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dc.contributor.authorTanyer, İlker
dc.contributor.authorTatlıcıoğlu, Enver
dc.contributor.authorZergeroğlu, Erkan
dc.date.accessioned2017-10-23T10:50:31Z
dc.date.available2017-10-23T10:50:31Z
dc.date.issued2017-05
dc.identifier.citationTanyer, İ., Tatlıcıoğlu, E., and Zergeroğlu, E. (2017). Model reference tracking control of an aircraft: a robust adaptive approach. International Journal of Systems Science, 48(7), 1428-1437. doi:10.1080/00207721.2016.1261200en_US
dc.identifier.issn0020-7721
dc.identifier.urihttp://doi.org/10.1080/00207721.2016.1261200
dc.identifier.urihttp://hdl.handle.net/11147/6408
dc.description.abstractThis work presents the design and the corresponding analysis of a nonlinear robust adaptive controller for model reference tracking of an aircraft that has parametric uncertainties in its system matrices and additive state- and/or time-dependent nonlinear disturbance-like terms in its dynamics. Specifically, robust integral of the sign of the error feedback term and an adaptive term is fused with a proportional integral controller. Lyapunov-based stability analysis techniques are utilised to prove global asymptotic convergence of the output tracking error. Extensive numerical simulations are presented to illustrate the performance of the proposed robust adaptive controller.en_US
dc.language.isoengen_US
dc.publisherTaylor & Francisen_US
dc.relation.isversionof10.1080/00207721.2016.1261200en_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectAircraftsen_US
dc.subjectLyapunov methodsen_US
dc.subjectRobust adaptive controlleren_US
dc.subjectUncertain dynamic systemsen_US
dc.titleModel reference tracking control of an aircraft: a robust adaptive approachen_US
dc.typearticleen_US
dc.contributor.authorIDTR123720en_US
dc.contributor.iztechauthorTanyer, İlker
dc.contributor.iztechauthorTatlıcıoğlu, Enver
dc.relation.journalInternational Journal of Systems Scienceen_US
dc.contributor.departmentİYTE, Mühendislik Fakültesi, Elektrik-Elektronik Mühendisliği Bölümüen_US
dc.identifier.volume48en_US
dc.identifier.issue7en_US
dc.identifier.startpage1428en_US
dc.identifier.endpage1437en_US
dc.identifier.wosWOS:000396822800008
dc.identifier.scopusSCOPUS:2-s2.0-85006152352


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