The Spacecraft Control Laboratory Experiment (SCOLE) was slewed from one attitude to the required attitude and an integral performance index which involves the control torques was minimized. Kinematic and dynamical equations, optimal control, two-point boundary-value problems, and estimation of unknown boundary conditions are presented.


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    Title :

    Optimal Torque Control for SCOLE (Spacecraft Control Laboratory Experiment) Slewing Maneuvers


    Contributors:
    P. M. Bainum (author) / F. Li (author)

    Publication date :

    1987


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English