Stabilization of a Satellite via Specific Optimum Control |
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| Authors: | Kumar K S P Teng Lincoln |
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| Institution: | Dept. of Electrical Engineering University of Minnesota Minneapolis, Minn.; |
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| Abstract: | 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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