Nonlinear structurally stable control of a flexible spacecraft
The problem of counteracting nonlinear perturbations in order to maintain output regulation with internal stability of a flexible spacecraft is discussed. Asymptotic tracking of the main body and antenna rotations of a flexible spacecraft in the face of system uncertainties and disturbances is consi...
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Published in | [1992] Proceedings of the 31st IEEE Conference on Decision and Control pp. 1129 - 1134 vol.1 |
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Main Author | |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
1992
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Subjects | |
Online Access | Get full text |
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Summary: | The problem of counteracting nonlinear perturbations in order to maintain output regulation with internal stability of a flexible spacecraft is discussed. Asymptotic tracking of the main body and antenna rotations of a flexible spacecraft in the face of system uncertainties and disturbances is considered. The structurally stable control scheme proposed relies upon a novel extension to nonlinear systems of the internal model principle. Plant extension is investigated in three different cases, with the aim of providing an overview of the possible applications of the methodology used. A switching logic, working also in the case of large initial errors, is proposed for feedback control of spacecraft attitudes.< > |
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ISBN: | 9780780308725 0780308727 |
DOI: | 10.1109/CDC.1992.371540 |