The dynamics and control of arbitrary slew maneuvers of a large flexible spacecraft are developed. The dynamics of slew maneuvers are nonlinear and include the coupling between the rigid orbiter and the flexible appendage. A decentralized control scheme is used to perform a large-angle slew maneuver about an arbitrary axis in space and to suppress the vibrations of the flexible appendage during and after the maneuver.


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    Title :

    Slew maneuvers of large flexible spacecrafts


    Contributors:

    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Decentralized slew maneuver control of large flexible spacecrafts

    Kakad, Y.P. / Crotts, B.D. | Tema Archive | 1990





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