I. Introduction
Wound-Rotor synchronous starter/generator (WRSSG) has been widely used as the generator in the aircraft power system. Integrated starter generator (ISG) system removes the special starter and uses WRSSG as the motor to start the aero engine in the starting mode [1]–[4]. The control of WRSSG in starting process requires the rotor position to generate the required torque. In traditional ISG system, the mechanical position sensor increases the size and decreases the reliability. Hence, the sensorless control techniques of WRSSG have been investigated in the past few years [5], [6].