Two adaptive controllers designed for the Spacecraft Control Laboratory Experiment (SCOLE) at NASA Langley Research Center are discussed. The first controller is an adaptive model following variable structure controller and the second is an indirect LQ adaptive controller. For each technique, the design of the controller is outlined and simulation results are presented. Plans for future studies are also discussed.


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    Titel :

    Adaptive control techniques for the SCOLE configuration


    Beteiligte:
    Ossman, K. (Autor:in) / Yurkovich, S. (Autor:in) / Ozguner, U. (Autor:in)

    Kongress:

    VPI&SU/AIAA Symposium ; 1987 ; Blacksburg, VA, United States


    Erscheinungsdatum :

    01.01.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    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


    Control of SCOLE

    Meirovitch, L. / Norris, M. A. | NTRS | 1987


    Control of the SCOLE Configuration Using Distributed Parameter Models

    Hsiao, M.-H. / Huang, J.-K. / National Aeronautics and Space Administration | British Library Conference Proceedings | 1994


    The SCOLE design challenge

    Taylor, Larry / Balakrishnan, A. V. | NTRS | 1987