Design and Modeling of a Gas-Electric Hybrid Quad Tilt-Rotor UAV with Morphing Wing


Cetinsoy E.

11th IEEE International Conference on Mechatronics and Automation (ICMA), Tianjin, China, 3 - 06 August 2014, pp.1193-1198 identifier identifier

  • Publication Type: Conference Paper / Full Text
  • Volume:
  • Doi Number: 10.1109/icma.2014.6885868
  • City: Tianjin
  • Country: China
  • Page Numbers: pp.1193-1198

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.