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

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

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

Multi-sensory data fusion for high performance attitude estimation

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

Designing attitude controller for nano/pico satellites at detumbling mode using magnetic sensor and actuator

Attitude Determination and Control for CubeSats

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

Intelligent robust adaptive attitude controller for small satellites

STATE ESTIMATION OF AN INERTIALLY GUIDED AIR VEHICLE