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Modeling and Single-Variable-Based Axial Force Balance Control of Conical PMSM for Electric Aircraft Propulsion System

  • Yukun Fan
  • , Peixin Liang
  • , Lirui Liu
  • , Xiaocun Gu
  • , Lihao Liang
  • , Weiguo Liu
  • , Qi He
  • Northwestern Polytechnical University Xian
  • Shaanxi Aero Electric Co. Ltd

科研成果: 期刊稿件文章同行评审

摘要

The permanent magnet synchronous motor (PMSM) and propeller direct-drive systems are widely used in electric aircraft due to their lightweight and high-efficiency structure. During flight, the thrust generated by the propeller is transmitted to the motor bearings through the rotating shaft, leading to increased bearing wear and consequently affecting the service life of the electric propulsion system. This article proposes an axial force balance control strategy by considering the characteristics of permanent magnet synchronous conical motors. First, to address the lack of mathematical models for axial forces in conical PMSMs (CPMSMs), a mathematical modeling method is proposed. Based on the characteristics of the mathematical model, a simplified method using the fundamental wave of magnetic potential is presented. To solve the control complexity caused by multivariate influences on axial forces, a single-variable-based model predictive axial force control (SVB-MP-AFC) is proposed, along with a state smooth switching method to reduce bearing wear and improve system stability. Finally, the simulations and experiments verify the accuracy of the mathematical model and the effectiveness of the control strategy.

源语言英语
页(从-至)4256-4268
页数13
期刊IEEE Journal of Emerging and Selected Topics in Power Electronics
14
4
DOI
出版状态已出版 - 1 8月 2026

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