain small closed
97
+ subsets, such as compact or complete pluripolar ones, and results in which the source manifold
98
+ is the disc D = {z ∈ C : |z| < 1}. Proper holomorphic discs in C2 avoiding closed complete
99
+ pluripolar sets of the form E = E′ × C, with E′ ⊂ C, were constructed by Alexander [5] in
100
+ 1977. The first named author showed in [13] (2004) that for every closed complete pluripolar
101
+ set E in a Stein manifold Y with dim Y > 1 and point p ∈ Y \ E there is a proper holomorphic
102
+ disc f : D → Y with p ∈ f(D) ⊂ Y \ E. If Y = C2 there also exist embedded holomorphic
103
+ discs with this property according to Borell et al. [8] (2008), and for dim Y ≥ 3 this holds
104
+ by the general position argument. Proper holomorphic discs in C2 with images contained in
105
+ certain concave cones were constructed by Globevnik and the second named author [23] in
106
+ 2001. They also constructed proper holomorphic discs in C2 with images in (C \ {0})2, and
107
+ hence proper harmonic discs D → R2, disproving a conjecture by Schoen and Yau [37, p. 18].
108
+ (Another construction of such maps was given by Boˇzin [9].) More generally, it was shown
109
+ by Alarc´on and L´opez [4, Corollary 1.1] in 2012 that every open Riemann surface X admits a
110
+ proper harmonic map to R2 which is the projection of a conformal minimal immersion X → R3.
111
+ The aforementioned result from [23] was used by the first named author in [12] (2002) to classify
112
+ closed convex sets in C2 whose complement is filled by images of holomorphic discs which are
113
+ proper in C2. More recently, Forstneriˇc and Ritter [24] (2014) proved Theorem 1.3 in the case
114
+ when E ⊂ Cn is a compact polynomially convex set and 2 dim X ≤ n (for immersions) or
115
+ 2 dim X < n (for embeddings), and for proper holomorphic maps X → Cn when dim X < n
116
+ and E is a compact convex set. A further development in this direction is the analogue of
117
+ Theorem 1.3 when Cn is replaced by a Stein manifold Y with the density property and E ⊂ Y
118
+ is a compact O(Y )-convex set; see [22, Remark 4.5] and the references therein. However, in all
119
+ mentioned results except those in [23, 12], the avoided sets are thin or compact.
120
+ Without insisting on approximation, the theorem of Remmert, Bishop, and Narasimhan is not
121
+ optimal with respect to the dimension of the target space. Indeed, it was shown by Eliashberg and
122
+ Gromov [17] in 1992, with an improvement for odd dimensional Stein manifolds by Sch¨urmann
123
+ [38] in 1997, that a Stein manifold X of dimension m ≥ 2 embeds properly holomorphically
124
+ in Cn with n =
125
+ �3m
126
+ 2
127
+
128
+ + 1, and for m ≥ 1 it immerses properly holomorphically in Cn with
129
+ n =
130
+ � 3m+1
131
+ 2
132
+
133
+ . (See also [20, Sect. 9.3].) However, the construction method in these papers,
134
+ which relies on the Oka principle for sections of certain stratified holomorphic fibre bundles,
135
+ does not give the density statement, and we do not know whether Theorem 1.3 holds for maps to
136
+ these lower dimensional spaces. It is also an open problem whether every open Riemann surface
137
+ embeds properly holomorphically in C2; see [20, Secs. 9.10-9.11] and the survey [21].
138
+ Theorem 1.3 is proved in Section 4. The proof relies on two main ingredients. One is the
139
+ result of Wold and the second named author [25, Theorem 1.8] which shows in particular that the
140
+ complement Ω = Cn \E of a closed convex set E having BCEH is an Oka domain. The second
141
+ main technique comes from the work of Dor [10, 11] (1993-95), following earlier papers by
142
+ Stensønes [39] (1989) and Hakim [30] (1990). Dor constructed proper holomorphic immersions
143
+ and embeddings of any smoothly bounded, relatively compact, strongly pseudoconvex domain
144
+ D in a Stein manifold X into any pseudoconvex domain Ω in Cn under the dimension conditions
145
+
146
+ 4
147
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
148
+ in Theorem 1.3.
149
+ Previously, Hakim [30] constructed proper holomorphic maps to balls in
150
+ codimension one. The main idea is to inductively lift the image of bD under a holomorphic
151
+ map f : ¯D → Ω to a given higher superlevel set of a strongly plurisubharmonic exhaustion
152
+ function ρ : Ω → R+ in a controlled way, taking care not to decrease the value of ρ ◦ f very
153
+ much anywhere on D during the process. When D is a finite bordered Riemann surface, this can
154
+ be achieved by using approximate solutions of a Riemann-Hilbert boundary value problem (see
155
+ [14]). In higher dimensions the proof is more subtle and uses carefully controlled holomorphic
156
+ peak functions on ¯D to push a given map f : ¯D → Ω locally at a point z ∈ f(bD) in the direction
157
+ of the zero set Sz of the holomorphic (quadratic) Levi polynomial of the exhaustion function
158
+ ρ : Ω → R. At a noncritical point z ∈ Ω of ρ, Sz is a smooth local complex hypersurface and
159
+ the restricted function ρ|Sz increases quadratically as we move away from z. If ρ is a strictly
160
+ convex function, this can be achieved by pushing the image of f(bD) in the direction of suitably
161
+ chosen affine complex hyperplanes. Dor’s construction was extended by the authors to maps
162
+ from strongly pseudoconvex domains in Stein manifolds to an arbitrary Stein manifold Ω, and
163
+ also to q-convex complex manifolds for suitable values of q ∈ N; see the papers [14, 15] from
164
+ 2007 and 2010, respectively. In those papers we introduced the technique of gluing holomorphic
165
+ sprays of manifold-valued maps on a strongly pseudoconvex Cartan pair with control up to the
166
+ boundary (a nonlinear version of the Cousin-I problem) and a systematic approach for avoiding
167
+ critical points of a q-convex Morse exhaustion function on Ω.
168
+ Earlier constructions of this type, using simpler holomorphic peak functions and higher
169
+ codimension, were given in 1985 by Løw [34] and Forstneriˇc [19] who showed that every
170
+ relatively compact strongly pseudoconvex domain D in a Stein manifold embeds properly
171
+ holomorphically in a high dimensional Euclidean ball. A related result with interpolation on
172
+ a suitable subset of the boundary of D is due to Globevnik [27] (1987). This peak function
173
+ technique was inspired by the construction of inner functions on the ball of Cn by Løw [33] in
174
+ 1982, based on the work of Hakim and Sibony [31].
175
+ We apply this technique to push the boundary f0(bD) ⊂ Ω = Cn \ E of a holomorphic map
176
+ f0 : ¯D → Cn in Theorem 1.3 out of a certain compact convex cap C attached to E along a part
177
+ of bC contained in bE and such that the set E1 = E ∪ C is convex and has bounded convex
178
+ exhaustion hulls. At the same time, we ensure that the new map g : ¯D → Cn still sends D \ K
179
+ to Ω. For a precise result, see Proposition 2.1. In the next step, we use that Ω1 = Cn \ E1 is
180
+ an Oka domain (see Corollary 3.6). Since g(bD) ⊂ Ω1, we can apply the Oka principle (see
181
+ Theorem 4.1) to approximate g by a holomorphic map f1 : X → Cn with f1(X \ D) ⊂ Ω1.
182
+ Continuing inductively, we obtain a sequence of holomorphic maps X → Cn converging to a
183
+ proper map satisfying Theorem 1.3. The details are given in Section 4.
184
+ The analogues of Theorem 1.3 and Corollary 1.4 also hold for minimal surfaces in Rn.
