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

被引：0
|
作者：
Cetinsoy, Ertugrul [1 ]
机构：
[1] Istanbul Commerce Univ, Fac Engn & Design, TR-34840 Istanbul, Turkey
来源：
2014 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION (IEEE ICMA 2014) | 2014年
关键词：
Quad tilt-rotor UAV; gas-electric hybrid; morphing wing; CONVERTIBLE MAV; FLIGHT CONTROL;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
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.
引用
收藏
页码：1193 / 1198
页数：6
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