Aero-engine fault diagnosis applying new fast support vector algorithm
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“Six professional talent summit projects” of Jiangsu Province(07-E-029); Natural Science Foundation of Colleges and Universities in Jiangsu Province(JHZD08-40); “Qing-Lan Project” Foundation of Jiangsu Province(2007).


Aero-engine fault diagnosis applying new fast support vector algorithm
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    摘要:

    A new fast learning algorithm was presented to solve the large-scale support vector machine (SVM) training problem of aero-engine fault diagnosis.The relative boundary vectors (RBVs) instead of all the original training samples were used for the training of the binary SVM fault classifiers.This pruning strategy decreased the number of final training sample significantly and can keep classification accuracy almost invariable.Accordingly,the training time was shortened to 1/20 compared with basic SVM classifier.Meanwhile,owing to the reduction of support vector number,the classification time was also reduced.When sample aliasing existed,the aliasing sample points which were not of the same class were eliminated before the relative boundary vectors were computed.Besides,the samples near the relative boundary vectors were selected for SVM training in order to prevent the loss of some key sample points resulted from aliasing.This can improve classification accuracy effectively.A simulation example to classify 5 classes of combination fault of aero-engine gas path components was finished and the total fault classification accuracy reached 96.1%.Simulation results show that this fast learning algorithm is effective,reliable and easy to be implemented for engineering application.

    Abstract:

    A new fast learning algorithm was presented to solve the large-scale support vector machine (SVM) training problem of aero-engine fault diagnosis.The relative boundary vectors (RBVs) instead of all the original training samples were used for the training of the binary SVM fault classifiers.This pruning strategy decreased the number of final training sample significantly and can keep classification accuracy almost invariable.Accordingly,the training time was shortened to 1/20 compared with basic SVM classifier.Meanwhile,owing to the reduction of support vector number,the classification time was also reduced.When sample aliasing existed,the aliasing sample points which were not of the same class were eliminated before the relative boundary vectors were computed.Besides,the samples near the relative boundary vectors were selected for SVM training in order to prevent the loss of some key sample points resulted from aliasing.This can improve classification accuracy effectively.A simulation example to classify 5 classes of combination fault of aero-engine gas path components was finished and the total fault classification accuracy reached 96.1%.Simulation results show that this fast learning algorithm is effective,reliable and easy to be implemented for engineering application.

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XU Qi-hua, GENG Shuai, SHI Jun. Aero-engine fault diagnosis applying new fast support vector algorithm[J].航空动力学报,2012,27(7):1604~1612. XU Qi-hua, GENG Shuai, SHI Jun. Aero-engine fault diagnosis applying new fast support vector algorithm[J]. Journal Of Aerospace Power,2012,27(7):1604-1612.

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  • 收稿日期:2011-11-28
  • 在线发布日期: 2012-08-03
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