DocumentCode :
1714992
Title :
On recognition method of aeroengine working conditions based on flight data
Author :
Qu Jianling ; Li Xiaojuan ; Si Jingguo ; Di Yazhou ; Zhou Yuping
Author_Institution :
Qingdao Branch, Naval Aeronaut. Eng. Inst., Qingdao, China
fYear :
2013
Firstpage :
3565
Lastpage :
3569
Abstract :
According to the complexity of the recognition of aeroengine working conditions and the time-consuming problem of artificial recognition, some intelligent recognition methods based on flight data were proposed in this paper. Four parameters which respectively were throttle position, high-pressure rotor speed, jet nozzle diameter and exhaust gas temperature were selected as sample data according to the working principle of aeroengine, and three multi-class classifications based on the Least Squares Support Vector Classification machine which respectively were One Versus One, One Versus the Rest and Error-Correcting Output Codes were trained and tested. Then the Error-Correcting Output Codes method which had less operation time and high test precision was used to recognize the five kinds of aeroengine working conditions which included stopping, crawling, cruising, biggest and boosting, and the results showed that it had a high recognition accuracy and good adaptability, and was convenient and quick, which laid the foundation for aeroengine condition monitoring and life expectency statistics.
Keywords :
aerospace computing; aerospace engines; condition monitoring; jets; least squares approximations; mechanical engineering computing; nozzles; rotors; support vector machines; aeroengine life expectency statistics; aeroengine working condition recognition method; artificial recognition; condition monitoring; error correcting output codes; exhaust gas temperature; flight data; high-pressure rotor speed; intelligent recognition methods; jet nozzle diameter; least squares support vector classification machine; throttle position; Artificial intelligence; Educational institutions; Electronic mail; Employee welfare; Europe; Silicon; Support vector machines; Error-Correcting Output Codes; Least Squares Support Vector Classification; aeroengine; condition recognition; flight data;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6640039
Link To Document :
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