Pages that link to "Item:Q5028694"
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The following pages link to Output constraints vibration control for a flexible aircraft wing with prescribed performance (Q5028694):
Displaying 7 items.
- Adaptive boundary control of store induced oscillations in a flexible aircraft wing (Q290876) (← links)
- Vibration control for a flexible satellite system with output constraints (Q345649) (← links)
- Modeling and vibration control of a flexible aerial refueling hose with variable lengths and input constraint (Q510138) (← links)
- Boundary feedback stabilization of a flexible wing model under unsteady aerodynamic loads (Q1716501) (← links)
- Vibration control of a flexible aerial refuelling hose with input saturation (Q5347313) (← links)
- Safe tracking control based on a secure boundary protection method for nonlinear systems with unknown initial tracking condition (Q6577116) (← links)
- Adaptive neural network control of multiple-sectioned flexible riser with time-varying output constraint and input nonlinearity (Q6583323) (← links)
