Attitude Determination and Control System for a LEO Debris Chaser Small Satellite
Author:
Affiliation:
1. Tata Consultancy Services Ltd
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0519
Reference17 articles.
1. Magnetic-Only Orbit and Attitude Estimation Using the Square-Root Unscented Kalman Filter: Application to the PROBA-2 Spacecraft
2. Kalman Filtering for Spacecraft Attitude Estimation
3. A Magnetometer-Only Attitude Determination Strategy for Small Satellites: Design of the Algorithm and Hardware-in-the-Loop Testing
4. A new optimal fusion algorithm for spacecraft attitude determination and estimation algorithms
5. Attitude and orbit determination for small satellite using magnetometer measurement
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