Study on stability and dynamic performance of three-phase aeronautical active power filter based on one-cycle control under simply space vector

  • Yong Wang*
  • , Miao Guan
  • , Chunlong Li
  • *Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The principle of three-phase aeronautical active power filter based on one-cycle control under simply space vector is analyzed. The mathematic model of three-phase aeronautical active power filter is established. Stability conditions of three-phase aeronautical active power filter based on one-cycle control under simply space vector are derived. Dynamic performance under big signal disturb is analyzed, and the resolvent is proposed. The modeling and digital simulation of three-phase aeronautical active power filter are implemented with Saber, and the experiments of 6 kVA three-phase aeronautical active power filter are carried out. The simulative and experimental results verify the theoretic analysis.

Original languageEnglish
Title of host publication2009 4th IEEE Conference on Industrial Electronics and Applications, ICIEA 2009
Pages2897-2901
Number of pages5
DOIs
StatePublished - 2009
Event2009 4th IEEE Conference on Industrial Electronics and Applications, ICIEA 2009 - Xi'an, China
Duration: 25 May 200927 May 2009

Publication series

Name2009 4th IEEE Conference on Industrial Electronics and Applications, ICIEA 2009

Conference

Conference2009 4th IEEE Conference on Industrial Electronics and Applications, ICIEA 2009
Country/TerritoryChina
CityXi'an
Period25/05/0927/05/09

Keywords

  • Aeronautical active power filter
  • Dynamic performance
  • One-cycle control
  • Simply space vector

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