Update README.md

README.md

@@ -72,6 +72,66 @@ dataset_info:
   download_size: 2623414
   dataset_size: 8924256
 ---
-# Dataset Card for "nasa_turbofan_degradation_FD003"
 
-[More Information needed](https://github.com/huggingface/datasets/blob/main/CONTRIBUTING.md#how-to-contribute-to-the-dataset-cards)
+# CMAPSS Jet Engine Simulated Data FD003 - NASA
+
+This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD003.
+
+Train trjectories: 100
+Test trajectories: 100
+Conditions: ONE (Sea Level)
+Fault Modes: TWO (HPC Degradation, Fan Degradation)
+
+## Sensor Descriptions
+
+| Sensor ID | Description                                | Units       |
+|-----------|--------------------------------------------|-------------|
+| s_1       | Total temperature at fan inlet            | ◦R          |
+| s_2       | Total temperature at LPC outlet           | ◦R          |
+| s_3       | Total temperature at HPC outlet           | ◦R          |
+| s_4       | Total temperature at LPT outlet           | ◦R          |
+| s_5       | Pressure at fan inlet                     | psia        |
+| s_6       | Total pressure in bypass-duct             | psia        |
+| s_7       | Total pressure at HPC outlet              | psia        |
+| s_8       | Physical fan speed                        | rpm         |
+| s_9       | Physical core speed                       | rpm         |
+| s_10      | Engine pressure ratio (P50/P2)            | -           |
+| s_11      | Static pressure at HPC outlet             | psia        |
+| s_12      | Ratio of fuel flow to Ps30                | pps/psia    |
+| s_13      | Corrected fan speed                      | rpm         |
+| s_14      | Corrected core speed                      | rpm         |
+| s_15      | Bypass Ratio                              | -           |
+| s_16      | Burner fuel-air ratio                     | -           |
+| s_17      | Bleed Enthalpy                            | -           |
+| s_18      | Demanded fan speed                        | rpm         |
+| s_19      | Demanded corrected fan speed              | rpm         |
+| s_20      | HPT coolant bleed                         | lbm/s       |
+| s_21      | LPT coolant bleed                         | lbm/s       |
+
+## Units Explanation
+
+- ◦R: Rankine scale
+- HPT: High Pressure Temperature
+- LPT: Low Pressure Temperature
+- HPC: High Pressure Chamber
+- LPC: Low Pressure Chamber
+- rpm: rotation per minute
+- psia: pound per square inch
+- pps: pulse per second
+- lbm: pound mass
+
+## Source
+
+[CMAPSS Jet Engine Simulated Data](https://data.nasa.gov/Aerospace/CMAPSS-Jet-Engine-Simulated-Data/ff5v-kuh6/about_data)
+
+## Citation
+
+```bibtex
+@article{Saxena2008DamagePM,
+  title={Damage propagation modeling for aircraft engine run-to-failure simulation},
+  author={Abhinav Saxena and Kai Goebel and Donald C. Simon and Neil H. W. Eklund},
+  journal={2008 International Conference on Prognostics and Health Management},
+  year={2008},
+  pages={1-9},
+  url={https://api.semanticscholar.org/CorpusID:206508104}
+}