Flight control design for a highly flexible flutter demonstrator
Author:
Affiliation:
1. Hungarian Academy of Sciences
2. German Aerospace Center (DLR)
3. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1817
Reference22 articles.
1. Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight
2. Designing an UAV Propulsion System for Dedicated Acceleration and Deceleration Requirements
3. Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings
4. Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator
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4. Comparing Different Potential Flow Methods for Unsteady Aerodynamic Modelling of a Flutter Demonstrator Aircraft;AIAA SCITECH 2023 Forum;2023-01-19
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