Parameter Estimation Based Angular Velocity Observer Design for Rigid-Body Spacecraft
Author:
Affiliation:
1. Beihang University,Beijing,China,102206
2. Northwestern Polytechnical University,National Key Laboratory of Aerospace Flight Dynamics,Xi'an,China,710072
3. Shanghai Institute of Satellite Engineering,Shanghai,China,201109
Funder
National Natural Science Foundation of China
Shanghai Academy of Spaceflight Technology
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10590709/10590710/10591304.pdf?arnumber=10591304
Reference25 articles.
1. Fundamentals of Spacecraft Attitude Determination and Control
2. Classification of Algorithms for Angular Velocity Estimation
3. A globally convergent angular velocity observer for rigid body motion
4. Output feedback control for attitude tracking
5. Partial Lyapunov Strictification: Smooth Angular Velocity Observers for Attitude Tracking Control
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