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).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Adaptive Attitude Control System For Space Station


    Contributors:

    Published in:

    Publication date :

    1995-07-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Adaptive control applied to Space Station attitude control system

    LAM, QUANG / CHIPMAN, RICHARD / HU, TSAY-HSIN et al. | AIAA | 1992


    Adaptive control applied to Space Station attitude control system

    Lam, Quang M. / Chipman, Richard / Hu, Tsay-Hsin G. et al. | NTRS | 1992



    Adaptive Nonlinear Attitude Control of the Space Station

    Paynter, S. J. / AIAA | British Library Conference Proceedings | 1994