Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/87943
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dc.contributor.authorWang, J.-
dc.contributor.authorJiang, B.-
dc.contributor.authorShi, P.-
dc.contributor.authorWang, H.-
dc.date.issued2008-
dc.identifier.citation3rd International Conference on Innovative Computing Information and Control, ICICIC'08, 2008, pp.1-5-
dc.identifier.isbn9780769531618-
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.-
dc.description.statementofresponsibilityJianfei Wang, Bin Jiang, Peng Shi, Hankang Wang-
dc.language.isoen-
dc.publisherIEEE-
dc.rights© 2008 IEEE-
dc.source.urihttp://dx.doi.org/10.1109/icicic.2008.118-
dc.titleAdaptive observer based actuator fault diagnosis for ASV-
dc.typeConference paper-
dc.contributor.conferenceInternational Conference on Innovative Computing, Information and Control (ICICIC) (18 Jun 2008 - 20 Jun 2008 : Dalian, Liaoning, China)-
dc.identifier.doi10.1109/ICICIC.2008.118-
dc.publisher.placeOnline-
pubs.publication-statusPublished-
dc.identifier.orcidShi, P. [0000-0001-8218-586X]-
Appears in Collections:Aurora harvest 7
Electrical and Electronic Engineering publications

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