The Optimum Stabilization of a tumbling satellite via Hamilton-Jacobi theory has been reported by one of the authors before in "On the optimum stabilization of a satellite" [2]. This companion paper discusses the synthesis of a specific optimum control law for the same problem and compares the results with the optimum solution. It is shown that a specific optimum control law yields, acceptable performance while being much easier to instrument than the optimum control law.


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    Title :

    Stabilization of a Satellite via Specific Optimum Control


    Contributors:


    Publication date :

    1966-07-01


    Size :

    1716427 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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