185
+ Theorem 1.6. Let n ≥ 3, and let φ : Rn−1 → R+ be a convex function such that the set {φ = 0}
186
+ is nonempty and compact. Given an open Riemann surface X, a compact O(X)-convex set K
187
+ in X, and a conformal minimal immersion f0 : U → Rn from a neighbourhood of K with
188
+ f0(bK) ⊂ Ω = {y < φ(x)}, we can approximate f0 uniformly on K by proper conformal
189
+ minimal immersions f : X → Rn (embeddings if n ≥ 5) satisfying f(X \ ˚
190
+ K) ⊂ Ω.
191
+ If in addition φ is of class C 1, strictly convex at infinity, and the epigraph Eφ = {y ≥ φ(x)}
192
+ has BCEH then one can add to this statement the interpolation of the map on discrete sets, in
193
+ analogy to Theorem 4.2.
194
+ Theorem 1.6 is obtained by following the proof of Theorem 1.3, replacing Proposition 2.1
195
+ by the analogous result obtained by the Riemann–Hilbert deformation method for conformal
196
+
197
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
198
+ 5
199
+ minimal surfaces (see [2] or [3, Chapter 6]). Furthermore, it has recently been shown by the
200
+ authors [16, Corollary 1.5] that the complement of a closed convex set E ⊂ Rn (n ≥ 3) is
201
+ flexible for minimal surfaces (an analogue of the Oka property in complex geometry) if and only
202
+ if E is not a halfspace or a slab; clearly this includes all sets with BCEH.
203
+ Another method for constructing proper minimal surfaces, which yields the same result in
204
+ some examples not covered by Theorem 1.6, was developed by Alarc´on and L´opez [4] in 2012.
205
+ They showed that Theorem 1.6 holds for any wedge domain Γ × R ⊂ R3, where Γ ⊂ R2 is an
206
+ open cone with angle > π; see [4, Theorem 5.6]. The complement of this set is convex but it
207
+ fails to satisfy the hypotheses of Theorem 1.6 due to the presence of lines in the boundary. An
208
+ important difference between these two fields, which affects the possible construction methods,
209
+ is that every open Riemann surface admits a proper harmonic map to the plane R2 (see [4,
210
+ Theorem I]), while only few such surfaces admit proper holomorphic maps to C.
211
+ The analogue of Problem 1.5 for minimal surfaces asks whether there is a domain in R3 of
212
+ the form {x3 < φ(x1, x2)}, where φ : R2 → R+ is a function with sublinear growth, which
213
+ contains minimal surfaces of hyperbolic type that are proper in R3, or just a proper hyperbolic
214
+ end of a minimal surface. In particular, it would be interesting to know whether the domain
215
+ below the upper half of a vertical catenoid has this property. On the other hand, the strong
216
+ halfspace theorem of Hoffman and Meeks [32] says that the only proper minimal surfaces in R3
217
+ contained in a halfspace are planes.
218
+ 2. Pushing a strongly pseudoconvex boundary out of a strictly convex cap
219
+ Let O be a convex domain in Cn for some n > 1. Recall that a continuous function ρ : O → R
220
+ is said to be strictly convex if for any pair of points a, b ∈ O we have that
221
+ ρ(ta + (1 − t)b) < tρ(a) + (1 − t)ρ(b) for all 0 < t < 1.
222
+ Assume now that ρt : O → R (t ∈ [0, 1]) is a continuous family of C 1 functions satisfying
223
+ the following conditions:
224
+ (a) For every t ∈ [0, 1] the function ρt is strictly convex. Note that dρt ̸= 0 on Mt := {ρt = 0}.
225
+ (b) If 0 ≤ s < t ≤ 1 then ρt ≤ 0 on Ms.
226
+ (c) There is an open relatively compact subset ω0 of M0 such that for every pair of numbers
227
+ 0 ≤ s < t ≤ 1 we have that Mt ∩ M0 = Mt ∩ Ms = M0 \ ω0.
228
+ This means that the hypersurfaces Mt coincide on the subset M0 \ ω0, and as t ∈ [0, 1]
229
+ increases the domains ωt = Mt \ M0 ⊂ Mt are pairwise disjoint and move into the convex
230
+ direction. Each compact set of the form
231
+ (2.1)
232
+ Ct =
233
+
234
+ s∈[0,t]
235
+ ωs for t ∈ [0, 1]
236
+ is called a strictly convex cap with the base ω0. Note that bCt = ω0 ∪ ωt, Ct is strictly convex
237
+ along ωt, strictly concave along ω0, and it has corners along ω0 ∩ ωt. As t ∈ [0, 1] increases to
238
+ 1, the caps Ct monotonically increase to C1 and they share the same base ω0. Likewise, for any
239
+ 0 ≤ s < t ≤ 1 the set Cs,t = �
240
+ u∈[s,t] ωu is a strictly convex cap with the base ωs. The sets
241
+ (2.2)
242
+ Et = {z ∈ O : ρt(z) ≤ 0} for t ∈ [0, 1]
243
+ are strictly convex along bEt = {ρt = 0}, they form a continuously increasing family in t, and
244
+ Et = E0 ∪ Ct for every t ∈ [0, 1].
245
+
246
+ 6
247
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
248
+ Under these assumptions, we have the following result.
249
+ Proposition 2.1. Let D be a smoothly bounded, relatively compact, strongly pseudoconvex
250
+ domain in a Stein manifold X with dim X < n. Let the sets Et ⊂ O ⊂ Cn (t ∈ [0, 1]) be
251
+ given by (2.2), and let f0 : ¯D → O be a map of class A ( ¯D) such that f0(bD) ∩ E0 = ∅. Given
252
+ a compact set K ⊂ D such that f0(D \ K) ∩ E0 = ∅ and a number ǫ > 0, there is a map
253
+ f : ¯D → O of class A ( ¯D) satisfying the following conditions:
254
+ (i) f(bD) ∩ E1 = ∅,
255
+ (ii) f(D \ K) ∩ E0 = ∅, and
256
+ (iii) maxx∈K |f(x) − f0(x)| < ǫ.
257
+ Recall that a map f : ¯D → O is said to be of class A ( ¯D) if it is continuous on ¯D and
258
+ holomorphic on D. In our application of Proposition 2.1 in the proof of Theorem 1.3, the set O
259
+ will be a ball (or the entire Euclidean space) and the hypersurfaces Mt = {ρt = 0} = bEt will
260
+ be convex graphs over the coordinate hyperplane Cn−1 × R ⊂ Cn.
261
+ In the proof of Proposition 2.1 we shall need the following lemma.
262
+ Lemma 2.2. Assume that O is a convex open subset of Cn for n > 1, L is a compact subset of
263
+ O, and ρ : O → R is a C 1 smooth strictly convex function. Then there is a number δ > 0 with
264
+ the following property. If D is a smoothly bounded strongly pseudoconvex domain in a Stein
265
+ manifold X of dimension dim X = m < n, K is a compact subset of D, and f : ¯D → O is a
266
+ map of class A ( ¯D) such that
267
+ (2.3)
268
+ ρ(f(z)) > −δ for all z ∈ bD
269
+ and
270
+ ρ(f(z)) > 0 if z ∈ bD and f(z) /∈ L,
271
+ then given η > 0 there is a map g : ¯D → O of class A ( ¯D) satisfying the following conditions:
272
+ (i) ρ(g(z)) > 0 for z ∈ bD,
273
+ (ii) ρ(g(z)) > δ for those z ∈ bD for which g(z) ∈ L,
274
+ (iii) ρ(g(z)) > ρ(f(z)) − η for z ∈ D \ K, and
275
+ (iv) |f(z) − g(z)| < η for z ∈ K.
276
+ For m = 1, i.e., when D is a finite bordered Riemann surface, this is a simplified version of
277
+ [14, Lemmas 6.2 and 6.3], which is proved by using approximate solutions of a Riemann–Hilbert
278
+ boundary value problem. This method was employed in several earlier papers mentioned in [14].
279
+ When ρ is strictly convex, C 1 smoothness suffices since in the proof we may take a continuous
280
+ family of tangential linear discs to the sublevel set of ρ.
