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一种小型无人机简易飞行控制系统的方案
引用本文:陈坚,郑忠培.一种小型无人机简易飞行控制系统的方案[J].实验流体力学,2006,20(4):99-105.
作者姓名:陈坚  郑忠培
作者单位:1. 重庆大学自动化学院,重庆,400030;中国空气动力研究与发展中心,绵阳,621000
2. 中国空气动力研究与发展中心,绵阳,621000
摘    要:针对低速、自然稳定的小型无人机的特点,以控制无人机按预定航线自主飞行为目标,设计了具有双回路的PID控制的纵横向飞行控制律,以及优化的GPS系统(磁航向传感器补偿)导航算法,形成只需少量传感器和执行机构的飞行控制方案。该方案广泛适用于低速、自然稳定的小型无人机,具有良好的静态和动态特性,并且造价低廉、使用简单。

关 键 词:无人机  自动驾驶仪  导航  飞行控制
文章编号:1672-9897(2006)04-0099-07
收稿时间:2006-04-27
修稿时间:2006-04-272006-10-12

A design of the small-scaled UAV's simple flight control system
CHEN Jian,ZHENG Zhong-pei.A design of the small-scaled UAV''''s simple flight control system[J].Experiments and Measur in Fluid Mechanics,2006,20(4):99-105.
Authors:CHEN Jian  ZHENG Zhong-pei
Abstract:In this article,a simple flight control system is designed.It adapts to the unmanned aerial vehicle(UAV)which flies at a low speed,is small scaled and has nature stability.The system is to be used to control the UAV to fly on the presumptive route.In the process of designing,the two negative feedback loops with PID controller,and the navigation methodology based on the GPS with the compensation of the magnetic compass are built up.Just a few sensors and servos are required by this flight control system.The system is widely applicable to the low-speed/small-scaled/nature-stability UAVs.It has good static and kinetic qualities.It is cheap and can be operated simply.
Keywords:unmanned aerial vehicle  automatic pilot  navigation  flight control
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