Robust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbance

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dc.authorid0000-0001-5623-9975en_US
dc.authorid0000-0003-4745-5304
dc.authorid0000-0003-3680-4628
dc.authorid0000-0002-1211-0448
dc.contributor.authorTanyer, İlker
dc.contributor.authorTatlıcıoğlu, Enver
dc.contributor.authorZergeroğlu, Erkan
dc.contributor.authorDeniz, Meryem
dc.contributor.authorBayrak, Alper
dc.date.accessioned2021-06-23T19:43:02Z
dc.date.available2021-06-23T19:43:02Z
dc.date.issued2016
dc.departmentBAİBÜ, Mühendislik Fakültesi, Elektrik Elektronik Mühendisliği Bölümüen_US
dc.description.abstractIn this study, an asymptotic tracking controller is developed for an aircraft model subject to additive, state-dependent, non-linear disturbance-like terms. Dynamic inversion technique in conjunction with robust integral of the sign of the error term is utilised in the controller design. Compared to the previous studies, the need of acceleration measurements of the aircraft have been removed. In addition, the proposed controller design utilises only the output of aircraft dynamics. Lyapunov based analysis is applied to prove global asymptotic convergence of the tracking error signal. Numerical simulation results are presented to illustrate the performance of the proposed robust controller.en_US
dc.identifier.doi10.1049/iet-cta.2015.1304
dc.identifier.endpage1619en_US
dc.identifier.issn1751-8644
dc.identifier.issn1751-8652
dc.identifier.issue14en_US
dc.identifier.scopus2-s2.0-84987607026en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage1612en_US
dc.identifier.urihttps://doi.org/10.1049/iet-cta.2015.1304
dc.identifier.urihttps://hdl.handle.net/20.500.12491/8672
dc.identifier.volume10en_US
dc.identifier.wosWOS:000384007500002en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.institutionauthorBayrak, Alper
dc.language.isoenen_US
dc.publisherInst Engineering Technology-Ieten_US
dc.relation.ispartofIet Control Theory And Applicationsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectRobust Controlen_US
dc.subjectAutonomous Aerial Vehiclesen_US
dc.subjectAircraften_US
dc.subjectControl System Synthesisen_US
dc.subjectLyapunov Methodsen_US
dc.subjectNumerical Analysisen_US
dc.subjectRobust Output Tracking Controlen_US
dc.subjectUnmanned Aerial Vehicleen_US
dc.subjectAdditive State Dependent Disturbanceen_US
dc.subjectAsymptotic Tracking Controlleren_US
dc.subjectAircraft Modelen_US
dc.subjectDynamic Inversion Techniqueen_US
dc.subjectAircraft Dynamicsen_US
dc.subjectLyapunov Based Analysisen_US
dc.subjectGlobal Asymptotic Convergenceen_US
dc.subjectNumerical Simulationen_US
dc.titleRobust output tracking control of an unmanned aerial vehicle subject to additive state dependent disturbanceen_US
dc.typeArticleen_US

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