ℒ1adaptive control of an aeroelastic system with unsteady aerodynamics and gust load
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Publication:4639936
DOI10.1177/1077546316640407zbMath1387.93099OpenAlexW2329766068MaRDI QIDQ4639936
Sahjendra N. Singh, Keum W. Lee
Publication date: 15 May 2018
Published in: Journal of Vibration and Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1177/1077546316640407
unsteady aerodynamicsparameter identification\(\mathcal L_1\) adaptive controlaeroelastic system controlaeroelastic vibration control
Cites Work
- Aeroservoelasticity. Modeling and control
- Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity
- ℒ1Adaptive Control Theory
- Adaptive nonlinear regulation: estimation from the Lyapunov equation
- Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
- Output feedback nonlinear control of an aeroelastic system with unsteady aerodynamics
- Adaptive and neural control of a wing section using leading- and trailing-edge surfaces
- Continuous robust control for aeroelastic vibration control of a 2-D airfoil under unsteady flow
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