I. INTRODUCTION
With the development of More Electric Aircraft (MEA), the Integrated Starter/Generator (ISG) system based on a multi-stage brushless Wound-Rotor Synchronous Machine becomes more and more popular, owing to its high safety (when facing short circuit problem, the fielding current can be cut off) [1]. This ISG system is consist of a Pre-Exciter (PE), a Main Exciter (ME), a Rotating Rectifier and a Main Machine (MM) [2]-[4]. The ME provides the field current for MM through the rotating rectifier.