DocumentCode :
114465
Title :
Research on a new accurate thrust control strategy for linear induction motor
Author :
Xu Qiwei ; Cui Shumei ; Zhang Qianfan ; Song Liwei ; Xiyuan Li
Author_Institution :
State Key Lab. of Power Transm. Equip. & Syst. Security & New Technol., Chongqing Univ., Chongqing, China
fYear :
2014
fDate :
7-11 July 2014
Firstpage :
1
Lastpage :
5
Abstract :
The linear induction motor is widely used in electromagnetic aircraft launch, convey systems and transportation application, and the thrust control accuracy of linear induction motor is the most important technical factor for stable running. In this paper, the mathematical model of linear induction motor was built, and a new accurate thrust control strategy was proposed, which included adaptive parameters identification and thrust deviation correction. The adaptive parameters identification was designed based on Lyapunov stabilization theory. Then, the thrust deviation correction system was presented based on q-axis component of secondary flux, improving the thrust control accuracy and dynamic response. In the last, the simulation model was built for verifying the proposed thrust control strategy.
Keywords :
Lyapunov methods; electromagnetic launchers; induction motors; linear motors; machine control; mathematical analysis; Lyapunov stabilization theory; adaptive parameters identification; convey systems; dynamic response; electromagnetic aircraft launch; linear induction motor; mathematical model; q-axis component; secondary flux; thrust control accuracy; thrust control strategy; thrust deviation correction system; transportation application; Adaptation models; Control systems; Equations; Inductance; Induction motors; Mathematical model; Parameter estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electromagnetic Launch Technology (EML), 2014 17th International Symposium on
Conference_Location :
La Jolla, CA
Type :
conf
DOI :
10.1109/EML.2014.6920651
Filename :
6920651
Link To Document :
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