Design and modeling of a gas-electric hybrid quad tilt-rotor UAV with morphing wing

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dc.contributor.authorÇetinsoy, Ertuğrul
dc.date.accessioned2020-11-21T15:56:24Z
dc.date.available2020-11-21T15:56:24Z
dc.date.issued2014en_US
dc.departmentİstanbul Ticaret Üniversitesien_US
dc.description11th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014 -- 3 August 2014 through 6 August 2014 -- Tianjin -- 107410en_US
dc.description.abstractIn this work, a gas-electric hybrid quad tilt-rotor UAV with morphing wing is designed. The mechanical design, propulsion system design and control architecture are explained. Dynamic model of the aerial vehicle is developed including the effects of tilting rotors, variable fuel weight, and morphing wing lift-drag forces and pitching moments. © 2014 IEEE.en_US
dc.identifier.doi10.1109/ICMA.2014.6885868en_US
dc.identifier.endpage1198en_US
dc.identifier.isbn9781480000000
dc.identifier.scopus2-s2.0-84906969192en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage1193en_US
dc.identifier.urihttps://doi.org/10.1109/ICMA.2014.6885868
dc.identifier.urihttps://hdl.handle.net/11467/4130
dc.identifier.wosWOS:000366848100207en_US
dc.identifier.wosqualityN/Aen_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherIEEE Computer Societyen_US
dc.relation.ispartof2014 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014en_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectgas-electric hybriden_US
dc.subjectmorphing wingen_US
dc.subjectQuad tilt-rotor UAVen_US
dc.titleDesign and modeling of a gas-electric hybrid quad tilt-rotor UAV with morphing wingen_US
dc.typeConference Objecten_US

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