Active Flutter Suppression Controllers Derived from Linear and Nonlinear Aerodynamics: Application to a Transport Aircraft Model
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2836
Reference27 articles.
1. Announcements and Acknowledgments
2. Flutter suppression control law design and testing for the active flexible wing
3. Aeroelastic responses identification of a high-aspect-ratio flexible wing model and its active flutter suppression strategy
4. Active flutter suppression of a multiple-actuated-wing wind tunnel model
5. Applied Active Control for a Nonlinear Aeroelastic Structure
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