Output tracking control of an aircraft subject to additive state dependent disturbance: an optimal control approach

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dc.authoridTanyer, Ilker/0000-0003-3680-4628
dc.authorscopusid35103640800
dc.authorscopusid14034778100
dc.authorscopusid57220036361
dc.contributor.authorTanyer, Ilker
dc.contributor.authorTatlicioglu, Enver
dc.contributor.authorZergeroglu, Erkan
dc.date.accessioned2023-01-12T20:12:14Z
dc.date.available2023-01-12T20:12:14Z
dc.date.issued2021
dc.departmentN/A/Departmenten_US
dc.description.abstractIn this paper, model reference output feedback tracking control of an aircraft subject to additive, uncertain, nonlinear disturbances is considered. In order to present the design steps in a clear fashion: first, the aircraft dynamics is temporarily assumed as known with all the states of the system available. Then a feedback linearizing controller minimizing a performance index while only requiring the output measurements of the system is proposed. As the aircraft dynamics is uncertain and only the output is available, the proposed controller makes use of a novel uncertainty estimator. The stability of the closed loop system and global asymptotic tracking of the proposed method are ensured via Lyapunov based arguments, asymptotic convergence of the controller to an optimal controller is also established. Numerical simulations are presented in order to demonstrate the feasibility and performance of the proposed control strategy.en_US
dc.identifier.doi10.24425/acs.2021.137418
dc.identifier.endpage286en_US
dc.identifier.issn2300-2611
dc.identifier.issn2300-2611en_US
dc.identifier.issue2en_US
dc.identifier.scopus2-s2.0-85112494328en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage267en_US
dc.identifier.urihttps://doi.org/10.24425/acs.2021.137418
dc.identifier.urihttps://hdl.handle.net/11454/78271
dc.identifier.volume31en_US
dc.identifier.wosWOS:000671275500002en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherPolska Akad Nauk, Polish Acad Sciencesen_US
dc.relation.ispartofArchives Of Control Sciencesen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectoptimal controlen_US
dc.subjectaerospace applicationsen_US
dc.subjectnonlinear systemsen_US
dc.subjectmechanical/mechatronics applicationsen_US
dc.subjectrobust controlen_US
dc.subjectNonlinear-Systemsen_US
dc.subjectAdaptive-Controlen_US
dc.subjectNeural-Networksen_US
dc.titleOutput tracking control of an aircraft subject to additive state dependent disturbance: an optimal control approachen_US
dc.typeArticleen_US

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