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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    Titel :

    Experiments on Jerk-Limited Slew Maneuvers of a Flexible Spacecraft


    Beteiligte:
    J Kim (Autor:in) / N.B Agrawal (Autor:in)

    Erscheinungsdatum :

    2006


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    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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