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 :
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