The feasibility of providing active damping augmentation of the Space Shuttle Remote Manipulator System (RMS) following normal payload handling operations is investigated. The approach used in the analysis is described, and the results for both linear and nonlinear performance analysis of candidate laws are presented, demonstrating that significant improvement in the RMS dynamic response can be achieved through active control using measured RMS tip acceleration data for feedback.


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    Titel :

    Active Vibration Damping of the Space Shuttle Remote Manipulator System


    Beteiligte:
    M. A. Scott (Autor:in) / M. G. Gilbert (Autor:in) / M. E. Demeo (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    SCOTT, MICHAEL / GILBERT, MICHAEL / DEMEO, MARTHA | AIAA | 1991


    Active vibration damping of the Space Shuttle Remote Manipulator System

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    Active Vibration Damping of the Space Shuttle Remote Manipulator System

    Michael A. Scott / Michael G. Gilbert / Martha E. Demeo | AIAA | 1993


    Active vibration damping of the Space Shuttle remote manipulator system

    Scott, Michael A. / Gilbert, Michael G. / Demeo, Martha E. | NTRS | 1991