Çetinsoy, Ertuğrul2020-11-212020-11-2120149781480000000https://doi.org/10.1109/ICMA.2014.6885868https://hdl.handle.net/11467/413011th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014 -- 3 August 2014 through 6 August 2014 -- Tianjin -- 107410In 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.eninfo:eu-repo/semantics/closedAccessgas-electric hybridmorphing wingQuad tilt-rotor UAVConference Object11931198N/AWOS:000366848100207N/A2-s2.0-8490696919210.1109/ICMA.2014.6885868