The time-optimal slewing problem of flexible spacecraft is considered. The system is discretised by the assumed-modes method, and the problem is solved for a linearized model in reduced state space by parameter optimization. Optimality is verified by the maximal principle. The linear solution is used to obtain time-optimal solutions for the nonlinear problem.
Time optimal slewing of flexible spacecraft
Zeitoptimales Schwenken eines flexiblen Raumfahrzeugs
1987
5 Seiten, 11 Quellen
Conference paper
English
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