基于PID控制的X模式四旋翼飞行器研究  

Study on the mode of X quadrotor helicopter based on PID control

作　　者：黄军友[1] 

机构地区：[1]四川信息职业技术学院,四川广元628000

出　　处：《电子设计工程》2014年第2期127-129,共3页Electronic Design Engineering

摘　　要：设计了X模式四旋翼飞行器飞行控制系统的总体方案;在此基础上,完成了飞行控制系统的软硬件设计,包括器件选型、硬件电路设计、系统软件设计,并把互补滤波器应用于姿态解算,姿态控制部分采用PID(Proportional Integral Derivative)控制器。通过仿真验证了器互补滤波和PID控制器算法可行性。The design of the overall scheme of the X mode Quadrotor Helicopter control system; on this basis, the hardware and software of the flight control system design, including the selection, hardware circuit design, software design, and the complementary filter is applied to the attitude calculation, attitude control part adopts PID （Proportional Integral Derivative） controller. Through the simulation for the complementary filter and PID control algorithm feasibility.

关 键 词：四旋翼飞行器 互补滤波器 PID 仿真 

分 类 号：TP212[自动化与计算机技术—检测技术与自动化装置]