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    Titel :

    AIAA-2006-6447 Complementary Roll/Yaw Attitude Controller for Three Axis Authority Momentum Spacecraft



    Kongress:

    AIAA guidance, navigation and control conference ; 2006 ; Keystone, Colo



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    13 pages


    Anmerkungen:

    Paper numbers 2006-6037 to 6807 with gaps held



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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