Method for flying-starting sensorless vector-controlled permanent magnet synchronous motor

Patent metadata

Field	Value
Publication number	US-2025167708-A1
Application number	US-202519023206-A
Country	US
Kind code	A1
Filing date	Jan 15, 2025
Priority date	Aug 10, 2023
Publication date	May 22, 2025
Grant date	—

Abstract

A method for flying-starting a sensorless vector-controlled permanent magnet synchronous motor (PMSM), including: setting, by a speed tracker of a sensorless vector-controlled PMSM in a flying-start state, an actual operating speed of the PMSM as a reference speed command, for field-oriented control to reduce a real-time running current of the PMSM; and checking, using an acceleration adaptive controller, whether the sensorless vector-controlled PMSM is starting with or against wind; if the sensorless vector-controlled PMSM is starting against the wind, setting an acceleration of the PMSM to a preset value; if the sensorless vector-controlled PMSM is starting with the wind, calculating a voltage error defined as a difference between a maximum bus voltage and a real-time bus voltage; and processing, through a proportional-integral controller, the voltage error to output a new acceleration of the PMSM.

First claim

What is claimed is:

1 . A method for flying-starting a sensorless vector-controlled permanent magnet synchronous motor (PMSM), the method comprising:
setting, by a speed tracker of a sensorless vector-controlled PMSM in a flying-start state, an actual operating speed (Spd_act) of the PMSM as a reference speed command (Spd_ref), with a q-axis reference current (Iq_ref) and a d-axis reference current (Id_ref) at zero, for field-oriented control (FOC) to reduce a real-time running current of the PMSM, where, the reference speed command (Spd_ref) is a current speed command used in a speed control loop; and checking, using an acceleration adaptive controller, whether the sensorless vector-controlled PMSM is starting with or against wind; if the sensorless vector-controlled PMSM is starting against the wind, setting an acceleration of the PMSM to a preset value (a 0 ); if the sensorless vector-controlled PMSM is starting with the wind, calculating a voltage error defined as a difference between a maximum bus voltage and a real-time bus voltage; and processing, through a proportional-integral (PI) controller, the voltage error to output a new acceleration (a) of the PMSM.

2 . The method of claim 1 , wherein the speed tracker and the acceleration adaptive controller are two additional units to a field-oriented control strategy;
during startup in the flying-start state, the speed tracker is initiated to monitor the actual operating speed (Spd_act); the actual operating speed (Spd_act) is set as the reference speed command (Spd_ref); both the q-axis reference current (Iq_ref) and the d-axis reference current (Id_ref) are set to zero; the FOC strategy is applied, until a real-time q-axis current (Iq) drops below a preset q-axis current (Iq 0 ); the speed tracker is disengaged, and the reference speed command (Spd_ref) is recorded; a first PI controller compares the q-axis reference current (Iq_ref) with the real-time q-axis current (Iq) to form a first current control loop; a second PI controller compares the d-axis reference current (Id_ref) with a real-time d-axis current (Id) to form a second current control loop; after the speed tracking is completed, the recorded reference speed command (Spd_ref) is compared with a target startup speed (Spd_target); if the recorded reference speed command (Spd_ref) is less than the target startup speed (Spd_target), the acceleration is set to a preset value (a 0 ); if the recorded reference speed command (Spd_ref) is greater than the target startup speed (Spd_target), the voltage error is calculated as the difference between the maximum bus voltage and the real-time bus voltage; and the voltage error is processed through a third PI controller to generate the new acceleration (a); and after acceleration adaptive control is completed, the FOC strategy is applied to adjust the actual operating speed (Spd_act) to approach the target startup speed (Spd_target).

3 . The method of claim 2 , wherein upon performing the FOC strategy, the PMSM starts with the recorded reference speed command (Spd_ref) and increases the reference speed command (Spd_ref), step by step, using the new acceleration (a) as a step size, to bring the reference speed command (Spd_ref) to match the target speed (Spd_target).

4 . The method of claim 3 , wherein when the reference speed command (Spd_ref) exceeds the target speed (Spd_target), the new acceleration (a) is calculated as follows:

a
=

kp
×
error

+

∫

(

ki
×
erorr

)

⁢
dt

where, kp and ki are parameters of the PI controller.

5 . The method of claim 4 , comprising:
S 1 : initializing all parameters, and setting a flag (Flag) to 1 for the speed tracker; S 2 : reading bus voltage (Vbus), phase currents, and the target startup speed (Spd_target); calculating the actual operating speed (Spd_act), the real-time q-axis current (Iq), and the real-time d-axis current (Id); S 3 : checking if the flag (Flag) is 1; if yes, proceeding to S 4 ; if no, skipping to S 6 ; S 4 : speed tracking: setting the actual operating speed (Spd_act) as the reference speed command (Spd_ref); checking if the real-time q-axis (Iq) is less than the preset q-axis current (Iq 0 ); if no, moving to S 5 ; if yes, setting the flag (Flag) to zero, recording the reference speed command (Spd_ref), and proceeding to S 6 ; S 5 : setting both the q-axis reference current (Iq_ref) and the d-axis reference current (Id_ref) to zero; applying the FOC strategy, and returning to S 2 ; S 6 : checking if the reference speed command (Spd_ref) is greater than the target startup speed (Spd_target); if no, setting the acceleration to a preset value a 0 ; if yes, calculating the voltage error defined as the difference between the maximum bus voltage and the real-time bus voltage; processing, through the PI controller, the voltage error to output the new acceleration a; and then proceeding to S 7 ; S 7 : recalculating, using the new acceleration a, the reference speed command (Spd_ref); comparing, through the PI controller, the recalculated reference speed command (Spd_ref) with the actual operating speed (Spd_act); performing FOC strategy, and then returning to S 2 .

6 . The method of claim 5 , wherein during the execution of the FOC strategy, the d-axis reference current (Id_ref) is generated by a maximum torque per ampere (MTPA) unit.

Assignees

• Zhongshan Broad Ocean Motor Co

Inventors

• Bian Wenqing

Classifications

• H02P21/34 Primary

  Arrangements for starting · CPC title

• H02P21/18

  Estimation of position or speed · CPC title

• H02P2205/07

  Speed loop, i.e. comparison of the motor speed with a speed reference · CPC title

• H02P2205/01

  Current loop, i.e. comparison of the motor current with a current reference · CPC title

• H02P2207/05

  Synchronous machines, e.g. with permanent magnets or DC excitation · CPC title