A double rate digital control law is proposed for large angle attitude maneuvers and stabilization of flexible satellites. Such a control law improves, with respect to the continuous control, the damping down of the elastic oscillations. Simulation results are discussed.
Multirate three axes attitude stabilization of spacecraft / Monaco, S.; Normand-Cyrot, D.; Stornelli, S.. - 1:(1989), pp. 797-802. (Intervento presentato al convegno Proceedings of the 28th IEEE Conference on Decision and Control. Part 1 (of 3) tenutosi a Tampa, FL; USA) [10.1109/CDC.1989.70230].
Multirate three axes attitude stabilization of spacecraft
Monaco S.
;Normand-Cyrot D.
;
1989
Abstract
A double rate digital control law is proposed for large angle attitude maneuvers and stabilization of flexible satellites. Such a control law improves, with respect to the continuous control, the damping down of the elastic oscillations. Simulation results are discussed.File allegati a questo prodotto
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