舰船电子工程2017，Vol.37Issue(4)：1-4,17,5.DOI:10.3969/j.issn.1672-9730.2017.04.001
多旋翼式无人飞行器系统设计研究
Design of Multiple Rotor Unmanned Aerial Vehicle System
程荣涛 1马恒 2王荣颖 2范松伟2
作者信息
- 1. 海军驻武汉四三八厂军事代表室 武汉 430060
- 2. 海军工程大学导航工程系 武汉 430033
- 折叠
摘要
Abstract
Comparing with other unmanned aerial vehicles, multiple rotor unmanned aerial vehicles have the advantages that it has the ability of vertical take-off and landing and can be controlled easily, thus having great application prospect in military tasks.As a result, this paper designs a system of multiple rotor unmanned aerial vehicle.At first, the design indicators of rotor unmanned spacecraft are presented in this paper.Then according to the design index, the overall design of multiple rotor unmanned aircraft system is carried out.Finally through the simulation experiment and the prototype flight test, the feasibility of the designed system is verified.关键词
多旋翼式无人飞行器/设计指标/系统设计/飞行试验Key words
multiple rotor unmanned aerial vehicles/design indicators/system design/flight test Class Number分类
航空航天引用本文复制引用
程荣涛,马恒,王荣颖,范松伟..多旋翼式无人飞行器系统设计研究[J].舰船电子工程,2017,37(4):1-4,17,5.