281
+ For m ≥ 2, Lemma 2.2 is a simplified and slightly modified version of [15, Lemma 5.3].
282
+ Besides the fact that we are considering single maps ¯D → O instead of sprays of maps, the only
283
+ difference is that the assumption in [15, Lemma 5.3] that the set {ρ = 0} is compact is replaced
284
+ by the assumption (2.3) saying that ρ(f(z)) for z ∈ bD may be negative only if f(z) lies in the
285
+ compact set L ⊂ O. This hypothesis ensures that the lifting for a relatively big amount (the role
286
+ of the constant δ) only needs to be made on a compact subset of O, while elsewhere it suffices to
287
+ pay attention not to decrease ρ ◦ f by more than a given amount and to approximate sufficiently
288
+ closely on K (the role of the constant η). The proof requires only a minor adaptation of [15,
289
+ proof of Lemma 5.3], using its local version [15, Lemma 5.2] in a finite induction with respect
290
+ to a covering of bD by small open sets on which there are good systems of local holomorphic
291
+ peak functions. In fact, Lemma 2.2 corresponds to a simplified version of [15, Sublemma 5.4],
292
+ which explains how to lift the image of bD with respect to ρ for a sufficiently large amount at
293
+ those points in bD which the map f sends to a certain coordinate chart Ui in the target manifold.
294
+
295
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
296
+ 7
297
+ In our situation, the role of Ui is played by an open relatively compact neighbourhood of the set
298
+ L ∩ {ρ = 0} in O, and there is no need to use the rest of the proof of [15, Lemma 5.3].
299
+ Proof of Proposition 2.1. For t ∈ [0, 1] let δt > 0 be a number for which the conclusion of
300
+ Lemma 2.2 holds for the function ρt and the compact set L = C1 (see (2.1)). The open sets
301
+ Ut = {z ∈ O : −δt < ρt(z) < δt} for t ∈ [0, 1]
302
+ form an open covering of C1, so there exists a finite subcovering {Utj} for 0 ≤ t1 < t2 < . . . <
303
+ tk ≤ 1. Applying Lemma 2.2 we inductively find maps f1, . . . , fk ∈ A ( ¯D) such that for every
304
+ j = 1, . . . , k we have that
305
+ (a) fj(bD) ∩ Etj = ∅ (where Et is given by (2.2)),
306
+ (b) fj(D \ K) ∩ E0 = ∅, and
307
+ (c) |fj − fj−1| < ǫ/k on K.
308
+ Note that conditions (a) and (b) hold for f0 and (c) is void. Assume inductively that for some
309
+ j ∈ {1, . . . , k} we have maps f0, . . . , fj−1 satisfying these conditions. Applying Lemma 2.2
310
+ with f = fj−1 and taking fj = g, condition (a) follows from part (i) in Lemma 2.2, (b) follows
311
+ from (ii) provided that the number η > 0 in Lemma 2.2 is chosen small enough, and (c) follows
312
+ from (iii) in Lemma 2.2 provided that η ≤ ǫ/k . This gives the map fj satisfying conditions
313
+ (a)–(c) and the induction may continue. The map f = fk then satisfies the proposition.
314
+
315
+ Remark 2.3. Proposition 2.1 also holds, with the same proof, if ρt (t ∈ [0, 1]) are strongly
316
+ plurisubharmonic functions of class C 2 satisfying dρt ̸= 0 on Mt = {ρt = 0}. Indeed, the
317
+ results from [15], which are used in the proof, pertain to this case. In the present paper we shall
318
+ only use the convex case under C 1 smoothness, which comes naturally in the construction.
319
+ 3. Closed convex sets with BCEH
320
+ In the context of convex analysis, closed unbounded convex sets that share several important
321
+ properties with compact convex sets were studied by Gale and Klee [26] in 1959.
322
+ They
323
+ introduced the class of continuous sets, and we show that this class coincides with the class
324
+ of sets having BCEH, introduced in Definition 1.2; see Proposition 3.3. We then develop further
325
+ properties of these sets which are relevant to the proof of our main theorems.
326
+ By a ray in Rn, we shall mean a closed affine halfline. Let E be a closed convex subset of
327
+ Rn. A boundary ray of E is a ray contained in the boundary of E. An asymptote of E is a ray
328
+ L ⊂ Rn \ E such that dist(L, E) = inf{|x − y| : x ∈ L, y ∈ E} = 0. The function
329
+ σ : {u ∈ Rn : |u| = 1} → R ∪ {+∞},
330
+ σ(u) = sup{x · u : x ∈ E}
331
+ is called the the support function of E. (Here, x · u denotes the Euclidean inner product.) A
332
+ closed convex set E is said to be continuous in the sense of Gale and Klee [26] if the support
333
+ function of E is continuous. Note that every compact convex set is continuous.
334
+ The following result is a part of [26, Theorem 1.3] due to Gale and Klee; we only list those
335
+ conditions that will be used. The last item (iv) uses also [26, Theorem 1.5].
336
+ Theorem 3.1. For a closed convex subset E in Rn the following conditions are equivalent:
337
+ (i) E is continuous.
338
+ (ii) E has no boundary ray nor asymptote.
339
+ (iii) For each point p ∈ Rn the convex hull Conv(E ∪ {p}) is closed.
340
+ (iv) For every compact convex set K ⊂ Rn the set Conv(E ∪ K) is closed.
341
+
342
+ 8
343
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
344
+ Condition (iii) implies that the closed convex hull Conv(E ∪ {p}) is the union of the line
345
+ segments connecting p to the points in E. It also shows that an unbounded continuous closed
346
+ convex subset E of Rn is not contained in any affine hyperplane.
347
+ Let us record the following observation which will be used in the sequel.
348
+ Lemma 3.2. Let E ⊂ Rn be a closed convex set, p ∈ Rn\E, and L ⊂ Rn be an affine subspace
349
+ containing p. Then, Conv(E ∪ {p}) ∩ L = Conv((E ∩ L) ∪ {p}).
350
+ Proof. Set E′ = E ∩ L. It is obvious that Conv(E′ ∪ {p}) ⊂ Conv(E ∪ {p}) ∩ L. Conversely,
351
+ since E is convex, every point q ∈ Conv(E ∪ {p}) belongs to a line segment from p to a point
352
+ q′ ∈ E. If in addition q ∈ L and q ̸= p then q′ ∈ E′, and hence q ∈ Conv(E′ ∪ {p}).
353
+
354
+ Proposition 3.3. A closed convex set E ⊂ Rn has BCEH if and only if it is continuous in the
355
+ sense of Gale and Klee [26].
356
+ Proof. Since all closed bounded convex sets have BCEH and are continuous, it suffices to
357
+ consider the case when the set E is unbounded.
358
+ If E is not continuous then by Theorem 3.1 it has a boundary ray or an asymptote. Denote it
359
+ by L, and let ℓ be the affine line containing L. Pick any affine 2-plane H ⊂ Rn containing ℓ.
360
+ There is a point p ∈ H \(ℓ∪E). By considering rays from p to points q ∈ E approaching L and
361
+ going to infinity (if L is a boundary ray, we can choose points q ∈ L), we see that the closure
362
+ of the set h(E, p) = Conv(E ∪ {p}) \ E contains the parallel translate L′ ⊂ H+ of L passing
363
+ through p, so h(E, p) is unbounded and hence E does not have BCEH.
364
+ Assume now that E is a continuous and let us prove that it has BCEH. We need to show that
365
+ for any closed ball B ⊂ Rn the set h(E, B) = Conv(E ∪ B) \ E is bounded. Assume to the
366
+ contrary that there is a sequence xm ∈ h(E, B) with |xm| → ∞ as m → ∞. Since the sets E
367
+ and B are convex, we have that
368
+ xm = tmbm + (1 − tm)em for tm ∈ [0, 1], bm ∈ B, em ∈ E, and m ∈ N.
