Pages that link to "Item:Q1307800"
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The following pages link to Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity (Q1307800):
Displaying 16 items.
- Adaptive boundary control of store induced oscillations in a flexible aircraft wing (Q290876) (← links)
- An analytical and experimental investigation into limit-cycle oscillations of an aeroelastic system (Q354919) (← links)
- Quadratic stabilization of a nonlinear aeroelastic system using a novel neural-network-based controller (Q412952) (← links)
- Hopf bifurcation of forced Chen system and its stability via adaptive control with arbitrary parameters (Q781402) (← links)
- Output feedback modular adaptive control of a nonlinear prototypical wing section (Q813865) (← links)
- Boundary feedback stabilization of a flexible wing model under unsteady aerodynamic loads (Q1716501) (← links)
- Flutter instability and active aeroelastic control with time delay for a two-dimensional airfoil (Q2063426) (← links)
- Detection of subcritical Hopf and fold bifurcations in an aeroelastic system via the describing function method (Q2098659) (← links)
- Stability and Hopf bifurcation of a two-dimensional supersonic airfoil with a time-delayed feedback control surface (Q2346251) (← links)
- A data-driven quadratic stability condition and its application for stabilizing unknown nonlinear systems (Q2346254) (← links)
- Limit cycle oscillation suppression of 2-DOF airfoil using nonlinear energy sink (Q2449698) (← links)
- Structured Model Reference Adaptive Control for a Wing Section with Structural Nonlinearity (Q4443152) (← links)
- ℒ<sub>1</sub>adaptive control of an aeroelastic system with unsteady aerodynamics and gust load (Q4639936) (← links)
- (Q5071329) (← links)
- Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances (Q5120989) (← links)
- Continuous robust control for aeroelastic vibration control of a 2-D airfoil under unsteady flow (Q5270821) (← links)
