航空学报 > 2009, Vol. 30 Issue (8): 1490-1496

四相永磁容错电机的SVPWM控制

任元1,2,孙玉坤2,朱纪洪3   

  1. 1.北京航空航天大学 仪器科学与光电工程学院 2.江苏大学 电气信息工程学院 3.清华大学 计算机科学与技术系
  • 收稿日期:2008-06-15 修回日期:2008-11-06 出版日期:2009-08-25 发布日期:2009-08-25
  • 通讯作者: 任元

SVPWM Control of Four-phase Faulttolerant Permanent Magnet Motor for Aircraft

Ren Yuan1,2, Sun Yukun2, Zhu Jihong3   

  1. 1.School of Instrument Science and Optoelectronics Engineering, Beijing University of Aeronautics and Astronautics 2.School of Electrical and Information Engineering, Jiangsu University 3.Department of Computer Science and Technology, Tsinghua University
  • Received:2008-06-15 Revised:2008-11-06 Online:2009-08-25 Published:2009-08-25
  • Contact: Ren Yuan

摘要: 为了提高四相永磁容错电机(FTPMM)在系统正常工作时的控制性能,在分析其结构和原理的基础上,建立了其在旋转坐标系下的数学模型,为实现电流、磁链、转矩的解耦控制创造了条件,设计了基于H桥的容错驱动,提出了一种新颖的四相永磁容错电机的电压空间矢量脉宽调制(SVPWM)策略,并巧妙设计了零矢量的插入顺序和重合矢量的选择顺序,方便了数字信号处理器(DSP)的实现。仿真和试验结果证明了在系统正常工作时该方法的正确性和优越性。

关键词: 容错, 永磁, 电机, 坐标变换, 电压空间矢量, 解耦控制

Abstract: In order to enhance the performance of the four-phase faulttolerant permanent magnet motor (FTPMM) in normal conditions, a study is first made of the structure and principle of the fourphase FTPMM, and its mathematical model is presented to decouple its current, stator flux and torque. Then a novel voltage space vector pulse width modulation (SVPWM) method for the fourphase FTPMM driven by H bridges is proposed, and the insertion sequence of the zero vectors as well as the performance sequence of the coincidencesector is designed to facilitate its digital signal processor (DSP) implementation. To verify the effectiveness of the control strategy in normal conditions, some simulations and experiments are developed and the results show satisfactory static and dynamic performance of the system.

Key words: fault tolerance, permanent magnets, motors, coordinates transformation, voltage space vector, decoupling control

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