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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    Title :

    Robust model-based controller synthesis for the SCOLE configuration


    Additional title:

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


    Contributors:


    Publication date :

    1988


    Size :

    6 Seiten, 13 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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