The dynamics of a zero-momentum three-axis attitude controlled satellite is used to formulate an optimal control problem, which is then solved for the special case where the flywheels operate in a nonsaturating mode. The results then serve as guidelines in the design of simple open-loop and feedback controllers.


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    Title :

    Nonsaturating Satellite Open-Loop Feedback Controls


    Contributors:
    Guibord, A. (author) / Ahmed, N.U. (author)

    Published in:

    Publication date :

    1979-03-01


    Size :

    1166695 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Nonsaturating satellite open-loop feedback controls

    Guibord, A. / Ahmed, N.U. | Tema Archive | 1979


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