I. Introduction
The flux-switching permanent magnet (FSPM) machines are favorable for high speed operation due to its simple and robust rotor structure [1]. However, their torque density are limited by the space conflict between magnets and armature windings which are both accommodated on the stator. With the purpose to improve machine inner space utilization and thus the torque density, novel dual-armature FSPM (DA-FSPM) machines were proposed by adding a set of rotor armature winding to the rotor slots of traditional FSPM machines [2] [3]. It is found that the DA-FSPM machines exhibit many superior performances including high torque density and high fault tolerant capability, which are highly desirable for aerospace applications.