Robust Finite-Time Continuous Control of an Unsteady Aeroelastic System
Author:
Affiliation:
1. Catholic Kwandong University, Gangneung 25601, Republic of Korea
2. University of Nevada, Las Vegas, Las Vegas, Nevada 89154
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G003087
Reference28 articles.
1. Historical Perspective on Analysis and Control of Aeroelastic Responses
2. Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations
3. Robust Multivariable Flutter Suppression for Benchmark Active Control Technology Wind-Tunnel Model
4. Transonic Flutter Suppression Control Law Design and Wind-Tunnel Test Results
5. Aeroelastic Response of a Rigid Wing Supported by Nonlinear Springs
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