期刊文献+

基于T型APF的三相整流器及其控制策略 被引量:3

T-Type APF Based Rectifier and Its Control Strategies
下载PDF
导出
摘要 提出一种基于T型有源滤波器(APF)的三相整流器拓扑结构,给出了系统主电路参数设计方法,建立了T型APF的数学模型,设计了两种控制策略并进行了比较研究,即仅采用系统电流反馈控制策略和系统电流反馈控制与负载电流前馈控制相结合的控制策略。采用PSCAD/EMTDC对两种控制策略进行了仿真分析,并进行了实验验证。仿真和实验结果的一致性表明,本文提出的拓扑结构是可行的,提出的控制策略是有效的。 A novel three-phase rectifier topology based on T-type active power filter (APF) is proposed. The design method of main circuit parameters is also given. The mathematical model of the T-type active power filter is deduced, and two control strategies, namely, source-side current feedback control strategy and source-side current feedback plus load current feed-forward control strategy are devised and compared. The proposed system is studied by digital simulation using PSCAD/EMTDC software and by experiments. The simulation and experimental results are consistent, which demonstrates the feasibility of the proposed topology and the effectiveness of the devised control strategies.
出处 《电工技术学报》 EI CSCD 北大核心 2009年第1期120-126,共7页 Transactions of China Electrotechnical Society
关键词 有源滤波器 谐波污染 PWM控制 功率因数矫正 Active power filter (APF), harmonic contamination, PWM control, power factor correction (PFC)
  • 相关文献

参考文献12

二级参考文献58

共引文献153

同被引文献53

  • 1王永,沈颂华.空间矢量和单周控制三相航空有源电力滤波器[J].北京航空航天大学学报,2007,33(1):90-93. 被引量:5
  • 2严仰光,龚春英,王慧贞,等.多电飞机和电气科[J].电源技术学报,2007,5(1):1-4.
  • 3Rosero J A,Ortega J A,E. Aldabas E, et al. Moving towards a more electric aircraft[J]. IEEE Aerospace and Electronic Systems Magazine,2007,22(3):3-9.
  • 4Emadi A, Ehsani M. Aircraft power systems.. technology,state of the art,and future trends[J]. IEEE Aerospace and Electronic Systems Magazine, 2000, 15(1) ,28-32.
  • 5Chang J,Wang A. New VF-power system architecture and evaluation for future aircraft [J]. IEEE Transactions on Aerospace and Electronic Systems, 2006,42(2):527-539.
  • 6RTCA. DO- 160D Environmental conditions and test procedures for airborne equipment [S]. Washington, USA:RTCA,Inc. ,1997.
  • 7RTCA. DO- 160F Environmental conditions and test procedures for airborne equipment [S]. Washington, USA .. RTCA, Inc. , 2007.
  • 8ISO. ISO 1540:2006(E) Aerospace: characteristics of aircraft electrical systems[S]. [S. l. ]. ISO, 2006.
  • 9Department of Defense. MIL-STD-704F Aircraft electric power characteristics[S]. USA: Department of Defense, 2004.
  • 10Clark T, Chivite-Zabalza F J, Forsyth A J, et al. Analysis and comparison of diode rectifier units suitable for aerospace applications[C]//Proceedings of the 2008 4th IET Conference on Power Electronics, Machines and Drives, April 2-4, 2008, York, England. Piscataway.. IEEE Press, 2008: 602-606.

引证文献3

二级引证文献16

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部