SLIDING MODE CONTROL WITH FUZZY BOUNDARY LAYER TO AIR-AIR MISSILE

摘要：

In this paper, we will consider designing the autopilot of an air to air missile using sliding mode control (SMC) based on fuzzy variable boundary layer.In sliding mode method, all systems states are guided toward a sliding surface through exerting a non-continuous control force on the dynamic system.This force and repeated switching produce chattering.To overcome this problem.Fuzzy control is applied to determine the boundary layer thickness.Therefore, the system is robust under various uncertainties and external disturbances.

关键词： Siding mode control Autopilot Chattering Boundary layer Fuzzy control

作者: NEGAR FXMI SADR ATA FAKHRI

作者单位: Faculty of Electrical Engineering,Tarbiat Modares University ,Tehran,Iran Faculty of Electrical Engineering,Islamic Azad University,Oskou Branch,Iran

会议类型: 国际会议

会议名称: 3rd International Conference on Mechanical and Electrical Technology(ICMET2011) (2011第三届机械与电气技术国际会议)

会议地点: 大连

会议语种:英文

页码: 183-187

在线出版日期: 2011-08-26（万方平台首次上网日期，不代表论文的发表时间）