High order harmonic balance applied to an aeroelastic T-tail model with a control surface freeplay
Author:
Affiliation:
1. Technical University of Milan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1704
Reference9 articles.
1. Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model
2. Active Aeroelastic Control Over a Multisurface Wing: Modeling and Wind-Tunnel Testing
3. Active Flutter Suppression for a Three-Surface Transport Aircraft by Recurrent Neural Networks
4. 5Roger, K. L. “Airplane Math Modeling Methods for Active Control Design,” Tech. Rep. CP-228, AGARD, August 1977.
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