Controller Design for Electro-mechanical Actuators
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-16-7423-5_46
Reference7 articles.
1. Cao, W., Mecrow, B., Atkinson, G., Bennett, J., Atkinson, D.: Overview of electric motor technologies used for more electric aircraft (MEA). IEEE Trans. Industr. Electron. 59(9), 3523–3531 (2012)
2. Thompson, K.: Notes on “The electric control of large aeroplanes.” IEEE Aerosp. Electron. Syst. Mag. 3(12), 19–24 (1988)
3. Li, J., et al.: A review of electromechanical actuation system for more electric aircraft. In: 2016 IEEE International Conference on Aircraft Utility Systems (AUS) (2016)
4. Papini, L., et al.: Design and testing of electromechanical actuator for aerospace applications. In: 2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED) (2018)
5. Aten, M.: Dynamic performance of a matrix converter driven electro-mechanical actuator for an aircraft rudder. In: Second IEE International Conference on Power Electronics, Machines and Drives (2004)
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