The design of a robust compensator is considered for the SCOLE configuration using a frequency-response shaping technique based on the LQG/LTR 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 employed potentially should be 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


    Contributors:


    Publication date :

    1988-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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