Pages that link to "Item:Q2313832"
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The following pages link to Unscented Kalman filter and smoothing applied to attitude estimation of artificial satellites (Q2313832):
Displaying 9 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)
- 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)
- Celestial mechanics, spacecrafts, and 50th years of the first humans on the Moon (Q2313826) (← links)
- Using extended Kalman filter and least squares method for spacecraft attitude estimation (Q2882846) (← links)
- SVD‐aided EKF attitude estimation with UD factorized measurement noise covariance (Q5215189) (← links)
- A computationally efficient unscented Kalman smoother for ameliorated tracking of subatomic particles in high energy physics experiments (Q6155964) (← links)