369
+ Note that (1 − tm)|em| → ∞ as m → ∞. By compactness of the respective sets we may
370
+ assume, passing to a subsequence, that em ̸= 0 for all m and the sequences tm, bm, and
371
+ 1
372
+ |em|em
373
+ are convergent. Denote their respective limits by t, b, and f. We have that
374
+ xm = tmbm + (1 − tm)em = bm + (1 − tm)|em|
375
+ � em
376
+ |em| − bm
377
+ |em|
378
+
379
+ = bm + (1 − tm)|em|fm
380
+ where fm =
381
+ � em
382
+ |em|− bm
383
+ |em|
384
+
385
+ . Note that limm→∞ fm = f. Pick a number α ≥ 0 and set p = b+αf.
386
+ If m is large enough then (1−tm)|em| > α, so the point ym = bm+αfm lies on the line segment
387
+ connecting bm and xm. Since xm ∈ Conv(E ∪ {bm}), it follows that ym ∈ Conv(E ∪ {bm}).
388
+ Note that the sequence ym converges to p. Since E is continuous, Conv(E ∪ {b}) is closed by
389
+ Theorem 3.1, so p = limm→∞ ym ∈ Conv(E ∪ {b}). Since this holds for every α ≥ 0, the ray
390
+ L = {b + αf : α ∈ [0, ∞)} lies in Conv(E ∪ {b}). By Lemma 3.2 there is α0 ∈ [0, ∞) such
391
+ that the ray L′ = {b + αf : α ≥ α0} lies in E. Since E is continuous, L is not a boundary ray
392
+ of E by Theorem 3.1, thus L contains a point q = b+α1f ∈ E \bE for some α1 ≥ α0. Choose
393
+ a neighbourhood Uq ⊂ E of q. For any large enough m we then have pm := bm + α1fm ∈ Uq.
394
+ Let Lm = {bm + αfm : α ≥ 0}. Note that Lm ∩ Conv(E ∪ {bm}) = Conv((Lm ∩ E) ∪ {bm})
395
+ by Lemma 3.2. However, for m large enough the point xm ∈ Lm lies on the opposite side of pm
396
+ than bm, so xm belongs to Lm ∩ Conv(E ∪ {bm}) but not to Conv((Lm ∩ E) ∪ {bm}). This
397
+ contradiction proves that E has BCEH.
398
+
399
+
400
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
401
+ 9
402
+ Given a function φ : Rn−1 → R, the epigraph of φ is the set
403
+ (3.1)
404
+ E = Eφ = {(x, y) ∈ Rn−1 × R : y ≥ φ(x)}.
405
+ Note that a function is convex if and only if its epigraph is convex.
406
+ Proposition 3.4. If E ⊊ Rn is a closed unbounded convex set with BCEH then
407
+ (i) E does not contain any affine real line, and
408
+ (ii) for every affine line ℓ intersecting E in a ray and any hyperplane H transverse to ℓ, E is
409
+ the epigraph of a convex function on H. In particular, there are affine coordinates (x, y)
410
+ on Rn in which E is of the form (3.1) for a convex function φ : Rn−1 → R+ satisfying
411
+ (3.2)
412
+ lim inf
413
+ |x|→+∞
414
+ φ(x)
415
+ |x|
416
+ > 0.
417
+ The condition (3.2) says that φ grows at least linearly at infinity. We show in Example 3.10
418
+ that linear growth is possible.
419
+ Proof. (i) Assume that ℓ ⊂ E is an affine line and let us prove that E does not have BCEH.
420
+ Since E is a proper subset of Rn, there is a parallel translate ℓ′ of ℓ which is not contained in E,
421
+ and hence ℓ′ \E contains a ray L. Let p be the endpoint of L, and let p′ ∈ L be an arbitrary other
422
+ point. Since E ∩L = ∅, there is a ball B around p′ such that Conv(B ∪{p})∩E = ∅. Clearly,
423
+ there is a point q ∈ B such that the ray Lq with the endpoint p and containing q intersects the
424
+ line ℓ, so the line segment from p to q belongs to Conv(E ∪ {p}) \ E = h(E, p). By moving
425
+ p′ ∈ L to infinity we see that h(E, p) is unbounded, so E does not have BCEH.
426
+ (ii) Since E is unbounded, it contains a ray L. Denote by ℓ the affine line containing L. Let
427
+ ℓ′ be any parallel translate of ℓ. Since E contains no affine lines by part (i), there is a point
428
+ p ∈ ℓ′ \E. The closed convex hull of the union of L and p contains the parallel translate L′ ⊂ ℓ′
429
+ of L passing through p. Since E has BCEH, we conclude that L′ ⊂ Conv(E ∪ {p}) and L′ \ E
430
+ is bounded. Since E ∩ L′ is convex, L′ ∩ E is a closed ray with the endpoint on bE. This shows
431
+ that E is a union of closed rays contained in parallel translates of the line ℓ, so it is an epigraph
432
+ of a convex function defined on any hyperplane H ⊂ Rn transverse to ℓ. Choosing H such that
433
+ H ∩ E = ∅ there are affine coordinates (x, y) on Rn with H = {y = 0} and ℓ = {x = 0}. In
434
+ these coordinates, E is of the form (3.1) for a positive convex function φ.
435
+ Finally, if condition (3.2) fails then there is a sequence (xk, yk) ∈ E with |xk| → +∞ and
436
+ yk/|xk| → 0 as k → ∞. The union of the line segments Lk connecting p = (0, −1) ∈ Rn−1×R
437
+ to (xk, yk), intersected with the lower halfspace y ≤ 0, is then an unbounded subset of
438
+ h(E, p) = Conv(E ∪ {p}) \ E, contradicting the assumption that E has BCEH.
439
+
440
+ Remark 3.5. The growth condition (3.2) for an epigraph can always be achieved in suitable
441
+ linear coordinates (even without the BCEH property) if there is a supporting hyperplane H ⊂ Rn
442
+ for E such that the set E∩H is nonempty and compact. Indeed, we may then choose coordinates
443
+ (x, y) on Rn such that H = {y = 0}, E ⊂ {y ≥ 0}, and 0 ∈ E. If the condition (3.2) fails,
444
+ there is a sequence (xk, yk) ∈ E with |xk| → +∞ and yk/|xk| → 0 as k → ∞. After passing
445
+ to a subsequence, a ray in E ∩ H lies in the closure of the union of the line segments Lk ⊂ E
446
+ connecting the origin to (xk, yk), contradicting the assumption that the latter set is compact.
447
+ Corollary 3.6. If E is a closed convex set in Cn (n > 1) having BCEH then Cn \ E is Oka.
448
+ Proof. By Proposition 3.4 the set E does not contain any affine real line, and hence Cn \ E is
449
+ Oka by [25, Theorem 1.8].
450
+
451
+
452
+ 10
453
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
454
+ The following lemma shows that the BCEH condition is stable under uniform approximation.
455
+ Lemma 3.7. Assume that φ : Rn−1 → R is a convex function whose epigraph Eφ (3.1) has
456
+ BCEH. Then for any ǫ > 0 and convex function ψ : Rn−1 → R satisfying |φ − ψ| < ǫ the
457
+ epigraph Eψ also has BCEH.
458
+ Proof. If Eψ fails to have BCEH then by Theorem 3.1 and Proposition 3.3 it has a boundary
459
+ ray or an asymptote, L. Since dist(L, Eψ) = 0 and Eψ is convex, dist(x, Eψ) converges
460
+ to zero as x ∈ L goes to infinity.
461
+ Thus, by making L shorter if necessary, we have that
462
+ L ⊂ Eφ−2ǫ \ Eφ+2ǫ. Hence, L lies out of Eφ+2ǫ but the vertical translation of L for 4ǫ pushes it
463
+ in Eφ+2ǫ. Since Eφ+2ǫ, being a translate of Eφ, has BCEH, this contradicts Proposition 3.4 (ii).
464
+ The contradiction shows that Eψ has BCEH as claimed.
