A relatively general formulation for studying the dynamics and control of an arbitrary spacecraft with interconnected flexible bodies has been developed. This self-contained and comprehensive numerical algorithm using system modes is applicable to a large class of spacecraft configurations of contemporary and future interest. Here, versatility of the approach is demonstrated through the dynamics and control studies aimed at the evolving Space Station Freedom.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Study of the Space Station Freedom Response to the Disturbance Environment


    Contributors:
    A. Suleman (author) / V. J. Modi (author) / V. B. Venkayya (author)

    Publication date :

    1994


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    A study of the Space Station Freedom response to the disturbance environment

    Suleman, Afzal / Modi, V. J. / Venkayya, V. B. | NTRS | 1994


    A Study of the Space Station `Freedom' Response to the Disturbance Environment (AAS 93-643)

    Suleman, A. / Modi, V. J. / Venkayya, V. B. et al. | British Library Conference Proceedings | 1993


    Space Station Freedom Disturbance Simulation and Management Tool

    LISMAN, SIMA / RATHBUN, DAVID | AIAA | 1990


    The Space Station Freedom microgravity environment

    Del Basso, Steve / Bogert, Philip B. | NTRS | 1993