The design of a robust compensator is considered for the SCOLE (spacecraft control laboratory experiment) configuration using a frequency-response shaping technique based on the LQG/LTR (linear quadratic Gaussian/loop transfer recovery) algorithm. Results indicate that a tenth-order compensator can be used to meet stability-performance-robustness conditions for a 26th-order SCOLE model without destabilizing spillover effects. Since the SCOLE configuration is representative of many proposed spaceflight experiments, the results and design techniques used should be potentially applicable to a wide range of large-space-structure control problems.


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    Titel :

    Robust model-based controller synthesis for the SCOLE configuration


    Weitere Titelangaben:

    Synthese von robusten, auf mathematischen Modellen beruhenden, Reglern fuer die SCOLE (spacecraft control laboratory experiment) Anordnung


    Beteiligte:
    Armstrong, E.S. (Autor:in) / Joshi, S.M. (Autor:in) / Stewart, E.J. (Autor:in)


    Erscheinungsdatum :

    1988


    Format / Umfang :

    6 Seiten, 13 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Adaptive control techniques for the SCOLE configuration

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    Maneuver and vibration control of SCOLE

    QUINN, R. / MEIROVITCH, L. | AIAA | 1986


    Maneuver and vibration control of SCOLE

    QUINN, R. D. / MEIROVITCH, L. | AIAA | 1988