Modeling and Experimental Study on the Dynamic Stiffness of an Electromechanical Actuator
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 305-701, Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33483
Reference17 articles.
1. KarpelM. “Design for Active and Passive Flutter Suppression and Gust Alleviation,” NASA CR-3482, 1981.
2. Nonlinear flutter analysis of missiles with pneumatic fin actuators
3. Stiffness enhancement of flight control actuator
4. New Flutter-Suppression Method for a Missile Fin with an Actuator
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