I. Introduction
With the rapid development of more electric aircraft, the wound-rotor synchronous starter/generator (WRSSG) has become the perfect candidate to become an integrated starter/generator due to its high safety and low maintenance cost [1], [2]. Furthermore, there is no position sensor installed for the WRSSG studied in this article since sensorless control for the WRSSG has become an inevitable trend and choice [3]–[5]. Fig. 1 shows the typical structure of the WRSSG, which 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, and an electrically excited wound-rotor synchronous machine serves as the MM. The ME is a rotating-armature electrically excited synchronous machine with three-phase stator windings. The rotating rectifier is a typical three-phase diode rectifier that is adopted to achieve a brushless structure.