A Variable Structure Control (VSC) approach is presented for multi-axial spacecraft attitude maneuvers. Nonlinear sliding surfaces are proposed which result in asymptotically stable, ideal linear decoupled sliding motions of Cayley-Rodrigues attitude parameters, as well as of angular velocities. The resulting control laws are interpreted as more robust and more easily implemented versions of those previously obtained by feedback linearization.


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    Title :

    Spacecraft reorientation maneuvers via linearizing variable structure control


    Additional title:

    Reaorientierungsmanoever von Raumfahrzeugen durch die Linearisierung einer variablen Strukturregelung


    Contributors:

    Published in:

    Twentieth ; 477-481


    Publication date :

    1987


    Size :

    5 Seiten, 6 Bilder, 20 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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