Dynamics of the Apollo electromechanical actuator.
Author:
Affiliation:
1. North American Rockwell Corporation, Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29302
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. Static Test Procedure for Electromechanical Actuators for UAV Applications;AIAA AVIATION 2022 Forum;2022-06-20
2. Torque Limiters for Aerospace Actuator Application;Energies;2022-02-17
3. A review of electromechanical actuators for More/All Electric aircraft systems;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2017-12-28
4. Review on signal-by-wire and power-by-wire actuation for more electric aircraft;Chinese Journal of Aeronautics;2017-06
5. Bibliography;Aerospace Actuators 2;2017-03-17
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