The problem of stabilizing a tumbling satellite prior to attitude control is discussed. The method of Hamilton-Jacobi theory is used to derive an explicit closed-loop control law for the problem.


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    Title :

    On the Optimum Stabilization of a Satellite


    Contributors:


    Publication date :

    1965-10-01


    Size :

    1092643 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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