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dc.contributor.authorTanyer, İlker
dc.contributor.authorTatlıcıoğlu, Enver
dc.contributor.authorZergeroğlu, Erkan
dc.date.accessioned2017-04-07T11:40:46Z
dc.date.available2017-04-07T11:40:46Z
dc.date.issued2013
dc.identifier.citationTanyer, İ., Tatlıcıoğlu, E., and Zergeroğlu, E. (2013, June 23-26). A robust dynamic inversion technique for asymptotic tracking control of an aircraft. Paper presented at the 9th Asian Control Conference. doi:10.1109/ASCC.2013.6606263en_US
dc.identifier.isbn9781467357692
dc.identifier.urihttp://doi.org/10.1109/ASCC.2013.6606263
dc.identifier.urihttp://hdl.handle.net/11147/5256
dc.description9th Asian Control Conference, ASCC 2013; Istanbul; Turkey; 23 June 2013 through 26 June 2013en_US
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. © 2013 IEEE.en_US
dc.language.isoengen_US
dc.publisherIEEEen_US
dc.relation.isversionof10.1109/ASCC.2013.6606263en_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectControllersen_US
dc.subjectAircraft modelsen_US
dc.subjectController designsen_US
dc.subjectGlobal asymptotic trackingen_US
dc.subjectRobust dynamic inversionsen_US
dc.titleA robust dynamic inversion technique for asymptotic tracking control of an aircraften_US
dc.typeconferenceObjecten_US
dc.contributor.authorIDTR123720en_US
dc.contributor.iztechauthorTanyer, İlker
dc.contributor.iztechauthorTatlıcıoğlu, Enver
dc.relation.journal9th Asian Control Conferenceen_US
dc.contributor.departmentİYTE, Mühendislik Fakültesi, Elektrik-Elektronik Mühendisliği Bölümüen_US
dc.identifier.wosWOS:000333734900274
dc.identifier.scopusSCOPUS:2-s2.0-84886509619


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