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一种小型旋翼无人机平台的设计及飞行验证
引用本文:郭庆,宋笔锋,张炜,张怡哲.一种小型旋翼无人机平台的设计及飞行验证[J].科学技术与工程,2007,7(11):2584-2589.
作者姓名:郭庆  宋笔锋  张炜  张怡哲
作者单位:西北工业大学航空学院,西安,710072
基金项目:西北工业大学航空科技创新基地项目资助
摘    要:研究了具有航拍和图像识别功能的旋翼无人机平台设计及工程实现方法。从直升机总体设计的理论出发,介绍了该旋翼无人机平台的设计及试飞验证过程。提出了总体方案及总体布局。在现有模型直升机的基础上,进行了旋翼与整机的匹配、球形云台的设计、动力系统的选择,及各种传感器的集成等方面的设计,并最终经过外场试飞实验验证设计的可行性。为进一步研究小型无人直升机提供了参考。

关 键 词:小型旋翼无人机  结构设计  集成设计  飞行验证
文章编号:1671-1819(2007)11-2584-06
修稿时间:2007-01-25

Design and Flight Test of A Mini Unmanned Rotorcraft
GUO Qing,SONG Bi-feng,ZHANG Wei,ZHANG Yi-zhe.Design and Flight Test of A Mini Unmanned Rotorcraft[J].Science Technology and Engineering,2007,7(11):2584-2589.
Authors:GUO Qing  SONG Bi-feng  ZHANG Wei  ZHANG Yi-zhe
Abstract:The purpose is to design and develop a mini unmanned rotorcraft with function of Airscape shoting and Target identifying . From the helicopter preliminary design of view. There are 6 parts , and approximately follows the actual design sequence . The progress of this six parts including preliminary design, means the purpose which the plan is used for is given . And conceptual design of taking picture in the sky. How to choose the engine. Solved to the problem that used some of sensor to help the helicopter fly more tranquilization. Testing validated the reliability of this plan, which provided reference for further research of theirs.
Keywords:mini unmanned rotorcraft structure design compositive design flight test
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