The robust stabilization of the angular position of a spacecraft with dynamic elastic elements under dissipative properties is proposed. The control scheme is based on bang-bang control and linear output feedback. The former is based on minimum-time optimal control and the latter is designed with the invariant ellipsoid method. The control is achieved under uncertainty in the system and disturbances in the output measurements.
Robust stabilization of a spacecraft with flexible elements using invariant ellipsoid technique
2008
5 Seiten, 14 Quellen
Conference paper
English
Attitude stabilization of large flexible spacecraft
AIAA | 1978
|Attitude Stabilization of Large Flexible Spacecraft
AIAA | 1981
|Spacecraft obstacle avoidance control method based on ellipsoid description
European Patent Office | 2020
|Flexible Spacecraft Control Using Robust Feedback Linearization
British Library Conference Proceedings | 2010
|