Robust aeroelastic control of a thin-walled wing structure with model uncertainty

Keyphrases

• Thin-walled 100%
• Model Uncertainty 100%
• Aeroelastic Control 100%
• Wing Structure 100%
• External Load 66%
• Numerical Results 33%
• Thin-walled Beam 33%
• External Excitation 33%
• Incompressible Flow 33%
• Dynamic Response 33%
• Circumferentially Asymmetric Stiffness 33%
• Sliding Mode Observer 33%
• Robust Features 33%
• Flow Field 33%
• Fiber-reinforced Composites 33%
• Stiffness Configuration 33%
• Sliding Mode Control 33%
• Dynamic Response Analysis 33%
• Unstable Dynamics 33%
• Unsteady Aerodynamics 33%
• Vibration Dynamics 33%
• Control Response 33%
• Aircraft Wing Structure 33%
• Sliding Mode Method 33%
• Robust Vibration Control 33%
• Linear Quadratic Gaussian Regulator 33%
• Motion Group 33%

Engineering

• Aeroelastic Control 100%
• Model Uncertainty 100%
• Dynamic Response 66%
• Sliding Mode 66%
• External Load 66%
• Vibration Control 33%
• Incompressible Flow 33%
• Wings 33%
• Linear Quadratic Gaussian 33%
• Reinforced Composite Material 33%
• Fiber-Reinforced Composite 33%
• Sliding Mode Control 33%
• Mode Method 33%
• Vibration Dynamics 33%
• Flow Distribution 33%