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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Robust model-based controller synthesis for the SCOLE configuration


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


    Erscheinungsdatum :

    01.10.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Robust model-based controller synthesis for the SCOLE configuration

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



    Regulation of the SCOLE configuration

    Norris, Gregory A. / Collins, Emmanuel G. / Skelton, Robert E. | NTRS | 1987


    Minimum time slew of the SCOLE configuration

    Fisher, S. / Posbergh, T. / Lindbergh, R. | NTRS | 1984


    Adaptive control techniques for the SCOLE configuration

    Ossman, K. / Yurkovich, S. / Ozguner, U. | NTRS | 1988