Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/83469
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dc.contributor.authorJiang, B.-
dc.contributor.authorGuo, Y.-
dc.contributor.authorShi, P.-
dc.date.issued2010-
dc.identifier.citationProceedings of the Institution of Mechanical Engineers Part I: Journal of Systems and Control Engineering, 2010; 224(6):713-723-
dc.identifier.issn0959-6518-
dc.identifier.issn2041-3041-
dc.identifier.urihttp://hdl.handle.net/2440/83469-
dc.description.abstractThis paper presents a framework for actuator fault accommodation using a multiple-model-based direct adaptive control approach that does not include explicit fault detection and isolation. This approach does not require exact information about the controlled system and persistent input excitations. The method can increase robustness and provides stable adaptation of unknown faults. Asymptotic model following conditions and adaptive rules are derived and system stability is guaranteed, while appropriate switching of the multiple models ensures asymptotic tracking for system outputs. An aircraft model is given to illustrate the efficiency of the proposed method.-
dc.description.statementofresponsibilityB Jiang, Y Guo, and P Shi-
dc.language.isoen-
dc.publisherProfessional Engineering Publishing Ltd-
dc.rights© Authors 2010-
dc.subjectactuator fault-
dc.subjectdirect adaptive reconfiguration control-
dc.subjectmultiple model-
dc.subjectflight control systems-
dc.titleAdaptive reconfiguration scheme for flight control systems-
dc.typeJournal article-
dc.identifier.doi10.1243/09596518JSCE894-
pubs.publication-statusPublished-
dc.identifier.orcidShi, P. [0000-0001-8218-586X]-
Appears in Collections:Aurora harvest 4
Electrical and Electronic Engineering publications

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