Design of MPCs for a fixed wing UAV

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dc.authoridBaykara, Cemal/0000-0002-3797-6563
dc.contributor.authorUlker, Hakan
dc.contributor.authorBaykara, Cemal
dc.contributor.authorOzsoy, Can
dc.date.accessioned2024-12-24T19:28:31Z
dc.date.available2024-12-24T19:28:31Z
dc.date.issued2017
dc.departmentSiirt Üniversitesi
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.
dc.identifier.doi10.1108/AEAT-08-2015-0198
dc.identifier.endpage901
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.issue6
dc.identifier.scopus2-s2.0-85033462532
dc.identifier.scopusqualityQ2
dc.identifier.startpage893
dc.identifier.urihttps://doi.org/10.1108/AEAT-08-2015-0198
dc.identifier.urihttps://hdl.handle.net/20.500.12604/7099
dc.identifier.volume89
dc.identifier.wosWOS:000414979600017
dc.identifier.wosqualityQ3
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherEmerald Group Publishing Ltd
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241222
dc.subjectFlight control
dc.subjectModel predictive control
dc.subjectFixed wing unmanned aerial vehicle
dc.titleDesign of MPCs for a fixed wing UAV
dc.typeArticle

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