Design and Control of a Gas-Electric Hybrid Quad TiltRotor UAV with Morphing Wing

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dc.contributor.authorÇetinsoy, Ertuğrul
dc.date.accessioned2020-11-21T15:56:04Z
dc.date.available2020-11-21T15:56:04Z
dc.date.issued2015en_US
dc.departmentİstanbul Ticaret Üniversitesien_US
dc.descriptionInternational Conference on Unmanned Aircraft Systems (ICUAS) -- JUN 09-12, 2015 -- Denver, COen_US
dc.descriptionWOS:000388438500011en_US
dc.description.abstractIn this work, design and control system development of a gas-electric hybrid quad tilt-rotor UAV with morphing wing are presented. The proposed aircraft has an all carbon-composite body, gas-electric hybrid electric generation system for 3 hours hovering or up to 10 hours of horizontal flight, a novel configuration for VTOL and airplane-like flights with minimized aerodynamic costs and mechanical morphing wings for both low speed and high speed horizontal flights. The mechanical design of the vehicle is performed to achieve a strong and light-weight structure, whereas the aerodynamic and propulsion system designs are aimed for accomplishing both fixed wing and rotary wing aircraft flights with maximized flight endurance. A detailed 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. Control system is designed for both flight regimes and flight simulations are carried out to check the performance of the proposed control system.en_US
dc.identifier.endpage91en_US
dc.identifier.isbn978-1-4799-6010-1
dc.identifier.issn2373-6720
dc.identifier.scopus2-s2.0-84941104562en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage82en_US
dc.identifier.urihttps://hdl.handle.net/11467/4086
dc.identifier.wosWOS:000388438500011en_US
dc.identifier.wosqualityN/Aen_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherIeeeen_US
dc.relation.ispartof2015 International Conference on Unmanned Aircraft Systems (Icuas'15)en_US
dc.relation.ispartofseriesInternational Conference on Unmanned Aircraft Systems
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectQuad tilt-rotor UAVen_US
dc.subjectgaselectric hybriden_US
dc.subjectmorphing wingen_US
dc.subjectdynamic modelen_US
dc.subjectsimulationen_US
dc.titleDesign and Control of a Gas-Electric Hybrid Quad TiltRotor UAV with Morphing Wingen_US
dc.typeConference Objecten_US

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