Title :
Research on the reconfigurable technique of SUAV flight control system
Author :
Xin-li, Xu ; Zhen, Jiang ; Bing-xiao, Fan
Author_Institution :
Coll. of Mech. Electr. Eng. & Autom., Shanghai Univ., Shanghai, China
Abstract :
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 apply 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.
Keywords :
aircraft control; micromechanical devices; mobile robots; reconfigurable architectures; reliability; remotely operated vehicles; SUAV flight control system; aircraft integration design; microelectronics technology; micromachine technology; mission effectiveness; reconfigurable technique; small unmanned air vehicle; Adaptation models; Adaptive systems; Aerospace control; Aircraft; Control systems; Fault diagnosis; Military aircraft; SUAV; fault and damage; flight control system; reconfigurable technique;
Conference_Titel :
Computing, Control and Industrial Engineering (CCIE), 2011 IEEE 2nd International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-9599-3
DOI :
10.1109/CCIENG.2011.6008063