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--- |
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--- |
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license: mit |
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base_model: fblgit/UNA-TheBeagle-7b-v1 |
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model_name: cosmosage |
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model_type: mistral |
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prompt_template: '{optional system message} |
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User: {prompt} |
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Assistant:' |
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language: |
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- en |
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pipeline_tag: question-answering |
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--- |
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# cosmosage |
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Cosmosage is a natural-language cosmology assistant that can answer questions about cosmology. |
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cosmosage_v1 is a fine tune of fblgit/UNA-TheBeagle-7b-v1 on various cosmology-related datasets including |
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open-access textbooks and scientific publications. It is primarily intended for Q&A mode, where the model |
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gives a single answer in response to a single question, though it performs decently as a chatbot, as well. |
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See https://github.com/tijmen/cosmosage for more details. |
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## Usage |
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One convenient way of using this model is with `text-generation-webui` |
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https://github.com/oobabooga/text-generation-webui |
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- Under the Model tab, download custom model, entering "Tijmen2/cosmosage_v1_gptq" |
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- When the download is complete, click the refresh icon next to Model. |
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- Select AutoGPTQ as your model loader. |
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- In the Model dropdown, choose `cosmosage_v0.4` and load it. |
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- Head over to the Notebook tab and ask away! |
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## Prompt Style |
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The model was trained with data formatted like |
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``` |
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{system, optional} |
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USER: {question} |
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ASSISTANT: {answer} |
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``` |
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Feel free to experiment with different prompts and sampling parameters. No system prompt, i.e. |
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``` |
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USER: <<<your question here>>> |
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ASSISTANT: |
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``` |
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works well, but usually leads to very short answers to questions. If you want longer responses, you should |
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ask for them in the system prompt. |
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The following is an example prompt that that leverages the model's instruction-following capabilities as |
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well as two-shot prompting. I've been using it with temperature=0.4, min_p=0.1. |
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``` |
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You are an expert cosmology assistant, able to answer questions on the cosmic microwave background, |
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galaxy formation, large scale structure, theoretical cosmology, inflation, big bang nucleosynthesis, cosmology |
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instrumentation, and other related topics. Please assume the user is fluent in scientific terminology. Elaborate |
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where possible to give a complete answer. If you do not know, say you do not know. You will get two examples, |
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then be expected to answer one question to the best of your ability. |
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## EXAMPLE 1 |
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USER: What is the ISW effect? |
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ASSISTANT: The Integrated Sachs-Wolfe effect describes the fact that cosmic microwave background photons gain |
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energy as they fall into potential wells and lose it again as they climb back out. The origin of the effect is |
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gravitational redshift. For static potential wells, there is no net effect. However, if the potentials grow or |
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decay, there is a net effect, known as the Integrated Sachs-Wolfe effect. In a matter-dominated universe, linear |
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potentials stay constant. The late-time ISW effect refers to the fact that at late times, dark energy causes a |
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deviation from matter domination and linear potentials decay. This causes an effect in the cosmic microwave |
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background which has been measured in cross-correlation with large-scale structure. The early-time ISW refers |
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to the fact that right after recombination, radiation still contributed a non-negligible amount of the energy |
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density of the universe, causing potentials to grow. This causes the photons to gain energy. The early-time ISW |
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has not been detected experimentally. |
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## EXAMPLE 2 |
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USER: What are the definitions of galaxy cluster mass (M200m, M500c, etc.)? |
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ASSISTANT: Calculating a galaxy cluster's mass is like calculating the population of a sprawling city; as you |
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get further out from city center, the suburbs never end. Eventually you have to stop counting and just say that |
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from there on the people belong to a different town. |
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In cluster masses, we integrate from the cluster center out to some radius r螖 where 螖 might be 200, 500, or |
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some other number. The definition of this radius is that the density of the enclosed mass is 螖 times the |
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average density of the universe at that redshift. The associated mass is M螖. |