465
+
466
+ We now give a differential characterization of the BCEH property of an epigraph (3.1).
467
+ Proposition 3.8. If φ : Rn−1 → R is a convex function of class C 1 satisfying condition (3.2),
468
+ then the epigraph E = {(x, y) ∈ Rn : y ≥ φ(x)} has BCEH if and only if
469
+ (3.3)
470
+ lim
471
+ |x|→∞ |x|
472
+
473
+ 1 −
474
+ φ(x)
475
+ x · ∇φ(x)
476
+
477
+ = +∞.
478
+ Proof. We first consider the case n = 2. Then, x is a single variable and (3.3) is equivalent to
479
+ (3.4)
480
+ lim
481
+ x→+∞
482
+
483
+ x − φ(x)
484
+ φ′(x)
485
+
486
+ = +∞
487
+ and
488
+ lim
489
+ x→−∞
490
+
491
+ x − φ(x)
492
+ φ′(x)
493
+
494
+ = −∞.
495
+ For every x ∈ R such that φ′(x) ̸= 0 the number
496
+ (3.5)
497
+ ξ(x) = x − φ(x)
498
+ φ′(x)
499
+ is the first coordinate of the intersection of the tangent line to the graph of φ at the point (x, φ(x))
500
+ with the first coordinate axis y = 0. By (3.2) and convexity of φ we have that |φ′(x)| is bounded
501
+ away from zero for all sufficiently big |x|. This shows that conditions (3.4) are invariant under
502
+ translations, so we may assume that φ ≥ 0 and φ(0) = 0. It is easily seen that the function ξ is
503
+ increasing. If φ is of class C 2, we have that ξ′(x) = φ(x)φ′′(x)/φ′(x)2 ≥ 0.
504
+ Assume now that conditions (3.4) hold.
505
+ Pick a pair of sequences aj < bj in R with
506
+ limj→∞ aj = −∞ and limj→∞ bj = +∞. The intervals Ij = [ξ(aj), ξ(bj)] then increase
507
+ to R as j → ∞. We identify Ij with Ij × {0} ⊂ R2. Since φ is convex, its epigraph lies above
508
+ the tangent line at any point. It follows that the set h(E, Ij) (see (1.1)) is the bounded region in
509
+ R×R+ whose boundary consists of Ij, the two line segments Lj and L′
510
+ j connecting the endpoints
511
+ (ξ(aj), 0) and (ξ(bj), 0) of Ij to the respective points Aj = (aj, φ(aj)) and Bj = (bj, φ(bj))
512
+ on bE, and the graph of φ over [aj, bj]. The supporting lines of Lj and L′
513
+ j intersect at a point
514
+ Cj in the lower halfspace y < 0, and we obtain a closed triangle ∆j with the endpoints Aj, Bj,
515
+ and Cj. Note that ∆j ∩ (R × {0}) = Ij. Since φ grows at least linearly (see (3.2)), the triangles
516
+ ∆j ⊂ R2 exhaust R2 as j → ∞, and the set h(E, ∆j) (1.1) is bounded for every j. Hence,
517
+ E has BCEH. This argument furthermore shows that for any point p = (0, −c) /∈ E there is
518
+ a unique pair of tangent lines to bE passing through p such that, denoting by q1, q2 ∈ bE the
519
+ respective points where these lines intersect bE, the convex hull Conv(E ∪ {p}) is the union of
520
+ E and the triangle with vertices p, q1, q2.
521
+ Conversely, if (3.3) fails then it is easily seen that E has a boundary ray or an asymptote, so
522
+ it does not have BCEH. We leave the details to the reader.
523
+
524
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
525
+ 11
526
+ The case with n ≥ 3 now follows easily. Pick a unit vector v ∈ Rn−1, |v| = 1, and let Lv
527
+ denote the 2-plane in Rn passing through the origin and spanned by v and en = (0, . . . , 0, 1).
528
+ Then, Ev := E ∩ Lv = {(t, y) ∈ R2 : y ≥ φ(tv)} and the first condition in (3.4) reads
529
+ (3.6)
530
+ lim
531
+ t→+∞
532
+
533
+ t −
534
+ φ(tv)
535
+ �n−1
536
+ j=1 vj
537
+ ∂φ
538
+ ∂xj (tv)
539
+
540
+ = +∞.
541
+ Writing x = tv with t ≥ 0 and v = x/|x|, this is clearly equivalent to (3.3). As before, let
542
+ p = (0, . . . , 0, −c) /∈ E. If (3.3) holds then Conv(Ev ∪ {p}) ⊂ Lv is obtained by adding to
543
+ Ev the triangle in Lv obtained by the two tangent lines to bEv passing through p as described in
544
+ the case n = 2. The sizes of these triangles are uniformly bounded with respect to the direction
545
+ vector |v| = 1, and condition (3.2) implies that these triangles increase to Lv as c → +∞,
546
+ uniformly with respect to v. Since �
547
+ |v|=1 Lv = Rn, Lemma 3.2 shows that
548
+ Conv(E ∪ {p}) =
549
+
550
+ |v|=1
551
+ Conv(Ev ∪ {p}),
552
+ and hence E has BCEH. The converse is seen as in the special case n = 2.
553
+
554
+ Corollary 3.9. If φ : Rn−1 → R+ is a convex function of class C 1 such that
555
+ lim
556
+ |x|→+∞
557
+ x · ∇φ(x)
558
+ |x|
559
+ = +∞,
560
+ then the epigraph E = {(x, y) ∈ Rn : y ≥ φ(x)} has BCEH.
561
+ Proof. By restricting to planes as in the above proof, it suffices to consider the case n = 2. We
562
+ may assume that φ ≥ 0 and φ(0) = 0. Since φ is convex, g(x) = φ′(x) is an increasing function
563
+ and the above condition reads limx→±∞ g(x) = ±∞. For any x0 > 0 and x ≥ x0 we have that
564
+ ξ(x) := x −
565
+ 1
566
+ g(x)
567
+ � x
568
+ 0
569
+ g(t)dt =
570
+ � x
571
+ 0
572
+
573
+ 1 − g(t)
574
+ g(x)
575
+
576
+ dt ≥
577
+ � x0
578
+ 0
579
+
580
+ 1 − g(t)
581
+ g(x)
582
+
583
+ dt.
584
+ Letting x → +∞ we have that g(t)
585
+ g(x) → 0 uniformly on t ∈ [0, x0], and hence the last integral
586
+ converges to x0. Letting x0 → ∞ we see that limx→+∞ ξ(x) = +∞. The analogous argument
587
+ applies when x → −∞. Hence, conditions (3.3) hold and therefore E has BCEH.
588
+
589
+ Example 3.10. There exist convex epigraphs (3.1) having BCEH where the function φ grows
590
+ linearly, although it cannot be too close to linear near infinity in the absence of boundary rays
591
+ and asymptotes. We give such an example in R2. Let g : R → (−1, 1) be an odd, continuous,
592
+ increasing function with limx→+∞ g(x) = 1 and
593
+ � ∞
594
+ 0 (1−g(x))dx = +∞. (An explicit example
595
+ is g(x) = 2
596
+ πArctan x.) Its integral φ(x) =
597
+ � x
598
+ 0 g(t)dt for x ∈ R then clearly satisfies φ(x) ≥ 0,
599
+ φ′(x) = g(x) ∈ (−1, +1) (hence φ grows linearly), and φ is convex. We now show that (3.3)
600
+ holds. Let x > 0 be large enough so that g(x) > 0. We have that
601
+ ξ(x) = x −
602
+ 1
603
+ g(x)
604
+ � x
605
+ 0
606
+ g(t)dt =
607
+ � x
608
+ 0
609
+
610
+ 1 − g(t)
611
+ g(x)
612
+
613
+ dt.
614
+ Fix x0 > 0 and let x ≥ x0. Then, ξ(x) ≥
615
+ � x0
616
+ 0 (1 − g(t)/g(x))dt. Since limx→+∞ g(x) = 1
617
+ and ξ is increasing for large enough |x|, it follows that limx→+∞ ξ(x) ≥
618
+ � x0
619
+ 0 (1 − g(t))dt.
