Data-driven active flutter control of airfoil with input constraints based on adaptive dynamic programming method
Author:
Affiliation:
1. Department of Mechanics, Tianjin University, Tianjin, China
2. Tianjin Key Laboratory of Nonlinear Dynamics and Control, China
3. School of Engineering, University of California, Merced, CA, USA
Abstract
Funder
National Natural Science Foundation of China
Natural Science Foundation of Tianjin
China Postdoctoral Science Foundation
Publisher
SAGE Publications
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science
Link
http://journals.sagepub.com/doi/pdf/10.1177/10775463211001182
Reference59 articles.
1. Modeling and identification of freeplay nonlinearity
2. Model-Free Gradient-Based Adaptive Learning Controller for an Unmanned Flexible Wing Aircraft
3. Active flutter control of thin walled wing-engine system using piezoelectric actuators
4. Terminal sliding mode control for aeroelastic systems
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