I. Introduction
The rapid development of more electric aircraft (MEA) has led to great demand for large-capacity and high-reliability integrated starter/generator systems. The wound-rotor synchronous starter/generator (WRSSG) has become a research focus due to its high reliability, mature generator technique, and large-scale on-board applications [1], [2]. As shown in Fig. 1, the WRSSG comprises a pre-exciter (PE), a main exciter (ME), a rotating rectifier, and a main machine (MM). The PE is a permanent magnet synchronous machine, and the ME is a rotating-armature electrically excited generator with three-phase stator windings. The rotating rectifier, mounted on the rotor shaft, is a three-phase full-bridge diode rectifier, and a wound-rotor synchronous machine serves as the MM.
Structure of the WRSSG.