DocumentCode :
1794805
Title :
Steering system fault tolerance simulation of PMSM control
Author :
Xiaojie Zang ; Feng Qi
Author_Institution :
Electr. Eng. Dept., Civil aviation Univ. of China, Tianjin, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
200
Lastpage :
205
Abstract :
Civil aircraft Steering system is one of the core systems. PMSM is widely used in Steering systems because of their superior performance. When the motor fails, the magnetic field will become asymmetric. The original dq model no longer applies to motor failure. This paper presents a fault-tolerant systems based on the three-phase decoupling control scheme for PMSM, through the three-phase motor model does not decouple further improvement, the use of extracted neutral wire greatly enhances the three-phase permanent synchronous motor fault tolerance to failure in the broken phase state of emergency still have some work to ensure the operating characteristics of steering system.
Keywords :
aircraft control; failure analysis; machine control; permanent magnet motors; steering systems; synchronous motors; PMSM control; broken phase state of emergency; civil aircraft steering system; core system; fault-tolerant system; magnetic field; motor failure; operating characteristics; steering system fault tolerance simulation; three-phase decoupling control scheme; three-phase motor model; three-phase permanent synchronous motor fault tolerance; Conferences; Navigation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007235
Filename :
7007235
Link To Document :
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