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Time-varying feedback stabilization of the attitude of a rigid spacecraft

Pascal Morin 1 Claude Samson 1 Jean-Baptiste Pomet 2 Zhong-Ping Jiang 1, 2
1 ICARE - Instrumentation, control and architecture of advanced robots
CRISAM - Inria Sophia Antipolis - Méditerranée
2 MIAOU - Mathematics and Computing in Automatic Control and Optimization for the User
CRISAM - Inria Sophia Antipolis - Méditerranée
Abstract : It is known that rigid body models with two controls cannot be locally asymptotically stabilized by smooth feedbacks which are functions of the state only. This impossibility does no longer hold when the feedback is also a function of time, or when it is non smooth. A locally stabilizing smooth time-varying feedback is here explicitly derived by using Center Manifold Theory combined with averaging and Lyapunov techniques.
Keywords : TIME-VARYING CONTROL SMOOTH FEEDBACK ATTITUDE STABILIZATION
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https://hal.inria.fr/inria-00074396
Contributor : Rapport de Recherche Inria <>
Submitted on : Wednesday, May 24, 2006 - 3:13:05 PM
Last modification on : Monday, October 14, 2019 - 3:12:02 PM
Document(s) archivé(s) le : Monday, April 5, 2010 - 12:09:07 AM

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  • HAL Id : inria-00074396, version 1

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Pascal Morin, Claude Samson, Jean-Baptiste Pomet, Zhong-Ping Jiang. Time-varying feedback stabilization of the attitude of a rigid spacecraft. [Research Report] RR-2275, INRIA. 1994. ⟨inria-00074396⟩

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