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

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

A TERRESTRIAL STRAPDOWN NAVIGATION ALGORITHM

ARCHITECTURE FOR FILTER ALGORITHM IN GPS/INS INTEGRATION

Observability Analysis and Kalman Filter Applications for Error Estimation of SDINS Ground Alignment

USINGADAPTIVE FILTERS FOR GPS RECEIVERS

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

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

Wavelet Spectral Techniques for GPS Errors Reduction

Improvement of CEP Accuracy for Vehicles Re-entry Using INS/GPS/GNSS Integrated System