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dc.contributor.authorHamayun, M.T.
dc.contributor.authorEdwards, Christopher
dc.contributor.authorAlwi, Halim
dc.date.accessioned2015-03-25T13:39:28Z
dc.date.issued2013-04-09
dc.description.abstractIn this paper a new fault tolerant control scheme is proposed, where only measured system outputs are assumed to be available. The scheme ensures closed-loop stability throughout the entire closed-loop response of the system even in the presence of certain actuator faults/failures. This is accomplished by incorporating ideas of integral sliding modes, unknown input observers and a fixed control allocation scheme. A rigorous closed-loop stability analysis is undertaken, and in fact a convex representation of the problem is created in order to synthesize the controller and observer gains. The efficacy of the proposed scheme is tested by applying it to a benchmark civil aircraft model.en_GB
dc.identifier.citationVol. 49 (6), pp. 1830 - 1837en_GB
dc.identifier.doi10.1016/j.automatica.2013.02.043
dc.identifier.urihttp://hdl.handle.net/10871/16612
dc.language.isoenen_GB
dc.publisherElsevieren_GB
dc.subjectfault tolerant control (FTC)en_GB
dc.subjectIntegral sliding mode (ISM) controlen_GB
dc.subjectLinear matrix inequalities (LMI)en_GB
dc.titleA fault tolerant control allocation scheme with output integral sliding modesen_GB
dc.typeArticleen_GB
dc.date.available2015-03-25T13:39:28Z
dc.identifier.issn0005-1098
dc.descriptionCopyright © 2013 Elsevier. NOTICE: this is the author’s version of a work that was accepted for publication in Automatica. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in Automatica Vol. 49 (2013), DOI: 10.1016/j.automatica.2013.02.043en_GB
dc.identifier.journalAutomaticaen_GB


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