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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    Title :

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


    Contributors:
    R. S. Harris (author) / D. C. Todman (author) / M. J. Hammond (author) / R. J. Annett (author)

    Publication date :

    1977


    Size :

    240 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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