Pages that link to "Item:Q4929482"
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The following pages link to Robust aeroelastic control of flapped wing systems using a sliding mode observer (Q4929482):
Displaying 11 items.
- Numerical analysis of flow-induced nonlinear vibrations of an airfoil with three degrees of freedom (Q365460) (← links)
- Sliding mode disturbance observer-based backstepping control for a transport aircraft (Q893633) (← links)
- Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material (Q1659816) (← links)
- Robust passive adaptive fault tolerant control for stochastic wing flutter via delay control (Q2423963) (← links)
- A new control framework for flapping-wing vehicles based on 3D pendulum dynamics (Q2662252) (← links)
- Active control of hypersonic airfoil flutter via adaptive fuzzy sliding mode method (Q2832371) (← links)
- (Q3561504) (← links)
- (Q4641439) (← links)
- Sliding Mode Observer Controller Design for a Two Dimensional Aeroelastic System with Gust Load (Q5194819) (← links)
- Robust Actuator‐Fault‐Tolerant Control System Based on Sliding‐Mode Observer for Thrust‐Vectoring Aircrafts (Q5194831) (← links)
- Continuous robust control for aeroelastic vibration control of a 2-D airfoil under unsteady flow (Q5270821) (← links)