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.


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    Titel :

    Study of the Space Station Freedom Response to the Disturbance Environment


    Beteiligte:
    A. Suleman (Autor:in) / V. J. Modi (Autor:in) / V. B. Venkayya (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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