Pages that link to "Item:Q5067038"
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The following pages link to Fault estimation and fault tolerance control for spacecraft formation systems with actuator fault and saturation (Q5067038):
Displaying 11 items.
- Fault reconstruction approach for distributed coordinated spacecraft attitude control system (Q1665470) (← links)
- A nonlinear observer-based approach to fault detection, isolation and estimation for satellite formation flight application (Q2280871) (← links)
- Spacecraft formation stabilization and fault tolerance: a state-varying switched system approach (Q2637587) (← links)
- Fault detection and isolation of the attitude control subsystem of spacecraft formation flying using extended Kalman filters (Q2799253) (← links)
- A distributed model predictive control (MPC) fault reconfiguration strategy for formation flying satellites (Q2807918) (← links)
- Cooperative actuator fault accommodation in formation flight of unmanned vehicles using relative measurements (Q2909409) (← links)
- A new aerodynamic decoupled frequential FDIR methodology for satellite actuator faults (Q3458163) (← links)
- Trajectory planning/re-planning for satellite systems in rendezvous mission in the presence of actuator faults based on attainable efforts analysis (Q5265645) (← links)
- Finite‐time fault‐tolerant output feedback attitude control of spacecraft formation with guaranteed performance (Q6083788) (← links)
- Distributed adaptive control for multiple unmanned aerial vehicles with state constraints and input quantization (Q6125673) (← links)
- Prescribed performance adaptive fault-tolerant control for nonlinear systems with actuator faults and input dead-zone (Q6545326) (← links)
