现代电子技术Issue(13)：98-100,106,4.
无人直升机非线性鲁棒控制器设计及仿真
Design and simulation of nonlinear robust controller for unmanned helicopter
李之果 1陈亚锋 1高亚瑞2
作者信息
- 1. 中国电子科技集团公司 第二十七研究所，河南 郑州 450047
- 2. 郑州大学 西亚斯国际学院，河南 郑州 450000
- 折叠
摘要
Abstract
According to the design of Torrnambe nonlinear robust controller,the unmanned helicopter nonlinear control sys⁃tem that lateral flight attitude remains disperse was designed based on lateral motion mathematic model of a certain type un⁃manned helicopter. Integral element contained in control system compensates various unknown disturbance inside or outside the system. The decoupling effect between channels is great. Simulation results show that the control method has better disturbance rejection ability compared with PID control.关键词
非线性鲁棒控制/直升机控制系统/鲁棒性/控制器Key words
nonlinear robust control/helicopter control system/robustness/controller分类
信息技术与安全科学引用本文复制引用
李之果,陈亚锋,高亚瑞..无人直升机非线性鲁棒控制器设计及仿真[J].现代电子技术,2015,(13):98-100,106,4.
