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 - Egyptian Knowledge Bank - troweb

23240

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

Article

Last updated: 04 Jan 2025

Overview Similar Items

Article

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

Article

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

Article

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

Article

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

Article

Multi-sensory data fusion for high performance attitude estimation

Article

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

Article

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

Article

A TERRESTRIAL STRAPDOWN NAVIGATION ALGORITHM

Article

HIGH ACCURACY SPACECRAFT ORBIT PROPAGATOR VALIDATION

Article

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