Variable structure systems theory is used to design an automatic controller for active nutation damping in momentum biased stabilized spacecraft. Robust feedback stabilization of roll and yaw angular dynamcis is achieved with prescribed qualitative characteristics which are totally independent of the spacecraft defining parameters.


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    Title :

    Variable structure controller design for spacecraft nutation damping


    Additional title:

    Entwurf von Reglern variabler Struktur zur Daempfung der Schlingerbewegungen von Raumfahrzeugen


    Contributors:

    Published in:

    Publication date :

    1987


    Size :

    4 Seiten, 6 Bilder, 12 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English