DocumentCode :
2099677
Title :
Study of high power factor rectifiers based on one cycle control in aircraft electric power system
Author :
Lei, Tao ; Zhang, Xiao-bin ; Dong, Yan-Jun ; Zhao, Jing-Hui ; Lin, Hui
Author_Institution :
Sch. of Autom., Northwestern Polytech. Univ., Xi´´an
fYear :
2008
fDate :
12-15 March 2008
Firstpage :
325
Lastpage :
329
Abstract :
The object of this paper is to present further study of three-phase rectifiers based on one-cycle control in aircraft electric power system. The fundamental vector principle of one cycle control is introduced and analyzed briefly. The Simulated model of three-phase Rectifiers based on one-cycle control is build by software Saber. The 4 kW prototype of three-phase rectifiers based on the one-cycle control is presented. An investigation of steady and dynamic performance for three-phase PFC system has been carried out in aircraft electric power system conditions. The result of simulation and experiments demonstrate that one-cycle controller features excellent performance, simple circuitry, and low cost control methods for three-phase rectifiers in aircraft electric power systems.
Keywords :
aircraft power systems; power factor; power factor correction; power system control; rectifiers; aircraft electric power system; high power factor rectifiers; one cycle control; power 4 kW; power factor correction system; software Saber; three phase rectifiers; Aerospace control; Aircraft manufacture; Control systems; Power system dynamics; Power system modeling; Power system simulation; Prototypes; Reactive power; Rectifiers; Software prototyping; Aircraft Electric Power System; High Power Factor Rectifiers; One-Cycle Control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power System Conference, 2008. MEPCON 2008. 12th International Middle-East
Conference_Location :
Aswan
Print_ISBN :
978-1-4244-1933-3
Electronic_ISBN :
978-1-4244-1934-0
Type :
conf
DOI :
10.1109/MEPCON.2008.4562299
Filename :
4562299
Link To Document :
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