DocumentCode
1792139
Title
Design and modeling of a gas-electric hybrid quad tilt-rotor UAV with morphing wing
Author
Cetinsoy, Ertugrul
Author_Institution
Fac. of Eng. & Design, Istanbul Commerce Univ., Istanbul, Turkey
fYear
2014
fDate
3-6 Aug. 2014
Firstpage
1193
Lastpage
1198
Abstract
In 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.
Keywords
aerospace components; aerospace propulsion; autonomous aerial vehicles; design engineering; hybrid electric vehicles; rotors (mechanical); vehicle dynamics; aerial vehicle dynamic model; control architecture; gas-electric hybrid quad tilt-rotor UAV; mechanical design; morphing wing; pitching moment; propulsion system design; tilting rotors; unmanned aerial vehicle; variable fuel weight; wing lift-drag force; Aerodynamics; Aircraft; Batteries; Control systems; Rotors; Vehicle dynamics; Vehicles; Quad tilt-rotor UAV; gas-electric hybrid; morphing wing;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2014 IEEE International Conference on
Conference_Location
Tianjin
Print_ISBN
978-1-4799-3978-7
Type
conf
DOI
10.1109/ICMA.2014.6885868
Filename
6885868
Link To Document