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
Link To Document :
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