Pages that link to "Item:Q4990452"
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The following pages link to Fixed‐time attitude tracking control for spacecraft based on adding power integrator technique (Q4990452):
Displaying 13 items.
- Fixed-time attitude tracking control for rigid spacecraft (Q2173966) (← links)
- Fixed-time control for high-precision attitude stabilization of flexible spacecraft (Q2220082) (← links)
- Predefined‐time control of cooperative manipulators (Q6061249) (← links)
- Output feedback stabilization within prescribed finite time of asymmetric time‐varying constrained nonholonomic systems (Q6061834) (← links)
- Constrained fast finite‐time exact tracking for disturbed nonlinear systems (Q6065811) (← links)
- Guaranteed cost control of rigid‐body attitude systems under control saturation (Q6068503) (← links)
- Predefined‐time tracking control for high‐order nonlinear systems with control saturation (Q6082755) (← links)
- Barrier Lypunov functions‐based nonsingular fixed‐time switching control for strict‐feedback nonlinear dynamics with full state constraints (Q6092362) (← links)
- Continuous precise predefined-time attitude tracking control for a rigid spacecraft (Q6105541) (← links)
- Continuous appointed‐time prescribed performance attitude tracking control for rigid spacecraft with actuator faults on SO(3) (Q6117459) (← links)
- Event-triggered adaptive fixed-time fuzzy control for uncertain nonlinear systems with unknown actuator faults (Q6125227) (← links)
- Neural learning fixed-time adaptive tracking control of complex stochastic constraint nonlinear systems (Q6136437) (← links)
- Fixed-time fuzzy adaptive robust \(H_\infty\) control for nonstrict-feedback nonlinear systems with input saturation and output constraints (Q6498028) (← links)
