The invention belongs to the related technical field of airplanes, and particularly relates to a control method of an
airplane starting and generating integrated motor, which comprises the following steps that S1, in a starting mode, firstly,
coordinate change needs to be carried out on current; a current waveform under a
natural coordinate system is converted into a synchronous rotating shaft, and error-free adjustment can be realized through a PI controller after a measured value is compared with a reference value; S2, SG transition control comprises control of connection and disconnection of a ground power supply, conversion of a closed-
loop control strategy and connection and disconnection of an equipment load switch; and S3, in the generating mode, the maximum direct-
current voltage output by the SG is limited by the
bus voltage. The invention provides a set of complete control strategy of the
airplane starting and generating integrated motor. Therefore, the SG can provide enoughkinetic energy when the
airplane engine is started, the safety of transition conversion can be guaranteed, the generating mode can be smoothly switched to, high-quality
electric energy is provided forthe whole airplane, and
technical support is provided for the application of the starting and generating integrated motor to a multi-electric airplane and a full-electric airplane.