航空永磁电机无位置传感器控制技术综述

Review of Sensorless Control Techniques for Aviation Permanent Magnet Synchronous Motors

  • 摘要: 随着航空电动化进程的加速,永磁同步电机在飞机起落架、舵面操纵及燃油泵等关键系统中广泛应用,对驱动系统的可靠性、环境适应性与冗余能力提出了更高要求。无位置传感器控制技术因其在提升系统可靠性与结构简化方面的优势,已成为航空电机驱动领域的重要研究方向。本文系统梳理了永磁电机无位置传感器控制技术的研究进展,重点综述了适用于低速区间的高频信号注入方法、面向中高速运行的模型类观测器设计以及复合估计策略的实现途径。分析了交叉耦合效应、逆变器非线性特性及电机参数失配等因素对转子位置估计精度的影响机理,进一步总结了从参数辨识、扰动补偿等提升鲁棒性的技术路线,并结合航空应用需求讨论了切换策略、稳态误差抑制等关键工程问题。最后,展望了航空永磁电机无位置传感器技术未来发展方向。

     

    Abstract: With the accelerated electrification of aircraft systems, permanent magnet synchronous motors(PMSMs) have been increasingly deployed in critical applications such as landing gear actuation, flight-control surfaces, and fuel-pump systems. These applications impose stringent requirements on the reliability, environmental adaptability, and redundancy of the drive system. Sensorless control techniques, which enhance system reliability and simplify the overall structure, have therefore become a key research focus in aviation-grade motor drives. A comprehensive review of recent advancements in sensorless control of PMSMs is provided. Particular attention is given to high-frequency signal injection methods suitable for low-speed operation, model-based observer designs for medium- to high-speed regions, and hybrid estimation strategies that integrate multiple approaches. The influences of cross-coupling magnetic saturation, inverter nonlinearities, and parameter mismatches on rotor position estimation accuracy are examined in detail. In addition, technical approaches for improving robustness—ranging from online parameter identification to disturbance-compensation structures—are summarized, and critical engineering issues such as algorithm-switching strategies and steady-state error suppression are discussed in the context of aviation requirements. Finally, potential future research directions for sensorless PMSM drives in aerospace applications are outlined.

     

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