Abstract
As the concept of more-electric aircraft is put forward, the power actuation system comes into being. In recent years, the electromechanical actuator system has attracted more and more attention due to the development of the rare-earth permanent magnet brushless DC motor. The Simulink model of Brushless DC motor(BLDCM) was established, the theoretical analysis of the typical BLCDM faults and the fault simulation results of motor windings and power transistor were given.
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