Robust Switching Control and Subspace Identification for Flutter of Flexible Wing
Author:
Affiliation:
1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China
2. College of Mechanical Engineering, Donghua University, Shanghai, China
Abstract
Funder
Jiangsu Innovation Program for Graduate Education
Publisher
Hindawi Limited
Subject
Mechanical Engineering,Mechanics of Materials,Geotechnical Engineering and Engineering Geology,Condensed Matter Physics,Civil and Structural Engineering
Link
http://downloads.hindawi.com/journals/sv/2018/9734684.pdf
Reference26 articles.
1. Summary of an Active Flexible Wing program
2. Flutter suppression control law design and testing for the active flexible wing
3. A Continuous Robust Control Strategy for the Active Aeroelastic Vibration Suppression of Supersonic Lifting Surfaces
4. Time-domain modeling and control of a wing-section stall flutter
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