Modelling of a direct‐driven electromechanical actuation system based on the Lagrange–Maxwell equation
Author:
Affiliation:
1. State Key Laboratory of Electrical Insulation and Power Equipment Xi'an Jiaotong University Xi'an Shannxi China
2. Aviation Industry Corporation of Qing'an Group Co. Xi'an Shannxi China
Publisher
Institution of Engineering and Technology (IET)
Subject
Electrical and Electronic Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1049/elp2.12111
Reference30 articles.
1. Fault-tolerant electric drive for an aircraft nose wheel steering actuator
2. More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft
3. Safety-critical design of electromechanical actuation systems in commercial aircraft
4. Considerations on the Development of an Electric Drive for a Secondary Flight Control Electromechanical Actuator
5. Electromechanical Actuator for Helicopter Rotor Damper Application
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