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Publishing Language: Chinese

Sensorless control of servo motor based on adaptive amplitude-phase square wave injection

Yang HE1( )Wangwang LI1Jinghua JI1Wenxiang ZHAO1,2Jihong ZHU3
School of Electrical and Information Engineering, Jiangsu University, Zhenjiang 212013, China
School of Electric Power Engineering, Nanjing Institute of Technology, Nanjing 211167, China
Department of Precision Instrument, Tsinghua University, Beijing 100084, China
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Abstract

Existing sensorless control methods are constrained by the convergence rate and estimation accuracy, and is difficult to be directly applied to high dynamic electro-mechanical servo systems. To improve the estimation accuracy of sensorless control under high dynamics, this paper proposes a novel sensorless control method for the permanent magnet synchronous motor based on amplitude-phase adaptive square wave injection. By injecting high-frequency square wave voltage signals and demodulating the high-frequency response current of the q-axis, high dynamic rotor position estimation is achieved. At the same time, the amplitude and phase of the injected voltage are adaptively adjusted according to the real-time operating status of the motor. Therefore, the estimation errors caused by inverter nonlinearity and motor cross-saturation effect are effectively reduced. Finally, the performance of the method proposed is experimentally verified on a 2 kW servo motor platform. The experimental results show that the proposed method can enhance the accuracy of rotor position estimation, while achieving high dynamic characteristics of sensorless control.

CLC number: V242.4; TP273 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 630211

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Cite this article:
HE Y, LI W, JI J, et al. Sensorless control of servo motor based on adaptive amplitude-phase square wave injection. Acta Aeronautica et Astronautica Sinica, 2024, 45(15): 630211. https://doi.org/10.7527/S1000-6893.2024.30211

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Received: 22 January 2024
Revised: 28 February 2024
Accepted: 08 May 2024
Published: 23 May 2024
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica