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Lighter aircraft structures increase their efficiency but introduce challenges due to their flexibility. A novel controller was developed using the wing motion and surface pressure measurements to eliminate these issues and enable flexible structures to fly safely.
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This page is a summary of: Experimental Active Flutter Suppression Control with Inertial and Aerodynamic Feedback, Journal of Aircraft, March 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037978.
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