摘要
对QT97型自控微型无人驾驶飞机的主要结构、技术性能、控制部分等软硬件结构及性能进行了简要说明,分析了无人机主要组成部分的配置的性能特点,并介绍了如何设计飞行航线和进行远程超视距台控飞行,当飞行航线偏离预定航线时可应用空气动力学原理调整飞行姿态。
In this paper, the author briefly introduced software and hardware structures, such as main structure, technical func- tion and control parts, and function of QT97 auto control micro robot bomb. Then, author analyzed features of allocation function of main component, and introduced how to design airline and control robot bomb. Finally, the author put forward aerodynamic principle adjust flight attitude when airline deviate scheduled routes.
出处
《科技创新与生产力》
2011年第8期79-81,共3页
Sci-tech Innovation and Productivity
关键词
无人飞机
机械结构
技术性能
远程控制
航线
robot bomb
mechanical structure
technical function
remote control
route