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Note that 'average density' can be defined in two ways. You can either include the energy density of dark |
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energy - in which case you are comparing to the critical density at that redshift - or you can use the matter |
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density only. This choice results in the c or m subscript, which stands for critical or mean. Note that the |
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critical density is higher than the mean density, so it gives an earlier cutoff in the integral. Therefore |
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'M螖c' masses are smaller than 'M螖m' ones. |
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## QUESTION |
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USER: <<<INSERT YOUR QUESTION>>> |
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ASSISTANT: |
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``` |
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## Example outputs |
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``` |
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USER: What is the current best measure of the optical depth to reionization? |
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ASSISTANT: The current best measure of the optical depth to reionization is 蟿=0.054卤0.007, as determined by the |
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Planck Collaboration et al. (2018b). This value provides strong evidence for reionization at high redshift and |
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helps constrain models of cosmic reionization. |
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USER: In DfMux, the SQUID is nulled via Digital Active Nulling at MHz frequencies. How is the SQUID kept nulled |
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at low frequency? |
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ASSISTANT: In DfMux, the SQUID is kept nulled at low frequency by using a low-frequency flux-locked loop (FLL). |
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The FLL is a feedback system that maintains the SQUID in its nulled state by adjusting the input current to |
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cancel out the flux signal. This is necessary because the SQUID is sensitive to magnetic fields, and the |
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magnetic field generated by the input current can change the bias flux, causing the SQUID to lose its null |
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state. The FLL helps to maintain the null state by continuously adjusting the input current to counteract any |
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changes in the bias flux. |
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USER: Why does a cross-spectrum not suffer from noise bias? |
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ASSISTANT: A cross-spectrum between two different tracers of the same underlying field does not suffer from |
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noise bias because the noise in each tracer is uncorrelated with the noise in the other tracer. This is because |
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the noise in each tracer is a random process that is independent of the other tracer. Therefore, the noise in |
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one tracer does not affect the expected value of the cross-spectrum between the two tracers. This is in |
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contrast to an auto-spectrum, which does suffer from noise bias because the noise in one tracer is correlated |
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with the noise in the same tracer. |
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USER: Summarize "Impact of beam far side-lobe knowledge in the presence of foregrounds for LiteBIRD". |
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ASSISTANT: This paper investigates the impact of beam far side-lobes on the estimation of the tensor-to-scalar |
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ratio in the presence of foregrounds for the LiteBIRD mission. The authors find that the presence of foregrounds |
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can significantly affect the estimation of the tensor-to-scalar ratio, and that the knowledge of the beam far |
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side-lobes is crucial for accurate results. The study also discusses the importance of accurately modeling the |
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beam profile and the challenges in estimating the tensor-to-scalar ratio in the presence of foregrounds. |
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USER: Explain a detailed design for a future CMB satellite. What detector technology would you choose? What |
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optics? Photometer vs spectrometer? etc. |
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ASSISTANT: A detailed design for a future CMB satellite would involve several key components. Firstly, the |
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choice of detector technology is crucial. One option could be using Transition Edge Sensor (TES) bolometers |
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coupled to superconducting detectors, similar to those used in the Planck mission. These detectors are highly |
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sensitive and can measure temperature fluctuations in the CMB with high precision. Another option could be |
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using Kinetic Inductance Detectors (KIDs), which offer fast response time and are less susceptible to |
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systematic effects. |
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Next, the optics design should aim to minimize stray light and ensure high optical efficiency. This can be |
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achieved by using a combination of reflective and refractive optics, along with a series of baffles and |
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filters to block unwanted stray light. |
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The choice between a photometer and a spectrometer depends on the science goals of the mission. A photometer |
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would provide broadband measurements of the CMB temperature and polarization anisotropies, while a spectrometer |
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would allow for more detailed studies of the spectral properties of the CMB. |
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Finally, the spacecraft design should consider factors such as thermal control, power generation, attitude |
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determination and control, communication, and data handling systems. It should also include redundant systems |
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to ensure reliability and fault tolerance during the long duration of the mission. |
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``` |
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## Qualitative evaluation |
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cosmosage_v1 is by far the best cosmosage model yet. However, like all LLMs, it continues to struggles with |
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_reliability_. While many of its answers are factually accurate, some are not. The outputs of cosmosage |
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(or any LLM) should not be trusted to be factual. |