Design and simulation of a quad rotor tail-sitter unmanned aerial vehicle
Design and simulation of a quad rotor tail-sitter unmanned aerial vehicle
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DOI：
10.1109/sii.2010.5708334
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发表时间：
2010-12
期刊：
影响因子：
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通讯作者：
Atsushi Oosedo;A. Konno;Takaaki Matumoto;Kenta Go;Kouji Masuko;S. Abiko;M. Uchiyama
中科院分区：
文献类型：
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作者：
Atsushi Oosedo;A. Konno;Takaaki Matumoto;Kenta Go;Kouji Masuko;S. Abiko;M. Uchiyama
在本文中，我们介绍了四旋翼尾翼无人机（无人机）的设计和概念。设计的无人机由四旋翼和固定翼组成。它可以像直升机一样盘旋，也可以像固定翼飞机一样巡航。为了验证这一概念，开发了四旋翼尾翼无人机模拟器。仿真结果表明，所提出的无人机比传统的四旋翼直升机型无人机在能源效率方面具有优势。本文还介绍了四旋翼尾翼无人机的研制。
In this paper, we present the design and concept of a quad rotor tail-sitter UAV (unmanned aerial vehicle). The designed UAV is composed of quad rotors and a fixed wing. It can hover like a helicopter, and can cruise like a fixed wing airplane. In order to verify this concept, a simulator of a quad rotor tail-sitter UAV is developed. Simulation results show the advantage in energy efficiency of the proposed UAV over a conventional quad rotor helicopter type UAV. This paper also describes the development of the quad rotor tail-sitter UAV.