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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    Title :

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


    Contributors:

    Conference:

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


    Publication date :

    1987-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English