Design of active flutter suppression and wind-tunnel tests of a wing model involving a control delay
Author:
Funder
Priority Academic Program Development of Jiangsu Higher Education Institutions
Publisher
Elsevier BV
Subject
Mechanical Engineering
Reference23 articles.
1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;AIAA Journal,1969
2. Multi-input/multi-output adaptive active flutter suppression for a wing model;Andrighettoni;Journal of Aircraft,1998
3. Active flutter suppression using recurrent neural networks;Bernelli-Zazzera;Journal of Guidance, Control and Dynamics,2000
4. Using a new discretization approach to design a delayed LQG controller;Haraguchi;Journal of Sound and Vibration,2008
5. Single-input/single-output adaptive flutter suppression of a three-dimensional aeroelastic system;Huang;Journal of Guidance, Control and Dynamics,2012
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