DocumentCode
2339005
Title
Fault detection and diagnosis for spacecraft using principal component analysis and support vector machines
Author
Gao, Yu ; Yang, Tianshe ; Xing, Nan ; Xu, Minqiang
Author_Institution
State Key Lab. of Astronaut. Dynamics, Xi´´an Satellite Control Center, Xi´´an, China
fYear
2012
fDate
18-20 July 2012
Firstpage
1984
Lastpage
1988
Abstract
Development of intelligent fault detection and diagnosis technologies for spacecraft is one of important issues in the space engineering. In this paper, we present a new fault detection and diagnosis approach for spacecraft based on Principal Component Analysis (PCA) and Support Vector Machines (SVM). Firstly, PCA is used to extract features from input data and reduce the input data to low dimensional feature vectors. Then the method use a binary SVM to detect whether there is a fault or not. If the fault is detected, a multi-class SVM is used to identify fault type. The experimental results show that the method is efficient and practical for fault detection and diagnosis of spacecraft system.
Keywords
aerospace computing; fault diagnosis; feature extraction; knowledge based systems; principal component analysis; space vehicles; support vector machines; PCA; binary SVM; fault type identification; feature extraction; intelligent fault detection; intelligent fault diagnosis; low dimensional feature vector; multiclass SVM; principal component analysis; space engineering; spacecraft system; support vector machine; Fault detection; Fault diagnosis; Feature extraction; Principal component analysis; Space vehicles; Support vector machines; Telemetry; fault detection; fault diagnosis; principal component analysis (PCA); spacecraft; support vector machine (SVM);
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications (ICIEA), 2012 7th IEEE Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4577-2118-2
Type
conf
DOI
10.1109/ICIEA.2012.6361054
Filename
6361054
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