Research on the Reconfigurable Technique of SUAV Flight Control System

摘要：

The research on a Small Unmaned Air Vehicle(SUAV) has developed with various kinds of advanced technology, such as micro-machine technology, micro-motor technology, micro-electronics technology, integrated technology, and especially the nanotechnology. As the core of SUAV systems, the reconfigurable technique of flight control system can applie to the unknown fault and damage, and enhance the survivability and mission effectiveness of the aircraft obviously. It has become one of the attractive research subjects in modern aircraft integration design area. In this paper, several important methods for reconfigurable flight control are introduced or analysed, and some focus problems on the reconfigurable flight control technique are summarized and proposed. Finally, an outlook is did about the development tendency of reconfigurable flight control technique.

关键词： SUAV flight control system fault and damage reconfigurable technique

作者: XU Xin-li JIANG Zhen FAN Bing-xiao

作者单位: College of Mechanical Electrical Engineering and Automation,Shanghai University,Shanghai, China Police Fire Brigade,Huangdao District of Qingdao City,Qingdao, China

会议类型: 国际会议

会议名称: 2011 IEEE 2nd International Conference on Computing，Control and Industrial Engineering(CCIE 2011)(第二届计算、控制与工业工程国际会议)

会议地点: 武汉

会议语种:英文

页码: 45-49

在线出版日期: 2011-08-20（万方平台首次上网日期，不代表论文的发表时间）