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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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