Multiple-Input Multiple-Output Experimental Aeroelastic Control Using a Receptance-Based Method
Author:
Affiliation:
1. University of Liverpool, Liverpool, England L69 GH, United Kingdom
2. Polytechnic University of Turin, 10129 Turin, Italy
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference28 articles.
1. Inverse eigenvalue problems in vibration absorption: Passive modification and active control
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3. RogerK. “Airplane Math Modelling Methods via Dynamic Realization,” AGARD, CP-228, Neuilly-Sur-Seine, France, April 1977.
4. Active Flutter Suppression-A Flight Test Demonstration
5. Reduced-Order Optimal Feedback Control Law Synthesis for Flutter Suppression
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