620
+ Sending x0 → +∞ gives limx→+∞ ξ(x) ≥
621
+ � ∞
622
+ 0 (1 − g(t))dt = +∞. Similarly we see that
623
+ limx→−∞ ξ(x) = −∞. Thus, (3.3) holds, and hence the epigraph of φ has BCEH.
624
+ By using the idea in the above example we now prove the following approximation result,
625
+ which extends Theorem 1.3 to a much bigger class of convex epigraphs (see Corollary 1.4).
626
+
627
+ 12
628
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
629
+ Proposition 3.11. Assume that φ : Rn−1 → R+ is a convex function such that the set {φ = 0}
630
+ is nonempty and compact. Given numbers ǫ > 0 (small) and R > 0 (big) there is a smooth
631
+ convex function ψ : Rn−1 → R such that ψ < φ on Rn−1, φ(x) − ψ(x) < ǫ for all |x| ≤ R,
632
+ and the epigraph Eψ = {y ≥ ψ} has BCEH.
633
+ Proof. By Remark 3.5 the function φ grows at least linearly near infinity (see (3.2)). Set
634
+ (3.7)
635
+ A = lim inf
636
+ |x|→∞
637
+ φ(x)
638
+ |x| > 0.
639
+ Since the set φ = 0 does not contain any affine line, Azagra’s result [6, Theorem 1 and
640
+ Proposition 1] implies that for every ǫ > 0 there is a smooth strictly convex function ψ on
641
+ Rn−1 satisfying φ − ǫ < ψ < φ. Replacing φ by ψ − minx ψ(x) ≥ 0 we may therefore assume
642
+ that φ is smooth. By increasing the number R > 0 if necessary, we may assume that
643
+ (3.8)
644
+ φ(x)
645
+ |x|
646
+ ≥ A
647
+ 2
648
+ for all |x| ≥ R.
649
+ Pick a number r ∈ (0, 1) close to 1 such that
650
+ (3.9)
651
+ (1 − r) sup
652
+ |x|≤R
653
+ φ(x) < ǫ.
654
+ Choose a smooth increasing function h : R → R+ such that
655
+ h(t) = 0 for t ≤ R,
656
+ lim
657
+ t→+∞ h(t) = 1,
658
+ and
659
+ � ∞
660
+ 0
661
+ (1 − h(t))dt = +∞.
662
+ (We can take a smoothing of the Arctan function used in Example 3.10.) Set
663
+ H(x) =
664
+ � |x|
665
+ 0
666
+ h(s)ds
667
+ for x ∈ Rn−1.
668
+ Clearly, H ≥ 0 is a radially symmetric smooth convex function that vanishes on |x| ≤ R and
669
+ satisfies H(x) ≤ |x| for all x ∈ Rn−1. With A and r as in (3.7) and (3.9) we set
670
+ δ = A(1 − r)
671
+ 2
672
+ .
673
+ We claim that the function
674
+ ψ(x) = rφ(x) + δH(x)
675
+ for x ∈ Rn−1
676
+ satisfies the conditions in the theorem. Clearly, ψ ≥ rφ is a smooth convex function. For
677
+ |x| ≤ R we have H(x) = 0, so ψ(x) = rφ(x) ≤ φ(x) and φ(x) − ψ(x) = (1 − r)φ(x) < ǫ by
678
+ (3.9). If |x| > R then φ(x)/|x| ≥ A/2 by (3.8) and H(x) < |x|, which implies
679
+ ψ(x)
680
+ |x|
681
+ ≤ rφ(x)
682
+ |x| + δ ≤ φ(x)
683
+ |x| .
684
+ Indeed, we have that φ(x)
685
+ |x| − r φ(x)
686
+ |x| = (1 − r)φ(x)
687
+ |x| ≥ A(1−r)
688
+ 2
689
+ = δ. Hence, ψ ≤ φ on Rn−1.
690
+ It remains to show that the epigraph Eψ satisfies BCEH. We shall verify (3.3), which is
691
+ equivalent to (3.6) with uniform convergence with respect to the vector v = x/|x|. Write
692
+ gv(t) = r∂φ(tv)
693
+ ∂t
694
+ ,
695
+ k(t) = δh(t),
696
+ ˜gv(t) = ∂ψ(tv)
697
+ ∂t
698
+ = gv(t) + k(t).
699
+
700
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
701
+ 13
702
+ The quantity in (3.6) associated to the function ψ is given by
703
+ ξv(t)
704
+ =
705
+ t − ψ(tv)
706
+ ˜gv(t) =
707
+ � t
708
+ 0
709
+
710
+ 1 − gv(s) + k(s)
711
+ gv(t) + k(t)
712
+
713
+ ds
714
+ =
715
+ � t
716
+ 0
717
+ gv(t) − gv(s)
718
+ gv(t) + k(t) ds +
719
+ � t
720
+ 0
721
+ k(t) − k(s)
722
+ gv(t) + k(t)ds
723
+
724
+ � t
725
+ 0
726
+ gv(t) − gv(s)
727
+ gv(t) + δ
728
+ ds +
729
+ � t
730
+ 0
731
+ k(t) − k(s)
732
+ gv(t) + δ ds,
733
+ where the last inequality holds since the functions gv and k are nonnegative and increasing and
734
+ k < δ. Pick c > 0. We will show that for large enough t > 0 and any unit vector v ∈ Rn−1 the
735
+ above expression is bigger than or equal to c. Choose positive numbers t0, a, t1 as follows:
736
+ t0 = 3c,
737
+ a = max{3 max
738
+ |v|=1 gv(t0), 3δ},
739
+ � t1
740
+ 0
741
+ (k(t1) − k(s))ds > ac.
742
+ Such t1 exists since limt→+∞
743
+ � t
744
+ 0(k(t) − k(s))ds = δ
745
+ � ∞
746
+ 0 (1 − h(s))ds = +∞. Since the
747
+ integrands in the bound for ξv(t) are nonnegative, we have for t ≥ max{t0, t1} and |v| = 1 that
748
+ (3.10)
749
+ ξv(t) ≥
750
+ � t0
751
+ 0
752
+ gv(t) − gv(s)
753
+ gv(t) + δ
754
+ ds +
755
+ � t1
756
+ 0
757
+ k(t) − k(s)
758
+ gv(t) + δ ds.
759
+ Assume that for some such (t, v) we have that gv(t) + δ ≥ a. Since a ≥ 3δ, it follows that
760
+ gv(t) ≥ 2δ and hence
761
+ gv(t)
762
+ gv(t) + δ ≥ 2
763
+ 3.
764
+ Furthermore, from a ≥ 3 max|v|=1 gv(t0) we get for 0 ≤ s ≤ t0 that
765
+ gv(s)
766
+ gv(t) + δ ≤ gv(t0)
767
+ a
768
+ ≤ 1
769
+ 3.
770
+ These two inequalities imply that the first integral in (3.10) is bounded below by t0/3 ≥ c. If
771
+ on the other hand gv(t) + δ < a then the denominator of the second integral in (3.10) is at most
772
+ a, so the integral is ≥ c by the choice of t1. This shows that ξv(t) ≥ c for all |v| = 1 and
773
+ t ≥ max{t0, t1}. Since c was arbitrary, condition (3.3) holds and hence Eψ has BCEH.
774
+
775
+ The following observation will be used in the proof of Theorem 1.3.
