Fault-Tolerant Control Strategies for Dual Three-Phase Permanent Magnet Synchronous Machine with YASA Topology under Open-Circuit Faults

For the dual three-phase permanent magnet motor with yokeless and segmented armature (YASA) topology used for electric aircraft propulsion, reliability is a fundamental requirement. Two fault-tolerant control strategies under single-phase open-circuit faults were analyzed in this paper, one of which is based on constant magnetomotive force (MMF), and another one is based on a reduced-order decoupling mathematical model. Minimization of copper loss and maximization of output torque were employed as control objectives. Through simulation analysis, the motor speed and torque can be maintained at pre-fault levels by fault-tolerant control. However, the connection of the neutral line brings significant odd harmonics in the current, causing notable torque ripple. The torque ripple reaches 7.51% and 14.26% for the two control objectives under constant MMF-based strategy. However, the reduced-order decoupling model-based control strategy alleviated this issue by mathematical correction of the post-fault model of the dual three-phase YASA machine, reducing torque ripple to 3.19%-4.10%.

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Publication Details

Published
2024-11-26
DOI
https://doi.org/10.23919/icems60997.2024.10921046
Citations
1
Primary Topic
Sensorless Control of Electric Motors
Type
article
Field-Weighted Citation Impact
0.21

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article

Fault-Tolerant Control Strategies for Dual Three-Phase Permanent Magnet Synchronous Machine with YASA Topology under Open-Circuit Faults

Zhongze Wu, Lingyun Shao, Xueyi Yan, Zhihong Liu et al.
1 citations
Sensorless Control of Electric Motors
0.21
article

Fault-Tolerant Control Strategies for Dual Three-Phase Permanent Magnet Synchronous Machine with YASA Topology under Open-Circuit Faults

Zhongze Wu, Lingyun Shao, Xueyi Yan, Zhihong Liu, Zhuoran Zhang
article en
1 citations

Abstract

For the dual three-phase permanent magnet motor with yokeless and segmented armature (YASA) topology used for electric aircraft propulsion, reliability is a fundamental requirement. Two fault-tolerant control strategies under single-phase open-circuit faults were analyzed in this paper, one of which is based on constant magnetomotive force (MMF), and another one is based on a reduced-order decoupling mathematical model. Minimization of copper loss and maximization of output torque were employed as control objectives. Through simulation analysis, the motor speed and torque can be maintained at pre-fault levels by fault-tolerant control. However, the connection of the neutral line brings significant odd harmonics in the current, causing notable torque ripple. The torque ripple reaches 7.51% and 14.26% for the two control objectives under constant MMF-based strategy. However, the reduced-order decoupling model-based control strategy alleviated this issue by mathematical correction of the post-fault model of the dual three-phase YASA machine, reducing torque ripple to 3.19%-4.10%.

Southeast University (CN), Nanjing University of Aeronautics and Astronautics (CN)
National Natural Science Foundation of China, China Postdoctoral Science Foundation, Natural Science Foundation of Jiangsu Province
Climate action
Openalex Percentile: Top 43%
Sensorless Control of Electric Motors
0.21
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