Problem of stabilizing tumbling satellite prior to attitude control is analyzed; method of Hamilton-Jacobi theory is used to derive explicit closed-loop control law.


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    Title :

    On optimum stabilization of satellite


    Additional title:

    IEEE Trans Aerospace Electronic Systems


    Contributors:


    Publication date :

    1965


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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