Title :
Research on the fault diagnosis of flight control system
Author :
Xu Xin-li ; Jiang Zhen ; Fan Bing-Xiao
Author_Institution :
Coll. of Mech. Electr. Eng. & Autom., Shanghai Univ., Shanghai, China
Abstract :
As the core of aircraft, the state of flight control system can impact the survivability and mission effectiveness of the aircraft obviously. The fault diagnosis of flight control system when it breaks down can provide some essential information for subsequent reconfigurable control, which can guarantee the system stability. In this paper, the history and current state of fault diagnosis methods about flight control system are introduced, and then some important methods for fault diagnosis are analysed. Some focus problems on fault diagnosis are also summarized. Finally, an outlook is did for the development tendency of fault diagnosis about flight control system.
Keywords :
aircraft control; stability; aircraft; fault diagnosis; flight control system; subsequent reconfigurable control; system stability; Aerospace control; Artificial intelligence; Fault detection; Fault diagnosis; Mathematical model; Signal processing; State estimation; fault and damage; fault diagnosis; flight control system; reconfigurable control;
Conference_Titel :
Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
Conference_Location :
Jilin
Print_ISBN :
978-1-61284-719-1
DOI :
10.1109/MEC.2011.6025739