The Flight Control Design of Mini Unmanned Helicopter on Sliding Mode Control

摘要：

Control system of Mini Unmanned Helicopter is a MIMO system, which is serious nonlinear and uncertain. The flight control design of Mini Unmanned Helicopter has always been a difficult problem. This paper introduces sliding mode control on reaching law to the flight control design of Mini Unmanned Helicopter, and it is the better method to solve this kind of problems. To improve control quality, appropriate reaching law is given. For Mini Unmanned Helicopter given input, the simulation results show that this method can realize fast tracks, and eliminate chattering of control input. This method lays the foundation for flight control design in further application.

关键词： Mini Unmanned Helicopter (MUH) Flight Control Design Reaching Law Sliding Mode Control

作者: Xijin Guo Wei Sun Zhenfeng Li Liangcai Ren

作者单位: School of Information and Electrical Engineering, China University of Mining & Technology, Xuzhou 221008

会议类型: 国际会议

会议名称: The 22nd China Control and Decision Conference(2010年中国控制与决策会议)

会议地点: 徐州

会议语种:英文

页码: 3245-3248

在线出版日期: 2010-05-26（万方平台首次上网日期，不代表论文的发表时间）