Proceedings of the 2017 International Conference on Manufacturing Engineering and Intelligent Materials (ICMEIM 2017)

Fault Diagnosis of Aircraft Power Starting System Based on MTBF-SVM

Authors
Liang Qin, Zhen Wang, Xian-Jun Shi
Corresponding Author
Liang Qin
Available Online February 2017.
DOI
10.2991/icmeim-17.2017.98How to use a DOI?
Keywords
SVM, Starting System, Fault Diagnosis
Abstract

In order to solve the fault diagnosis of aircraft power starting system, the fault diagnosis method through constructing binary tree SVM (support vector machines) is researched in this paper. Consider that the components which have high fault rate have priority to be isolated, the method trains the classifier depend on MTBF from small to big and uses the basic structure of binary tree-SVM to generate the leaf nodes gradually, each leaf node represents a fault mode. The method is applied to the identify the common nine fault mode of aircraft power starting system.

Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 2017 International Conference on Manufacturing Engineering and Intelligent Materials (ICMEIM 2017)
Series
Advances in Engineering Research
Publication Date
February 2017
ISBN
10.2991/icmeim-17.2017.98
ISSN
2352-5401
DOI
10.2991/icmeim-17.2017.98How to use a DOI?
Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Liang Qin
AU  - Zhen Wang
AU  - Xian-Jun Shi
PY  - 2017/02
DA  - 2017/02
TI  - Fault Diagnosis of Aircraft Power Starting System Based on MTBF-SVM
BT  - Proceedings of the 2017 International Conference on Manufacturing Engineering and Intelligent Materials (ICMEIM 2017)
PB  - Atlantis Press
SP  - 581
EP  - 584
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmeim-17.2017.98
DO  - 10.2991/icmeim-17.2017.98
ID  - Qin2017/02
ER  -