Design of MPCs for a fixed wing UAV

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dc.contributor.authorUlker, Hakan
dc.contributor.authorBaykara, Cemal
dc.contributor.authorOzsoy, Can
dc.date.accessioned2024-03-13T10:35:37Z
dc.date.available2024-03-13T10:35:37Z
dc.date.issued2017
dc.departmentİstanbul Beykent Üniversitesien_US
dc.description.abstractPurpose - The purpose of the paper is to examine a fixed wing unmanned aerial vehicle (UAV) as it undergoes five flight scenarios under straight and level, level climb, level turn, climbing turn and level steady heading sideslip conditions in a desired and controlled manner using constrained multi input multi output (MIMO) model predictive controllers (MPCs). Design/methodology/approach - An MPC strategy based on the lateral and longitudinal linear models is proposed for the flight control design. Simulations are carried out for the nonlinear closed-loop aircraft Simulink model available from the University of Minnesota UAV research group with the implemented MIMO MPCs designed in this paper. Findings - The results of the simulations show that the MIMO MPCs can achieve satisfactory performance and flying qualities under three different test conditions in terms of existing unmeasured outputs and unmeasured output disturbances. Practical Implications - The MPCs designed in this paper can be implemented to UAVs. Therefore, the implementation is considered as an advanced research. Originality/value - The proposed MPC design in this paper provides more flexibility in terms of tracking complex trajectories comparing with the classical controllers in the literature. Besides they provide to change more than one reference of the states at any time.en_US
dc.identifier.doi10.1108/AEAT-08-2015-0198
dc.identifier.endpage901en_US
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.issue6en_US
dc.identifier.scopus2-s2.0-85033462532en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage893en_US
dc.identifier.urihttps://doi.org/10.1108/AEAT-08-2015-0198
dc.identifier.urihttps://hdl.handle.net/20.500.12662/4521
dc.identifier.volume89en_US
dc.identifier.wosWOS:000414979600017en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherEmerald Group Publishing Ltden_US
dc.relation.ispartofAircraft Engineering And Aerospace Technologyen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectFlight controlen_US
dc.subjectModel predictive controlen_US
dc.subjectFixed wing unmanned aerial vehicleen_US
dc.titleDesign of MPCs for a fixed wing UAVen_US
dc.typeArticleen_US

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