Pages that link to "Item:Q2416670"

The following pages link to Output feedback robust \(H_\infty\) control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach (Q2416670):

Displaying 11 items.

• Observer-based stabilization of spacecraft rendezvous with variable sampling and sensor nonlinearity (Q474722) (← links)
• Observer-based robust control for spacecraft rendezvous with thrust saturation (Q1724791) (← links)
• Disturbance observer based fault-tolerant control for cooperative spacecraft rendezvous and docking with input saturation (Q1991822) (← links)
• Delayed anti-windup strategy for input-delay systems with actuator saturations (Q2181368) (← links)
• Output feedback gain scheduled control of actuator saturated linear systems with applications to the spacecraft rendezvous (Q2263943) (← links)
• Multi-objective output feedback control for autonomous spacecraft rendezvous (Q2410792) (← links)
• Robust active suppression for body-freedom flutter of a flying-wing unmanned aerial vehicle (Q2656867) (← links)
• Robustness of ISS systems to inputs with limited moving average: application to spacecraft formations (Q2798391) (← links)
• A class of globally stabilizing feedback controllers for the orbital rendezvous problem (Q3133861) (← links)
• Robust H_∞ dynamic output feedback control for spacecraft rendezvous with poles and input constraint (Q5347318) (← links)
• Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation (Q6149795) (← links)