Aeroelastic dynamic response and control of an airfoil section with hysteresis nonlinearity

Engineering

• Actuator 100%
• Control Law 100%
• Nonlinearity 100%
• Delay Time 100%
• Dynamic Response 100%
• Control Input 100%
• Airfoil Section 100%
• Simulation Result 50%
• Feedback Control 50%
• Two Dimensional 50%
• Frequency Vibration 50%
• Riccati Equation 50%
• Nonlinear Effect 50%
• State Feedback 50%
• State Variable 50%
• Numerical Approach 50%