In this paper, experimental verifications of various jerk-limited control designs are presented. The focus is on a large slew maneuver of a flexible spacecraft where the fast and accurate pointing is required at the end of the maneuver. Various control profiles are investigated including input shaping and jerk-limited optimal control profiles, especially to account the effect of jerk in the control profile. The control design is verified by the experiment using the Flexible Spacecraft Simulator (FSS).


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    Title :

    Experiments on Jerk-Limited Slew Maneuvers of a Flexible Spacecraft


    Contributors:
    J Kim (author) / N.B Agrawal (author)

    Publication date :

    2006


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    AIAA-2006-6187 Experiments on Jerk-Limited Slew Maneuvers of a Flexible Spacecraft

    Kim, J. / Agrawal, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


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