Robust compensator design for attitude control of the Spacecraft Control Laboratory Experiment (SCOLE) configuration is considered. A loop-shaping procedure similar to that used in the LQG/LTR method is used to iteratively design the compensator. A satisfactory compensator is obtained by including the rigid modes and three elastic modes in the design model.


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    Titel :

    Design of robust line-of-sight pointing control system for the SCOLE configuration


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

    Kongress:

    1987 American Control Conference ; 1987 ; Minneapolis, MN, United States


    Erscheinungsdatum :

    01.01.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch