DocumentCode
3428037
Title
Health diagnosis for aircraft based on the ARMA model
Author
Jianguo, Cui ; Zhang Jie ; Liqiu, Liu ; Yun, Zhao ; Keli, Zhang ; Zhou Guoqiang
Author_Institution
Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China
fYear
2010
fDate
22-24 Oct. 2010
Firstpage
277
Lastpage
280
Abstract
According to the AE (Acoustic Emission, AE) signal that caused by the aircraft structural crack, this paper proposed a health diagnosis approach based on ARMA model and SVM (Support Vector Machine, SVM). Firstly, this method apperceives the healthy information of a real aircraft stabilizer with real time by using AE detecting system. And then, deal with the information collected. Secondly, built an ARMA model and extracting parameter of ARMA model to set up characteristic vector. Finally, design and apply SVM monitor to diagnose the aircraft structure healthy state. Experiments show that the monitor has good performance to recognize and diagnose the fatigue crack of aircraft stabilizer, this approach is proposed to be effective. And it presents a new kind of approach to monitor the health state of aircraft structure and can also be used in other complex system structure health monitoring.
Keywords
aircraft maintenance; autoregressive moving average processes; condition monitoring; fatigue cracks; mechanical engineering computing; structural acoustics; structural engineering; support vector machines; AE detecting system; ARMA model; SVM; acoustic emission signal; aircraft structural crack; fatigue crack; health diagnosis; structural health monitoring; support vector machine; Acoustic emission; Aerospace electronics; Aircraft; Atmospheric modeling; Biological system modeling; NASA; ARMA model; Aircraft; SVM; health diagnosis;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computing and Integrated Systems (ICISS), 2010 International Conference on
Conference_Location
Guilin
Print_ISBN
978-1-4244-6834-8
Type
conf
DOI
10.1109/ICISS.2010.5657166
Filename
5657166
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