Pages that link to "Item:Q2799253"
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The following pages link to Fault detection and isolation of the attitude control subsystem of spacecraft formation flying using extended Kalman filters (Q2799253):
Displaying 10 items.
- A two-stage extended Kalman filter method for fault estimation of satellite attitude control systems (Q509360) (← links)
- Spacecraft actuator diagnosis with principal component analysis: application to the rendez-vous phase of the Mars sample return mission (Q892579) (← links)
- Incremental locally linear embedding-based fault detection for satellite attitude control systems (Q1660851) (← links)
- A nonlinear observer-based approach to fault detection, isolation and estimation for satellite formation flight application (Q2280871) (← links)
- Two-stage exogenous Kalman filter for time-varying fault estimation of satellite attitude control system (Q2306185) (← links)
- FDI(R) for satellites: how to deal with high availability and robustness in the space domain? (Q2861922) (← links)
- Fault-tolerant cooperative output regulation for multi-vehicle systems with sensor faults (Q3132973) (← links)
- Adaptive finite‐time actuator fault‐tolerant coordinated attitude control of multispacecraft with input saturation (Q4967747) (← links)
- Distributed finite-time tracking control for multiple uncertain Euler-Lagrange systems with error constraints (Q5020779) (← links)
- Attitude coordinated output feedback control based on event triggering for multiple spacecrafts (Q5043500) (← links)
