I. Introduction
With the development of the more electric aircraft, the integrated starter/generator has become the development trend. Further, the wound-rotor synchronous generator has been regarded as excellent candidate to be the integrated starter/generator for its mature generator technique and wide application [1]. As illustrated in Fig. 1, the wound-rotor synchronous starter/generator (WRSSG) consists of the pre-exciter (PE), the main exciter (ME), the rotating rectifier and the main machine (MM). The PE is a permanent magnet generator which does not connect to the system in the startup process. The ME is a rotating-armature electrically excited synchronous generator with three-phase field windings. The rotating rectifier is a three- phase full bridge diode rectifier and a wound-rotor synchronous machine serves as the MM.