776
+ Proposition 3.12. Denote by B the open unit ball in Rn. Let Eφ ⊂ Rn be a closed convex
777
+ set of the form (3.1) with C 1 boundary having BCEH, where the function φ : Rn−1 → R is
778
+ bounded from below and strictly convex near infinity. Then there is an r0 > 0 such that for every
779
+ r ≥ r0 the convex hull Conv(Eφ ∪ rB) = {y ≥ ψ(x)} is a closed convex set with BCEH, and
780
+ ψ : Rn−1 → R is a convex function of class C 1 such that ψ ≤ φ and these functions agree near
781
+ infinity. Furthermore, if r ≥ r0 is large enough then the function φt : Rn−1 → R defined by
782
+ (3.11)
783
+ φt(x) = (1 − t)φ(x) + tψ(x),
784
+ x ∈ Rn−1
785
+ is strictly convex for every t ∈ (0, 1), and for any 0 < t0 < t1 < 1 the closure of the set
786
+ {(x, y) ∈ Rn : φt1(x) < y < φt0(x)}
787
+ is a strictly convex cap with the base in the strictly convex hypersurface {y = φt0(x)}.
788
+
789
+ 14
790
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
791
+ Proof. Consider the function on Rn−1 given by
792
+ ˜φr(x) =
793
+
794
+ min{φ(x), −
795
+
796
+ r2 − |x|2},
797
+ |x| < r,
798
+ φ(x),
799
+ |x| ≥ r.
800
+ (Note that ˜φr may be discontinuous at the points of the sphere |x| = r.) The convex hull of its
801
+ epigraph E˜φr equals Conv(E∪rB), which is closed by Theorem 3.1 (iv), and the set h(E, rB) =
802
+ Conv(E ∪ rB) \ E is bounded since E has BCEH. By smoothing ˜φr we get a function ˜ψr of
803
+ class C 1 which agrees with φ near infinity such that Conv(E ˜ψr) = Conv(E ∪ rB). By [28,
804
+ Theorem 3.2] we conclude that Conv(E ∪ rB) has C 1 boundary, so it is the epigraph Eψr of a
805
+ convex function ψr : Rn−1 → R of class C 1 which agrees with φ near infinity.
806
+ Since φ grows at least linearly, there is a function τ(r) defined for r ∈ R+ large enough such
807
+ that ψr(x) = −
808
+
809
+ r2 − |x|2 for |x| ≤ τ(r) and τ(r) → +∞ as r → +∞. By choosing r large
810
+ enough, the compact set of points where the function φ fails to be strictly convex is contained
811
+ in the ball |x| < τ(r). Since on this ball we have that ψr(x) = −
812
+
813
+ r2 − |x|2 which is strictly
814
+ convex, the convex combinations φt in (3.11) of φ and ψ = ψr are strictly convex on Rn−1 for
815
+ all 0 < t < 1. For such r, the last statement in the proposition is evident. (Note that the strictly
816
+ convex functions ρt(x, y) = exp(ψt(x) − y) − 1 for t ∈ (0, 1) correspond to those used in
817
+ Section 2.)
818
+
819
+ 4. Proof of Theorem 1.3
820
+ For the definition and the main theorem on Oka manifolds, see [20, Definition 5.4.1 and
821
+ Theorem 5.4.4]. We shall use the following version of the Oka principle; see [22, Theorem 1.3].
822
+ Theorem 4.1. Assume that X is a Stein manifold, K is a compact O(X)-convex set in X, X′
823
+ is a closed complex subvariety of X, Ω is an Oka domain in a complex manifold Y , f : X → Y
824
+ is a continuous map which is holomorphic on a neighbourhood of K, f|X′ : X′ → Y is
825
+ holomorphic, and f(X \ ˚
826
+ K) ⊂ Ω. Then there is a homotopy {ft}t∈[0,1] of continuous maps
827
+ ft : X → Y connecting f = f0 to a holomorphic map f1 : X → Y such that for every t ∈ [0, 1]
828
+ the map ft is holomorphic on a neighbourhood of K, it agrees with f on X′, it approximates f
829
+ uniformly on K and uniformly in t ∈ [0, 1] as closely as desired, and ft(X \ ˚
830
+ K) ⊂ Ω.
831
+ Proof of Theorem 1.3. By Proposition 3.4 there are complex coordinates z = (z′, zn) on Cn
832
+ such that the given set E is an epigraph of the form (1.2). We shall write z = (x, y) where
833
+ x = (z′, ℜzn) ∈ Cn−1 × R ∼= R2n−1 and y = ℑzn ∈ R, so E = Eφ = {y ≥ φ(x)} where
834
+ φ ≥ 0 is a convex function as in Proposition 3.4. Let the set K ⊂ X and the map f0 : K → Cn
835
+ be as in the theorem; in particular, f0(bK) ⊂ Cn \ E. Thus, there are an open neighbourhood
836
+ U ⊂ X of K and ǫ > 0 such that f0 is holomorphic in U and f0(U \ ˚
837
+ K) ⊂ Cn \ Eφ−ǫ. By
838
+ Azagra [6, Theorem 1.8] there is a a real analytic strictly convex function φ0 : R2n−1 → R such
839
+ that φ − ǫ < φ0 < φ. Its epigraph E0 = {(x, y) ∈ Cn : y ≥ φ0(x)} is a closed strictly convex
840
+ set with real analytic boundary which has BCEH by Lemma 3.7, and f0(U \ ˚
841
+ K) ⊂ Cn \ E0.
842
+ Let B denote the open unit ball in Cn centred at 0. Recall the notation h(E, K) in (1.1). Pick
843
+ a number r0 > 0. We can find an increasing sequence rk > 0 diverging to infinity such that
844
+ (4.1)
845
+ h(E0, rkB) ⊂ rk+1B
846
+ for k = 0, 1, 2, . . . .
847
+
848
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
849
+ 15
850
+ Indeed, since E0 has BCEH, the set h(E0, rkB) is bounded for each k, and hence (4.1) holds if
851
+ the number rk+1 is chosen large enough. Set
852
+ Ek+1 = Conv(E0 ∪ rkB) = E0 ∪ h(E0, rkB)
853
+ for k = 0, 1, 2, . . ..
854
+ We clearly have that E0 ⊂ E1 ⊂ · · · ⊂ �∞
855
+ k=0 Ek = Cn. Furthermore, (4.1) shows that for
856
+ j = 0, 1, . . . , k + 1 we have that E0 ⊂ Ej ⊂ E0 ∪ rk+1B and hence
857
+ (4.2)
858
+ Ek+2 = Conv(Ej ∪ rk+1B) for j = 0, 1, . . . , k + 1.
859
+ Proposition 3.12 shows that for each k = 1, 2, . . . we have Ek = {y ≥ φk(x)} where φk a
860
+ convex function of class C 1 which agrees with φ0 near infinity, and Ek has BCEH. Hence,
861
+ Ωk = Cn \ Ek = {(x, y) ∈ Cn : y < φk(x)}
862
+ is an Oka domain for every k = 0, 1, . . . by Corollary 3.6. In view of Ek+2 = Conv(Ek∪rk+1B)
863
+ (see (4.2)), Proposition 3.12 also shows that if rk+1 is chosen large enough then the function
864
+ (4.3)
865
+ ψt = (1 − t)φk + tφk+2 : Cn−1 × R → R
866
+ is strictly convex for every t ∈ (0, 1), and for each 0 < t0 < t1 < 1 the closure of the set
867
+ (4.4)
868
+ C = {(x, y) : ψt1 < y < ψt0}
869
+ is a strictly convex cap as described in Section 2. (Note that the strictly convex functions
870
+ ρt(x, y) = exp(ψt(x) − y) − 1 for t ∈ (0, 1) correspond to those used in Section 2.)
871
+ Choose an exhaustion D0 ⊂ D1 ⊂ · · · ⊂ �∞
872
+ k=0 Dk = X by smoothly bounded, relatively
873
+ compact, strongly pseudoconvex domains with O(X)-convex closures such that K ⊂ D0 ⊂
874
+ ¯D0 ⊂ U. For consistency of notation we set D−1 = K. We now construct a sequence of
875
+ holomorphic maps fk : ¯Dk → Cn satisfying the following conditions for k = 0, 1, 2, . . .:
876
+ (a) fk(Dk \ Dk−1) ⊂ Ωk = Cn \ Ek,
877
+ (b) fk+1(Dk \ Dk−1) ⊂ Ωk, and
878
+ (c) fk+1 approximates fk uniformly on ¯Dk−1 as closely as desired.
