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

Author

Wang, Yong ; Guan, Miao ; Li, Chunlong

Author_Institution

Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China

fYear

2009

fDate

25-27 May 2009

Firstpage

2897

Lastpage

2901

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.

Keywords

active filters; avionics; power filters; stability; apparent power 6 kVA; digital simulation; dynamic performance; one-cycle control; space vector analysis; stability conditions; stability performance; three-phase aeronautical active power filter; Active filters; Aerodynamics; Digital simulation; Functional analysis; Mathematical model; Mathematics; Performance analysis; Signal analysis; Signal resolution; Stability; aeronautical active power filter; dynamic performance; one-cycle control; simply space vector;

fLanguage

English

Publisher

ieee

Conference_Titel

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

Conference_Location

Xi´an

Print_ISBN

978-1-4244-2799-4

Electronic_ISBN

978-1-4244-2800-7

Type

conf

DOI

10.1109/ICIEA.2009.5138739

Filename

5138739