计算技术与自动化2017，Vol.36Issue(2)：46-50,5.
四旋翼飞行器的自抗扰控制方法研究
Study on Active Disturbance Rejection Control Method for Quadrotor
戴启浩 1马国梁1
作者信息
- 1. 南京理工大学 能源与动力工程学院,江苏 南京 210094
- 折叠
摘要
Abstract
To test whether the ADRC can be applied in quadrotor flight control system.This paper introduces the principle of ADRC and basic components.In view of the quadrotor flying at low speed or hover state,the writer puts forward a method of control system based on ADRC and on the simulation platform for stability control experiments,height control experiments,and analysis of the experiment compared with the PID control system.The simulation results show that: the control system based on ADRC has good dynamic quality,steady precision and strong robustness.The adrc designed in this paper can be used in quadrotor flight control system.关键词
四旋翼飞行器/自抗扰控制/扩张状态观测器/PID控制Key words
quadrotor/ADRC/ESO/PID分类
信息技术与安全科学引用本文复制引用
戴启浩,马国梁..四旋翼飞行器的自抗扰控制方法研究[J].计算技术与自动化,2017,36(2):46-50,5.
