A Robust Dynamic Inversion Technique for Asymptotic Tracking Control of an Aircraft

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dc.contributor.authorTanyer, Ilker
dc.contributor.authorTatlıcıoğlu, Enver
dc.contributor.authorZergeroğlu, Erkan
dc.date.accessioned2025-10-29T11:37:03Z
dc.date.issued2013
dc.departmentFakülteler, Mühendislik Fakültesi, Bilgisayar Mühendisliği Bölümü
dc.departmentFakülteler, Mühendislik Fakültesi, Elektronik Mühendisliği Bölümü
dc.description9th Asian Control Conference (ASCC) -- JUN 23-26, 2013 -- Istanbul, TURKEY
dc.description.abstractIn this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear disturbance-like terms. In the design of the controller, dynamic inversion technique is utilized in conjuction with a robust term. Only the output of aircraft dynamics is utilized in the controller design and acceleration measurements are not required. Lyapunov based stability analysis is used to prove global asymptotic tracking.
dc.identifier.isbn978-1-4673-5769-2
dc.identifier.isbn978-1-4673-5767-8
dc.identifier.issn2072-5639
dc.identifier.orcid0000-0003-3680-4628
dc.identifier.scopus2-s2.0-84886509619
dc.identifier.scopusqualityN/A
dc.identifier.urihttps://hdl.handle.net/20.500.14854/13633
dc.identifier.wosWOS:000333734900274
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherIEEE
dc.relation.ispartof2013 9th Asian Control Conference (Ascc)
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20251020
dc.subjectFlight Control
dc.subjectAdaptive-Control
dc.subjectFeedback
dc.titleA Robust Dynamic Inversion Technique for Asymptotic Tracking Control of an Aircraft
dc.typeConference Object

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