Report presents theoretical foundation for attitude control system for proposed Space Station Freedom in orbit around Earth. Intended to maintain space station in torque equilibrium with designated axes of its structure aligned with local vertical, local along-trajectory horizontal, and local across-trajectory horizontal axes, respectively. System required to provide desired combination of control performance and stability in presence of disturbances (e.g., variations in masses of payloads, movements of astronauts and equipment, atmospheric drag, gravitational anomalies, and interactions with docking spacecraft).
Adaptive Attitude Control System For Space Station
NASA Tech Briefs ; 19 , 7
1995-07-01
Miscellaneous
No indication
English
Adaptive Attitude Control System for Space Station
Online Contents | 1995
Adaptive nonlinear attitude control of the Space Station
AIAA | 1994
|Adaptive Nonlinear Attitude Control of the Space Station
British Library Conference Proceedings | 1994
|