Model Reference Sliding Mode Controller Design for Reconfigurable Flight Control

摘要：

Based on the model reference control, a sliding mode controller is proposed for the reconfigurable flight control system in this paper. Using this controller, the controlled plant can track the reference model precisely. It is shown that this method provides better performance for the flight control system. Firstly, a Proportional-Integral type sliding surface is designed through Linear- Quadratic Regulator method to make the sliding mode have good dynamic characteristics and to eliminate the steady state error. Secondly, the simple saturating control is adopted to avoid the chattering phenomena. The simulation results show that the flight control system with this controller not only doesnt require the procedure of fault detection and isolation, but also achieves the model tracking control.

关键词： reconfigurable flight control model reference sliding mode control

作者: YANG Zhijun QI Xiaohui SHAN Ganlin HE Wei

作者单位: Department of Optics and Electronics Engineering, Mechanical Engineering College,Shijiazhuang 050003 Hebei University of Science and Technology, Shijiazhuang 050003, China

会议类型: 国际会议

会议名称: 第七届国际测试技术研讨会

会议地点: 北京

会议语种:英文

在线出版日期: 2007-08-05（万方平台首次上网日期，不代表论文的发表时间）