Design and flight tests of a holonomic quadrotor UAV with sub-rotor control surfaces

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dc.contributor.authorÇetinsoy, Ertuğrul
dc.date.accessioned2020-11-21T15:56:22Z
dc.date.available2020-11-21T15:56:22Z
dc.date.issued2013en_US
dc.departmentİstanbul Ticaret Üniversitesien_US
dc.description2013 10th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013 -- 4 August 2013 through 7 August 2013 -- Takamastu -- 100781en_US
dc.description.abstractIn this work, a quadrotor helicopter UAV with sub-rotor control surfaces for non-inclined horizontal motion is designed. Dynamic model of the air vehicle and an eight output PID control system is designed for controlling both the rotor speeds and control surface angles. The performance of this control system on the air vehicle is presented through simulation results with severe wind conditions and initial flight test results acquired from the prototype. © 2013 IEEE.en_US
dc.identifier.doi10.1109/ICMA.2013.6618084en_US
dc.identifier.endpage1202en_US
dc.identifier.isbn9781470000000
dc.identifier.scopus2-s2.0-84887855989en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage1197en_US
dc.identifier.urihttps://doi.org/10.1109/ICMA.2013.6618084
dc.identifier.urihttps://hdl.handle.net/11467/4126
dc.identifier.wosWOS:000335375900201en_US
dc.identifier.wosqualityN/Aen_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.relation.ispartof2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013en_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleDesign and flight tests of a holonomic quadrotor UAV with sub-rotor control surfacesen_US
dc.typeConference Objecten_US

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