Pages that link to "Item:Q2882846"
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The following pages link to Using extended Kalman filter and least squares method for spacecraft attitude estimation (Q2882846):
Displaying 11 items.
- A two-stage extended Kalman filter method for fault estimation of satellite attitude control systems (Q509360) (← links)
- Optimal estimation for the satellite attitude using star tracker measurements (Q1076656) (← links)
- Application of federal Kalman filter with neural networks in the velocity and attitude matching of transfer alignment (Q1646454) (← links)
- Analysis of attitude determination methods using GPS carrier phase measurements (Q1954966) (← links)
- Unscented Kalman filter applied to the spacecraft attitude estimation with Euler angles (Q1955439) (← links)
- Two-stage exogenous Kalman filter for time-varying fault estimation of satellite attitude control system (Q2306185) (← links)
- Unscented Kalman filter and smoothing applied to attitude estimation of artificial satellites (Q2313832) (← links)
- Fault detection and isolation of the attitude control subsystem of spacecraft formation flying using extended Kalman filters (Q2799253) (← links)
- Relative position estimation using an extended Kalman filter during the homing phase of rendezvous and docking (Q3363198) (← links)
- Augmented robust three-stage extended Kalman filter for Mars entry-phase autonomous navigation (Q4638007) (← links)
- Focal plane calibration of the Spitzer space telescope (Q5375711) (← links)
