Control gains computed via matrix Riccati equation. Software-based system controlling aim of gimbaled rocket motor on spacecraft adaptive and optimal in sense it adjusts control gains in response to feedback, according to optimizing algorithm based on cost function. Underlying control concept also applicable, with modifications, to thrust-vector control on vertical-takeoff-and-landing airplanes, control of orientations of scientific instruments, and robotic control systems.


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    Title :

    Thrust-Vector-Control System


    Contributors:

    Published in:

    Publication date :

    1992-02-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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