Pages that link to "Item:Q4565997"
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The following pages link to Nussbaum‐type function–based attitude control of spacecraft with actuator saturation (Q4565997):
Displaying 12 items.
- Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft (Q2081840) (← links)
- Inertia‐free attitude stabilization for flexible spacecraft with active vibration suppression (Q3300450) (← links)
- Fault‐tolerant spacecraft attitude control under actuator saturation and without angular velocity (Q3300462) (← links)
- Adaptive fuzzy finite‐time consensus tracking for multiple Euler‐Lagrange systems with unknown control directions (Q6049912) (← links)
- Finite‐time rotation‐matrix‐based tracking control for autonomous underwater vehicle with input saturation and actuator faults (Q6063186) (← links)
- Guaranteed cost control of rigid‐body attitude systems under control saturation (Q6068503) (← links)
- Adaptive saturated tracking control for spacecraft proximity operations via integral terminal sliding mode technique (Q6082381) (← links)
- Predefined‐time tracking control for high‐order nonlinear systems with control saturation (Q6082755) (← links)
- Finite‐time fault‐tolerant output feedback attitude control of spacecraft formation with guaranteed performance (Q6083788) (← links)
- Event‐triggered anti‐disturbance attitude control for rigid spacecrafts with multiple disturbances (Q6083842) (← links)
- Distributed finite-time backstepping adaptive containment control for multiple unmanned aerial vehicles with input saturation (Q6577276) (← links)
- Novel robust observer-controller synthesis method for Takagi-Sugeno systems (Q6578444) (← links)
