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Mathematical modeling and vertical flight control of a tilt-wing UAV

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dc.contributor.authorOner, Kaan Taha
dc.contributor.authorCetinsoy, Ertugrul
dc.contributor.authorSirimoglu, Efe
dc.contributor.authorHancer, Cevdet
dc.contributor.authorUnel, Mustafa
dc.contributor.authorAksit, Mahmut Faruk
dc.contributor.authorGulez, Kayhan
dc.contributor.authorKandemir, Ilyas
dc.date.accessioned2026-06-27T13:18:23Z
dc.date.issued2012
dc.description.abstractThis paper presents a mathematical model and vertical flight control algorithms for a new tilt-wing unmanned aerial vehicle (UAV). The vehicle is capable of vertical take-off and landing (VTOL). Due to its tilt-wing structure, it can also fly horizontally. The mathematical model of the vehicle is obtained using Newton-Euler formulation. A gravity compensated PID controller is designed for altitude control, and three PID controllers are designed for attitude stabilization of the vehicle. Performances of these controllers are found to be quite satisfactory as demonstrated by indoor and outdoor flight experiments.en
dc.description.sponsorshipTUBITAK [107M179]
dc.description.urihttps://doi.org/10.3906/elk-1007-624
dc.identifier.doi10.3906/elk-1007-624
dc.identifier.eissn1303-6203
dc.identifier.endpage157
dc.identifier.issn1300-0632
dc.identifier.issue1
dc.identifier.startpage149
dc.identifier.urihttps://hdl.handle.net/20.500.14981/51708
dc.identifier.volume20
dc.identifier.wos000300137900012
dc.language.isoeng
dc.publisherTubitak Scientific & Technological Research Council Turkey
dc.relation.ispartofTURKISH JOURNAL OF ELECTRICAL ENGINEERING AND COMPUTER SCIENCES
dc.rightsopenAccess
dc.subjectTilt-wing
dc.subjectquadrotor
dc.subjectPID
dc.subjectVTOL
dc.subjecthover
dc.subjectComputer Science
dc.subjectEngineering
dc.titleMathematical modeling and vertical flight control of a tilt-wing UAV
dc.typeArticle
dspace.entity.typePublication
local.import.sourceWOS

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