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