Design of PMSM for EMA Employed in Secondary Flight Control Systems-Reference-Cited by-同舟云学术

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Design of PMSM for EMA Employed in Secondary Flight Control Systems

Published:2018-11 Issue: Volume: Page:
ISSN:
Container-title:2018 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC)
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Author:

Giangrande P.,Al-Timimy A.,Galassini A.,Papadopoulos S.,Degano M.,Galea M.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/8598649/8607267/08607467.pdf?arnumber=8607467

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An eGaN HEMT-Based High Power Density Controller for Permanent Magnet Synchronous Motor;2023 26th International Conference on Electrical Machines and Systems (ICEMS);2023-11-05

2. Minimisation of Failure Transients in a Fail-Safe Electro-Mechanical Actuator Employed for the Flap Movables of a High-Speed Helicopter-Plane;Aerospace;2022-09-19

3. Electromagnetic Design of Dual Winding Permanent Magnet Synchronous Motor for Electromechanical Actuators of Flight Control Systems;2022 International Power Electronics Conference (IPEC-Himeji 2022- ECCE Asia);2022-05-15

4. Design of Double Redundancy Controller for Electric Actuator Based on Dual three-phase PMSM;2021 IEEE 2nd China International Youth Conference on Electrical Engineering (CIYCEE);2021-12-15

5. Model-Based Condition-Monitoring and Jamming-Tolerant Control of an Electro-Mechanical Flight Actuator with Differential Ball Screws;Actuators;2021-09-09

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