A fault tolerant single sided matrix converter for flight control actuation systems

Xiao-yan HUANG; Mao-jing JIN; Jian-cheng ZHANG; Qin-fen LU; You-tong FANG; Andrew GOODMAN; Chris GERADA

doi:10.1631/jzus.C1200164

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A fault tolerant single sided matrix converter for flight control actuation systems

电气工程 | Updated：2022-12-09

- A fault tolerant single sided matrix converter for flight control actuation systems
- A fault tolerant single sided matrix converter for flight control actuation systems
- 信息与电子工程前沿（英文） 2012年13卷第11期页码：866-874
- Affiliations：
  
  1.College of Electrical Engineering, Zhejiang University, Hangzhou 310027, China
  2.High Technology Research and Development Center, Ministry of Science and Technology, Beijing 100044, China
  3.University of Nottingham, Nottingham NG72RD, UK
- Author bio：
  
  [ "Xiao-yan HUANG, E-mail: eezxh@zju.edu.cn" ]
  Qin-fen LU, E-mail: luqinfen@zju.edu.cn
- Funds：
  
  Project supported by the UK government under the DTI CARAD program, the National Natural Science Foundation of China (No.51007078), the National Key Technology Research and Development Program of the Ministry of Science and Technology of China (No.2009BAG12A05), and the National High-Tech R & D (863) Program of China (No. 2011AA11A101)
- DOI：10.1631/jzus.C1200164
  中图分类号： TM46
- 收稿：2012-05-25，
  
  修回：2012-10-12，
  
  纸质出版：2012-11
- Accepted：
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A fault tolerant single sided matrix converter for flight control actuation systems[J]. 信息与电子工程前沿（英文）, 2012,13(11):866-874.

Xiao-yan HUANG, Mao-jing JIN, Jian-cheng ZHANG, et al. A fault tolerant single sided matrix converter for flight control actuation systems[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(11): 866-874.
A fault tolerant single sided matrix converter for flight control actuation systems[J]. 信息与电子工程前沿（英文）, 2012,13(11):866-874. DOI： 10.1631/jzus.C1200164.

Xiao-yan HUANG, Mao-jing JIN, Jian-cheng ZHANG, et al. A fault tolerant single sided matrix converter for flight control actuation systems[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(11): 866-874. DOI： 10.1631/jzus.C1200164.

摘要

Abstract

We describe a single sided matrix converter (SSMC) designed for safety critical applications like flight control actuation systems. Dynamic simulations of multi-phase SSMC using Matlab Simulink are carried out to evaluate the fault tolerance capabilities. Investigation into different numbers of phases and power converter topologies under single phase open circuit

single switch open circuit

and single switch short circuit has been executed. The simulation results confirm 5-phase SSMC design as a compromise between fault tolerance and converter size/volume. A 5-phase SSMC prototype was built. Experimental results verify the effectiveness of our design.

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references

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