T. Lei, Xiao-bin Zhang, Yang Dong, Jingjing Zhao, Hui Lin
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Study of high power factor rectifiers based on one cycle control in aircraft electric power system
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.
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