DocumentCode
2704916
Title
Deicing system based on fault-tolerance control for aircraft
Author
Tao, Jun ; XU, Huibin ; Tao, Jianwu
Author_Institution
Dept. of Control Eng., Aviation Univ., Jilin
fYear
2008
fDate
21-24 April 2008
Firstpage
1
Lastpage
4
Abstract
An energy-saving fault-tolerance control deicing system for aircraft is proposed in this paper. In the deicing system, we used the separation deicing method and optimal energy-control method to save deicing energy markedly, adopted the fault-tolerance system structure to improve the reliability of it noticeably. The results of the experiment have shown that the reliability of this system is high and its energy-saving effect is remarkable.
Keywords
aircraft control; fault tolerance; optimal control; power control; aircraft control; aircraft deicing system; energy saving fault tolerance control; fault tolerance system structure; optimal energy control; separation deicing method; Aerospace control; Aircraft propulsion; Automatic control; Control systems; Fault tolerant systems; Frequency; Ice surface; Pulse measurements; Strips; Voltage; Deicing system; Energy-saving Technique; Fault-tolerance Control;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Technology, 2008. ICIT 2008. IEEE International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-1705-6
Electronic_ISBN
978-1-4244-1706-3
Type
conf
DOI
10.1109/ICIT.2008.4608402
Filename
4608402
Link To Document