Fast Converging with High Accuracy Est imates of Satellite Attitude and Orbit Based on Magnetometer Augmented with Gyro, Star Sensor and GPS via Extended Kalman Filter

Position fusion of sensors with dissimilar accuracies

Concurrent Spacecraft Attitude and Orbit Estimation with Attitude Control Based on Magnetometer, Gyroscope, and GPS Measurements through Extended Kalman Filter

Multisensor Data Fusion Fuzzy Similarity-based of Several Kalman Filters

Fusion of Low-Cost MEMS IMU/GPS Integrated Navigation System

SPACECRAFT ATTITUDE AND ATTITUDE RATE ESTIMATION USING HYBRID KALMAN FILTERING OF MAGNETOMETER MEASUREMENTS

SPACECRAFT ATTITUDE AND ATTITUDE RATE ESTIMATION USING HYBRID KALMAN FILTERING OF MAGNETOMETER MEASUREMENTS.

Adaptive dynamic kalman filter for high-performance tilt-angles estimation

Improving the Navigation System of a UAV Using Multi-Sensor Data Fusion Based on Fuzzy C-Means Clustering

Integrated MEMS-Based IMU/GPS navigation system for motion dynamical vehicles