DocumentCode
3546906
Title
Simulation analysis of three-phase bridge rectifier circuit of aviation device
Author
Jin Changjiang ; Liu Ling ; Tang Bin ; Kesong, Chen
Author_Institution
Innovation Base of Sch.-Enterprise Cooperation in Aviation Electron. Technol. in Sichuan, Chengdu, China
Volume
2
fYear
2013
fDate
15-17 Nov. 2013
Firstpage
407
Lastpage
409
Abstract
In recent years, with the upgrading of airborne device, most power source circuit of airborne devices use single-phase bridge and three-phase bridge uncontrolled rectifying circuit. Nonlinear characteristics of the rectifier circuit bring serious harmonic interference to the AC power system of the aircraft. This paper simulate and analyses the three-phase bridge circuit of airborne device power source with the help of Matlab, in order to help the governance of the aircraft AC power system harmonic.
Keywords
aircraft power systems; power system harmonics; rectifying circuits; Matlab; airborne device; aircraft AC power system harmonic; aviation device; harmonic interference; nonlinear characteristics; power source circuit; three-phase bridge rectifier circuit; uncontrolled rectifying circuit; Aircraft; Analytical models; Bridge circuits; Integrated circuit modeling; Power harmonic filters; Power supplies; Rectifiers;
fLanguage
English
Publisher
ieee
Conference_Titel
Communications, Circuits and Systems (ICCCAS), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-3050-0
Type
conf
DOI
10.1109/ICCCAS.2013.6765368
Filename
6765368
Link To Document