Study of high power factor rectifiers based on one cycle control in aircraft electric power system

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.