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 (Space Control Laboratory Experiment) Configuration


    Contributors:

    Publication date :

    1988


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Robust model-based controller synthesis for the SCOLE configuration

    Armstrong, E.S. / Joshi, S.M. / Stewart, E.J. | Tema Archive | 1988


    Robust model-based controller synthesis for the SCOLE configuration

    Armstrong, E. S. / Joshi, S. M. / Stewart, E. J. | NTRS | 1988




    SCOLE (Spacecraft Control Laboratory Experiment) Design Challenge

    L. Taylor / A. V. Balakrishnan | NTIS | 1987