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.
On the Optimum Stabilization of a Satellite
IEEE Transactions on Aerospace and Electronic Systems ; AES-1 , 2 ; 82-83
01.10.1965
1092643 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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