Improved Optimal Fault-Tolerant Control Considering Reluctance Torque for Five-Phase IPMSM in Aerospace Electric Actuation Application-Reference-Cited by-同舟云学术

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Improved Optimal Fault-Tolerant Control Considering Reluctance Torque for Five-Phase IPMSM in Aerospace Electric Actuation Application

Published:2024-10 Issue:10 Volume:71 Page:11785-11795
ISSN:0278-0046
Container-title:IEEE Transactions on Industrial Electronics
language:
Short-container-title:IEEE Trans. Ind. Electron.

Author:

Xu Jinquan¹^ORCID,Jin Wenbo¹^ORCID,Guo Hong¹^ORCID,Zhang Boyi¹^ORCID

Affiliation:

1. School of Automation Science and Electrical Engineering and the Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing, China

Funder

National Natural Science Foundation of China

Yeqisun Science Foundation

Major Program of the National Natural Science Foundation of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/41/10589453/10436376.pdf?arnumber=10436376

Reference29 articles.

1. Review of Electric Machines in More-/Hybrid-/Turbo-Electric Aircraft

2. Actuation Challenges in the More Electric Aircraft: Overcoming Hurdles in the Electrification of Actuation Systems

3. PWM Harmonic-Current-Based Interturn Short-Circuit Fault Diagnosis for the Aerospace FTPMSM System Even in the Fault-Tolerant Operation Condition

4. A Robust Observer and Nonorthogonal PLL-Based Sensorless Control for Fault-Tolerant Permanent Magnet Motor With Guaranteed Postfault Performance

5. A Novel Electro Hydrostatic Actuator System With Energy Recovery Module for More Electric Aircraft

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