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

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

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

Estimation of GPS Position Using Iterative Least Squares and Extended Kalman Filter

Multi-sensory data fusion for high performance attitude estimation

Attitude Determination and Control for CubeSats

Design and Implementation of Attitude Determination and Control Subsystem for Cube Satellites

Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems

Fuel and Time Optimize and Adaptive Control for Gravity Gradient Spacecraft

HIGH ACCURACY SPACECRAFT ORBIT PROPAGATOR VALIDATION