In this paper the attitude control system of a small spacecraft is considered. The readings of airborne magnetometers and satellite Global Positioning System (GPS) data are used for determination of the parameters of object motion. Such choice of measurements aims to raise estimation stability against disturbances of the magnetic storm type. At considerably undefined initial conditions for estimation of the desired parameters of motion, we use the algorithm with an extended convergence domain.
Spacecraft attitude control using the magnetic-GPS dataware system. I
Journal of Automation and Information Sciences ; 33 , 1 ; 69-75
2001
7 Seiten, 20 Quellen
Article (Journal)
English
On Spacecraft Magnetic Attitude Control
AIAA | 2018
|Fault-Tolerant Spacecraft Magnetic Attitude Control
British Library Conference Proceedings | 2013
|Spacecraft Attitude Control Using Magnetic and Mechanical Actuation
Online Contents | 2015
|Magnetic attitude control for geosynchronous spacecraft
Tema Archive | 1978
|