This paper is concerned with the problem of slewing a large structure in space and suppressing any vibration at the same time. The structure is assumed to undergo large rigid-body motions and small elastic deformations. A perturbation method permits a maneuver strategy independent of the vibration control. Optimal control and pole placement techniques, formulated to include first-order actuator dynamics, are used to suppress the vibration during maneuver. The theory is illustrated by simultaneous maneuvering and vibration control of the Spacecraft Control Laboratory Experiment (SCOLE) model in a space environment.


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    Titel :

    Maneuvering and vibration control of flexible spacecraft


    Beteiligte:
    Meirovitch, L. (Autor:in) / Quinn, R. D. (Autor:in)


    Erscheinungsdatum :

    01.09.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Maneuvering and Vibration Control of Flexible Spacecraft

    L. Meirovitch / R. D. Quinn | NTIS | 1987


    Maneuvering and vibration control of flexible spacecraft

    Meirovitch, L. / Quinn, R. D. | NTRS | 1987




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