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On the Optimum Stabilization of a Satellite |
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| Authors: | Kumar K. S. P. |
| Affiliation: | Department of Electrical Engineering University of Minnesota Minneapolis, Minn.; |
| Abstract: | 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. |
| Keywords: | |