Liu Jiarun, Shen Gongzhang. Attitude control based on inverse dynamics and online parameter identification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(02): 111-115. (in Chinese)
Citation: CAO Huiling, GAO Sheng, XUE Penget al. Aeroengine fault diagnosis based on multi-classification AdaBoost[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(9): 1818-1825. doi: 10.13700/j.bh.1001-5965.2017.0774(in Chinese)

Aeroengine fault diagnosis based on multi-classification AdaBoost

doi: 10.13700/j.bh.1001-5965.2017.0774
Funds:

the Fundamental Research Funds for the Central Universities 3122014D010

More Information
  • Corresponding author: CAO Huiling, E-mail:hlcao@cauc.edu.cn
  • Received Date: 13 Dec 2017
  • Accepted Date: 09 Mar 2018
  • Publish Date: 20 Sep 2018
  • The data mining of aeroengine operational data is an important research for engine fault diagnosis. Due to the limitations of various algorithms, the accuracy of fault classification is difficult to be greatly enhanced with a single algorithm. Using a combination of classifications and diagnosis of multiple classification models, AdaBoost algorithm is a good method to improve the fault recognition accuracy. This paper combined the AdaBoost algorithm and its improved algorithm, and established a multi-classification AdaBoost algorithm. Support vector machine (SVM) was taken as the basic classifier, and a comprehensive diagnostic model was established. Fault identification data in statistics of fingerprint maps were processed with unit vector, ratio coefficient and correlation coefficient, and the training data for fault diagnosis with few effects of fault degrees were obtained. Then the model was constructed. The experimental results illustrate that the AdaBoost based combination algorithm can significantly improve the performance of classifier. With the actual fault cases, it is verified that the established diagnostic model can be well applied to engine fault diagnosis.

     

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