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

A state feedback suboptimal control law based on the state-dependent Riccati equation is derived for aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer was constructed to estimate the unavailable state variables of the system. With the control law designed, nonlinear effect of time delay between the control input and actuator are investigated by numerical approach. The closed-loop system including the observer and nonlinear controller is asymptotically stable. The simulation results show that the observer can give precise estimations for the plunge displacement and the velocities in pitch and plunge and that the controller is effective for flutter suppression. The time delay between the control input and actuator may jeopardize control performance and cause high-frequency vibration.