Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/87943
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dc.contributor.authorWang, J.en
dc.contributor.authorJiang, B.en
dc.contributor.authorShi, P.en
dc.contributor.authorWang, H.en
dc.date.issued2008en
dc.identifier.citation3rd International Conference on Innovative Computing Information and Control, ICICIC'08, 2008 / pp.1-5en
dc.identifier.isbn9780769531618en
dc.identifier.urihttp://hdl.handle.net/2440/87943-
dc.description.abstractThis paper deals with the actuator fault diagnosis and accommodation problem for the aero space vehicle (ASV). A novel nonlinear robust adaptive observer is developed for estimation of the actuator fault under the Lipschitz condition on the nonlinear part of such systems, which is used to continuously accommodate the control signal, so as to ensure the stability of faulty system. Finally, simulation results about ASV are presented to illustrate the feasibility and effectiveness of the proposed methods.en
dc.description.statementofresponsibilityJianfei Wang, Bin Jiang, Peng Shi, Hankang Wangen
dc.language.isoenen
dc.publisherIEEEen
dc.rights© 2008 IEEEen
dc.titleAdaptive observer based actuator fault diagnosis for ASVen
dc.typeConference paperen
dc.identifier.rmid0020128341en
dc.contributor.conferenceInternational Conference on Innovative Computing, Information and Control (ICICIC) (18 Jun 2008 - 20 Jun 2008 : Dalian, Liaoning, China)en
dc.identifier.doi10.1109/ICICIC.2008.118en
dc.publisher.placeOnlineen
dc.identifier.pubid19494-
pubs.library.collectionElectrical and Electronic Engineering publicationsen
pubs.library.teamDS01en
pubs.verification-statusVerifieden
pubs.publication-statusPublisheden
dc.identifier.orcidShi, P. [0000-0001-8218-586X]en
Appears in Collections:Electrical and Electronic Engineering publications

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