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EKF based surface fault detection and reconfiguration in aircraft control systems

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dc.contributor.authorCaliskan, Fikret
dc.contributor.authorHajiyev, Chingiz
dc.date.accessioned2026-01-24T18:36:10Z
dc.date.issued2000-01-01
dc.description.abstractIn this paper, a surface fault detection algorithm based on the extended Kalman filter (EKF) is presented. The innovation, the difference between the actual plant states, and the plant states identified by the EKF are evaluated for the fault detection and identification, and the control reconfiguration procedure is executed by considering the identified control distribution matrix.
dc.description.urihttps://doi.org/10.1109/acc.2000.876694
dc.description.urihttps://doi.org/10.1109/ACC.2000.876694
dc.description.urihttps://dx.doi.org/10.1109/acc.2000.876694
dc.identifier.doi10.1109/acc.2000.876694
dc.identifier.endpage1224 vol.2
dc.identifier.openairedoi_dedup___::2551066c770a143f80ac956eff3f824e
dc.identifier.orcid0000-0003-4115-341x
dc.identifier.startpage1220
dc.identifier.urihttps://hdl.handle.net/11527/37716
dc.publisherIEEE
dc.relation.ispartofProceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334)
dc.titleEKF based surface fault detection and reconfiguration in aircraft control systems
dc.typeArticle
dspace.entity.typePublication

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