Technical Papers
Jun 9, 2020

Novel Extreme Learning Machine Using Kalman Filter for Performance Prediction of Aircraft Engine in Dynamic Behavior

Publication: Journal of Aerospace Engineering
Volume 33, Issue 5

Abstract

In this paper, a novel state-propagation extreme learning machine using a Kalman filter (KF-ELM) is proposed. In comparison with the plain extreme learning machine, the proposed algorithm takes the topological parameters as state variables and minimizes the covariance of state estimates to overcome the state conjunction and transformation dilemma in time series. As a result, its topological stability and prediction accuracy are enhanced, and these merits are further proved theoretically. In addition, the computational effort of KF-ELM is on the same order of magnitude as the plain extreme learning machine, while the former possesses a faster convergent speed. Then, several benchmark datasets are utilized to test the effectiveness and soundness of the proposed algorithm. Finally, it is employed to predict the gas path performance of a turbofan engine. The performance prediction accuracy is better than the plain ELM with different input rules in the dynamic process. Particularly under various flight operation conditions, the proposed algorithm performs well and its stability is sufficiently showcased. In a word, the proposed algorithm provides a candidate technique for predicting aircraft engine performance in dynamic behavior.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

We are grateful for the financial support of the National Nature Science Foundation of China (No. 91960110) and the Fundamental Research Funds for the Central Universities (No. NS2018018). Gratitude is also extended to the China Scholarship Council for supporting the first author to carry out collaborative research in the Department of Mechanical and Industrial Engineering at the University of Toronto.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 33Issue 5September 2020

History

Received: Oct 24, 2018
Accepted: Mar 9, 2020
Published online: Jun 9, 2020
Published in print: Sep 1, 2020
Discussion open until: Nov 9, 2020

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Authors

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Associate Professor, Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author). Email: [email protected]
Assistant Engineer, Control System Institute, Aero Engine Corporation of China, 792 Liangxi Rd., Wuxi, Jiangsu 214063, China. Email: [email protected]
Jinquan Huang [email protected]
Professor, Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China. Email: [email protected]
Xiaojie Qiu [email protected]
Senior Engineer, Control System Institute, Aero Engine Corporation of China, 792 Liangxi Rd., Wuxi, Jiangsu 214063, China. Email: [email protected]
Zhaoguang Wang [email protected]
Senior Engineer, Hunan Power Machinery Research Institute, Aero Engine Corporation of China, Dongjiaduan, Zhuzhou, Hunan 412002, China. Email: [email protected]

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