@inproceedings{ce29d1773e43458e85cb173230162107,
title = "Design and testing of electromechanical actuator for aerospace applications",
abstract = "Electromechanical actuators are gaining interest in the aerospace industry within the More Electrical Aircraft (MEA) architecture. The end-goal of fully electric aircraft includes Electromechanical actuation for flight control systems. The design and testing of a flight control system for helicopter swash-plate is presented in this work. The mechanical system is driven by electrical machines and controlled by dedicated power electronics, both of which fit challenging space requirements and environmental conditions. The predicted performances are validated by experimental testing of prototypes.",
keywords = "Electro-mechanical actuator, Fault Tolerant, More Electric Aircraft, Permanent Magnet Machine",
author = "L. Papini and P. Connor and C. Patel and L. Empringham and C. Gerada and P. Wheeler",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives, IWED 2018 ; Conference date: 31-01-2018 Through 02-02-2018",
year = "2018",
month = mar,
day = "21",
doi = "10.1109/IWED.2018.8321392",
language = "English",
series = "2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives, IWED 2018 - Proceedings",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1--6",
booktitle = "2018 25th International Workshop on Electric Drives",
address = "United States",
}
