Skip to Main content Skip to Navigation
Reports

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
Document type :
Reports
Complete list of metadata
https://hal.inria.fr/inria-00074396
Contributor : Rapport de Recherche Inria Connect in order to contact the contributor
Submitted on : Wednesday, May 24, 2006 - 3:13:05 PM
Last modification on : Friday, February 4, 2022 - 3:07:59 AM
Long-term archiving on: : Monday, April 5, 2010 - 12:09:07 AM

Files

Vignette du document
RR-2275.pdf

Identifiers

  • HAL Id : inria-00074396, version 1

Collections

INRIA | INRIA-RRRT | LARA | INRIA2

Citation

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⟩

Export

BibTeX TEI DC DCterms EndNote Datacite

Share

Metrics

Record views

56

Files downloads

338

 

Contact                    Legal Notice                    Personal Data