Fast converging with high accuracy estimates of satellite attitude and orbit based on magnetometer augmented with gyro, star sensor and GPS via extended Kalman filter

Fast converging with high accuracy estimates of satellite attitude and orbit based on magnetometer augmented with gyro, star sensor and GPS via extended Kalman filter

The primary goal of this work is to extend the work done in, Tamer (2009), to provide high accuracy satellite attitude and orbit estimates needed for imaging purposes and also before execution of spacecraft orbital maneuvers for the next Egyptian scientific satellite. The problem of coarse satellite...

Full description

Bibliographic Details
Main Author: Tamer Mekky Ahmed Habib
Format: Article
Language:English
Published: Elsevier 2011-12-01
Series:Egyptian Journal of Remote Sensing and Space Sciences
Subjects:
Fast convergence
Attitude
Orbit
High accuracy
Estimation
Magnetometer
Gyro
Star sensor GPS
Earth oblateness
Drag
Solar radiation
Residual dipole
Extended Kalman filter
Online Access:http://www.sciencedirect.com/science/article/pii/S1110982311000159

Internet

http://www.sciencedirect.com/science/article/pii/S1110982311000159

Similar Items