Linear-Parameter-Varying Control of an Improved Three-Degree-of-Freedom Aeroelastic Model
Author:
Affiliation:
1. University of Adelaide, Adelaide, South Australia 5005, Australia
2. Texas A&M University, College Station, Texas 77843
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.45657
Reference11 articles.
1. Historical Perspective on Analysis and Control of Aeroelastic Responses
2. Modeling the Benchmark Active Control Technology wind-tunnel model for application to flutter suppression
3. Identification and Control of Limit Cycle Oscillations in Aeroelastic Systems
4. Control of a Nonlinear Wing Section Using Leading- and Trailing-Edge Surfaces
5. Suppression of Control Reversal Using Leading- and Trailing-Edge Control Surfaces
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