DocumentCode :
2553780
Title :
Early fault self-recovery model and fault self-recovery methods on aircraft
Author :
Zhongsheng, Wang ; Ming, Li
Author_Institution :
Coll. of Aeronaut., Northwestern Polytech. Univ., Xian
fYear :
2008
fDate :
2-4 July 2008
Firstpage :
487
Lastpage :
489
Abstract :
In order to increase the safety of aircraft and its the reliability, the early fault self-recovery model of aircraft is established and the early fault self-recovery methods are presented. They are based on the early fault mechanisms analysis of the aircraft and the early fault characteristics of the aircraft are used. In this paper, the smart structure, the fault compensation, the system reconstruction, the function reconfiguration, the mechanism regeneration and the autonomic repair are put forward and they are analyzed. At the same time, the basic structure of fault self-recovery system was given, key technologies are studied, implementation way is analyzed and examples on the fault self-recovery are introduced, too. It provides a new technology way to develop modern aircraft that has high performance, long life, few maintenance and low cost, and has important value in the theory and application.
Keywords :
aircraft; fault tolerance; maintenance engineering; aircraft; autonomic repair; early fault self-recovery methods; fault compensation; function reconfiguration; mechanism regeneration; smart structure; system reconstruction; Aerospace safety; Air safety; Aircraft; Costs; Educational institutions; Electronic mail; Fault detection; Intelligent structures; Noise reduction; Stress; Aircraft; Early Fault; Fault Self-recovery Methods; Fault Self-recovery Model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference, 2008. CCDC 2008. Chinese
Conference_Location :
Yantai, Shandong
Print_ISBN :
978-1-4244-1733-9
Electronic_ISBN :
978-1-4244-1734-6
Type :
conf
DOI :
10.1109/CCDC.2008.4597358
Filename :
4597358
Link To Document :
بازگشت