Pages that link to "Item:Q1660439"
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The following pages link to Analytical redundancy based fault diagnosis scheme for satellite attitude control systems (Q1660439):
Displaying 12 items.
- 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)
- Fault reconstruction approach for distributed coordinated spacecraft attitude control system (Q1665470) (← links)
- Fault diagnosis for a kind of nonlinear systems by using model-based contribution analysis (Q1796759) (← links)
- A nonlinear observer-based approach to fault detection, isolation and estimation for satellite formation flight application (Q2280871) (← links)
- Robust actuator fault diagnosis scheme for satellite attitude control systems (Q2451865) (← links)
- FDI(R) for satellites: how to deal with high availability and robustness in the space domain? (Q2861922) (← links)
- A new aerodynamic decoupled frequential FDIR methodology for satellite actuator faults (Q3458163) (← links)
- Fault diagnosis for satellite sensors and actuators using nonlinear geometric approach and adaptive observers (Q5208255) (← links)
- Advances in Neural Networks – ISNN 2005 (Q5707635) (← links)
- Observer-based multiple faults diagnosis scheme for satellite attitude control system (Q6563335) (← links)
- Redundancy analysis for zone target multivariable control system (Q6578867) (← links)
