Computation, details, computer listings, graphs, and tables are presented for the investigation into flexure-satellite attitude interaction due to two uniform beam arrays on a three axis stabilized spacecraft.


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    Titel :

    Attitude Control of Three-Axes Stabilized Spacecraft with Flexible Appendages, Volume 2


    Beteiligte:
    R. S. Harris (Autor:in) / D. C. Todman (Autor:in) / M. J. Hammond (Autor:in) / R. J. Annett (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    240 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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