Pages that link to "Item:Q5743757"
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The following pages link to Robust adaptive unscented Kalman filter for attitude estimation of pico satellites (Q5743757):
Displaying 15 items.
- Robust Kalman filtering for small satellite attitude estimation in the presence of measurement faults (Q397555) (← links)
- Robust adaptive filter for small satellite attitude estimation based on magnetometer and gyro (Q1722222) (← 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)
- Adaptive decentralized Kalman filters with non-common states for nonlinear systems (Q2667480) (← links)
- UKF based in-flight calibration of magnetometers and rate gyros for pico satellite attitude determination (Q2937828) (← links)
- Adaptive UKF algorithm under condition of sensor faults (Q2992387) (← links)
- Augmented robust three-stage extended Kalman filter for Mars entry-phase autonomous navigation (Q4638007) (← links)
- Adaptive Kalman filtering for closed-loop systems based on the observation vector covariance (Q5095503) (← links)
- Adaptive unscented Kalman filter for neuronal state and parameter estimation (Q6172485) (← links)
- Unscented Kalman filter with stable embedding for simple, accurate, and computationally efficient state estimation of systems on manifolds in Euclidean space (Q6190232) (← links)
- Attitude filtering with uncertain process and measurement noise covariance using <scp>SVD</scp>‐aided adaptive <scp>UKF</scp> (Q6194850) (← links)
- Robust attitude estimation of rotating space debris based on virtual observations of neural network (Q6495641) (← links)
- Adaptive Gaussian filters for nonlinear state estimation with one-step randomly delayed measurements (Q6580890) (← links)