879
+ For k = 0 the initial map f0 in Theorem 1.3 satisfies condition (a) while conditions (b) and (c)
880
+ are void. Assuming inductively that we found maps f0, . . . , fk satisfying these conditions, the
881
+ construction of the next map fk+1 is made in two steps as follows.
882
+ By compactness of the set fk(bDk) ⊂ Ωk = {y < φk(x)} we can choose t0 ∈ (0, 1) small
883
+ enough such that f(bDk) ⊂ {y < ψt0(x)}, where the function ψt (t ∈ [0, 1]) is given by (4.3).
884
+ By (4.1) we can also choose t1 ∈ (t0, 1) sufficiently close to 1 such that
885
+ Ek+1 ⊂ {(x, y) : y ≥ ψt1(x)}.
886
+ Proposition 2.1 applied to the map fk : ¯Dk → Cn, the set Ek, and the strictly convex cap
887
+ C (4.4) (which corresponds to C1 in Proposition 2.1) gives holomorphic map gk : ¯Dk → Cn
888
+ approximating fk on Dk−1 and satisfying
889
+ (4.5) gk(bDk) ⊂ {(x, y) : y < ψt1(x)} ⊂ Cn \ Ek+1 = Ωk+1 and gk(Dk \ Dk−1) ⊂ Ωk.
890
+ In the second step, we use that Ωk+1 is an Oka domain. Since Ωk+1 is contractible and
891
+ gk(bDk) ⊂ Ωk+1 by (4.5), gk extends from ¯Dk to a continuous map X → Cn sending
892
+ X \ Dk to Ωk+1. Theorem 4.1 applied to gk gives a holomorphic map fk+1 : ¯Dk+1 → Cn
893
+ approximating gk on ¯Dk and satisfying fk+1(Dk+1 \ Dk) ⊂ Ωk+1 (which is condition (a) for
894
+ k + 1) and fk+1(Dk \ Dk−1) ⊂ Ωk (condition (b)). Since fk+1 approximates gk on ¯Dk and gk
895
+ approximates fk on ¯Dk−1, fk+1 also satisfies condition (c). This completes the induction step.
896
+
897
+ 16
898
+ B. Drinovec Drnovˇsek and F. Forstneriˇc
899
+ If the approximations are close enough then the sequence fk converges uniformly on
900
+ compacts in X to a holomorphic f : X → Cn. Conditions (a)–(c) and the fact that the sets
901
+ Ek exhaust Cn imply that f is a proper holomorphic map satisfying f(X \ ˚
902
+ K) ⊂ Ω0 = Cn \E0.
903
+ To construct proper holomorphic immersions and embeddings in suitable dimensions given in
904
+ the theorem, we use the general position argument at every step to ensure that every map fk in the
905
+ sequence is an immersion or an embedding. (See e.g. [20, Corollary 8.9.3].) If the convergence
906
+ is fast enough then the same holds for the limit map f by a standard argument.
907
+
908
+ Proof of Corollary 1.4. Given a holomorphic map f0 : K → Cn with f0(bK) ⊂ Cn \ Eφ as
909
+ in Theorem 1.3, Proposition 3.11 furnishes a closed convex set Eψ ⊃ Eφ with BCEH such that
910
+ f0(bK) ⊂ Cn \ Eψ. Applying Theorem 1.3 with Eψ gives the desired conclusion.
911
+
912
+ We have the following analogue of Theorem 1.3 with interpolation on a closed complex
913
+ subvariety of X. Unlike in the above corollary, approximation of E from the outside by convex
914
+ sets enjoying BCEH cannot be used since the subvariety f(X′) may have zero distance to bE.
915
+ This results extends the case of [24, Theorem 15] when E is a compact convex set.
916
+ Theorem 4.2. Let E be a closed convex set in Cn (n > 1) with C 1 boundary which is strictly
917
+ convex near infinity and has bounded convex exhaustion hulls. Let X be a Stein manifold,
918
+ K ⊂ X be a compact O(X)-convex set, U ⊂ X be an open set containing K, X′ be a
919
+ closed complex subvariety of X, and f0 : U ∪ X′ → Cn be a holomorphic map such that
920
+ f0|X′ : X′ → Cn is proper holomorphic and f0(bK ∪ (X′ \ K)) ∩ E = ∅. Given ǫ > 0 there
921
+ exists a proper holomorphic map f : X → Cn satisfying the following conditions:
922
+ (a) f(X \ ˚
923
+ K) ⊂ Cn \ E,
924
+ (b) ∥f − f0∥K < ǫ,
925
+ (c) f|X′ = f0|X′.
926
+ If 2 dim X ≤ n then f can be chosen an immersion (and an embedding if 2 dim X + 1 ≤ n)
927
+ provided that f0|X′ is one.
928
+ Proof. This is proved by a small modification of the proof of Theorem 1.3, similar to the one
929
+ in [24, proof of Theorem 15]. The initial step in the proof, approximating E from the outside
930
+ by a strictly convex set, is unnecessary since bE is strictly convex near infinity. The main (and
931
+ essentially the only) change comes in the choice of the exhaustion Dk of the Stein manifold
932
+ X. In the inductive step when constructing the map fk+1, we must assume in addition that
933
+ fk(bDk ∩ X′) ⊂ Ωk+1 = Cn \Ek+1. Then, we push the image of bDk out of Ek+1 by the same
934
+ method as before, using Proposition 2.1 but ensuring that the modifications are kept fixed on X′
935
+ and small near bDk ∩ X′. This is possible since the method from [15] is applied locally near
936
+ bDk (away from bDk ∩ X′), and these local modifications are glued together by preserving the
937
+ value of the map on X′. We refer to [24, proof of Theorem 15] for a more precise description.
938
+ This gives the next holomorphic map fk+1 : X → Cn satisfying fk+1(X \ Dk) ⊂ Ωk+1,
939
+ fk+1|X′ = fk|X′, and conditions (b) and (c) in the proof of Theorem 1.3. We then choose the
940
+ next domain Dk+1 ⊂ X big enough such that fk+1(bDk+1 ∩X′) ⊂ Ωk+2 = Cn \Ek+2. This is
941
+ possible since the map fk+1|X′ = f0|X′ : X′ → Cn is proper, f0(X′ \ ˚
942
+ K) ⊂ Ω = Cn \ E, and
943
+ the domain Ωk+2 agrees with Ω near infinity by the construction. Clearly the induction step is
944
+ now complete. Assuming that the approximations are close enough, the sequence fk converges
945
+ to a limit holomorphic map f : X → Cn satisfying the stated conditions.
946
+
947
+ Acknowledgements. The first named author is supported by grants P1-0291, J1-3005, and N1-
948
+ 0137 from ARRS, Republic of Slovenia. The second named author is supported by the European
949
+ Union (ERC Advanced grant HPDR, 101053085) and grants P1-0291, J1-3005, and N1-0237
950
+
951
+ Proper holomorphic maps in Euclidean spaces avoiding unbounded convex sets
952
+ 17
953
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954
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+ Barbara Drinovec Drnovˇsek
1040
+ Faculty of Mathematics and Physics, University of Ljubljana, Jadranska 19, SI–1000 Ljubljana,
1041
+ Slovenia
1042
+ Institute of Mathematics, Physics and Mechanics, Jadranska 19, SI–1000 Ljubljana, Slovenia.
1043
+ e-mail: [email protected]
1044
+ Franc Forstneriˇc
1045
+ Faculty of Mathematics and Physics, University of Ljubljana, Jadranska 19, SI–1000 Ljubljana,
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+ Slovenia
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+ Institute of Mathematics, Physics and Mechanics, Jadranska 19, SI–1000 Ljubljana, Slovenia
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+ e-mail: [email protected]
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+
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