DocumentCode
2496636
Title
Identification model of aeroengine based on improved LS-SVM
Author
Cai, Kailong ; Yao, Wuwen ; Lv, Boping
Author_Institution
First Aeronaut. Inst. of the Air Force, Xinyang
fYear
2008
fDate
25-27 June 2008
Firstpage
7368
Lastpage
7373
Abstract
Because of aeroengine properties such as the strong nonlinearity and time-varying uncertainty, a new identification algorithm of aeroengine model based on improved LS-SVM was brought forward. In the method, LS-SVM robustness was improved by adding weighed values to errors and its sparseness was improved by clipping algorithm. In terms of the recorded flight data on some turbofan engine, improved LS-SVM identification model of aeroengine was set up. Through the identification of the recorded flight data, the results show that the improved LS-SVM identification model has the advantages of high identification precision, good self-adaptability and strong robustness. It is effective that the improved LS-SVM identification model is used in aeroengine.
Keywords
aerospace computing; jet engines; support vector machines; LS-SVM robustness; aeroengine identification model; aeroengine nonlinearity; clipping algorithm; time-varying uncertainty; turbofan engine; Automation; Electronic mail; Engines; Intelligent control; Lagrangian functions; Least squares methods; Nonlinear systems; Robustness; Support vector machines; Uncertainty; Aeroengine; Identification Model; Improved LS-SVM; Nonlinear System;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on
Conference_Location
Chongqing
Print_ISBN
978-1-4244-2113-8
Electronic_ISBN
978-1-4244-2114-5
Type
conf
DOI
10.1109/WCICA.2008.4594065
Filename
4594065
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