Pages that link to "Item:Q5270821"
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The following pages link to Continuous robust control for aeroelastic vibration control of a 2-D airfoil under unsteady flow (Q5270821):
Displaying 13 items.
- Control of limit cycle oscillations of a two-dimensional aeroelastic system (Q966393) (← links)
- On unsteady aerodynamic airfoil loads in the design of a control system for minimizing the effect of wind perturbations using the rudder on the trailing edge of the wing (Q1951897) (← links)
- Feedback control of a nonlinear aeroelastic system with non-semi-simple eigenvalues at the critical point of Hopf bifurcation (Q2235349) (← links)
- Robust aeroelastic control of two-dimensional supersonic flapped wing systems (Q2385312) (← links)
- Advances in the linear/nonlinear control of aeroelastic structural systems (Q2575192) (← links)
- Robust active suppression for body-freedom flutter of a flying-wing unmanned aerial vehicle (Q2656867) (← links)
- (Q3561504) (← links)
- A note on typographical errors defining Theodorsen's coefficients for aeroelastic analysis (Q4554648) (← links)
- A feedback control strategy for the airfoil system under non-Gaussian colored noise excitation (Q4591603) (← links)
- ℒ<sub>1</sub>adaptive control of an aeroelastic system with unsteady aerodynamics and gust load (Q4639936) (← links)
- Efficient roll control using distributed control surfaces and aeroelastic effects (Q4929439) (← links)
- Adaptive aeroelastic vibration suppression of a supersonic airfoil with flap (Q4929492) (← links)
- Geometric-control formulation and averaging analysis of the unsteady aerodynamics of a wing with oscillatory controls (Q5158356) (← links)
