I. Introduction
The switched reluctance motor (SRM) is very suitable to be used as the core motor of aerospace starting/generating systems because of its advantages of large capacity, simple structure, large starting torque, high power density, high fault tolerance, and appropriate high speed, high temperature, and other harsh conditions [1], [2], [3], [4]. SRM allows bidirectional energy transfer. It has good speed regulation performance in starting mode [5], [6] and does well in high-speed generating mode [7], [8]. Since the control methods of the electric and the generating modes are the same, the conversion between the two modes can be easily realized without any other accessories [9], so it can ensure high stability and fault tolerance in complex and harsh working environments.