Reconfigurable Flight Control Law Based on Adaptive Model Following Scheme

摘要：

The design of Reconfigurable control law is one of focus problem in flight control field, its performance affects directly the systems safety and survivability. A method of reconfigurable flight control law based on adaptive model following is proposed with an asymptotic model following condition in this paper. The method can make the outputs of failure system exactingly tracking those of reference model by detecting the location and amplitude of failure of actuator failure, modifying control parameter, and redesigning control law on-line to counteract dynamics caused by actuators failure. The simulation example shows that this method is valid.

关键词： reconfigurable flight control model following adaptive control

作者: QI Xiao-hui YANG Zhi-jun WU Xiao-bei

作者单位: Department of Optical and Electronic Engineering, Mechanical Engineering Collage,Shijiazhuang 050003 Department of Optical and Electronic Engineering, Mechanical Engineering Collage,Shijiazhuang 050003 Department of Automation, Nanjing University of Science and Technology, Nanjing, 210094, 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）