DocumentCode
3131621
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
Volume
2
fYear
2011
fDate
20-21 Aug. 2011
Firstpage
45
Lastpage
49
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Computing, Control and Industrial Engineering (CCIE), 2011 IEEE 2nd International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-9599-3
Type
conf
DOI
10.1109/CCIENG.2011.6008063
Filename
6008063
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