Controllability of Spacecraft Using Only Magnetic Torques
Optimization and Control
2016-03-24 v1
Abstract
Spacecraft attitude control using only magnetic torques is a time-varying system. Many designs were proposed using LQR and H-infinity formulations. The existence of the solutions depends on the controllability of the linear time-varying systems which has not been established. In this paper, we will derive the conditions of the controllability for this linear time-varying systems.
Keywords
Cite
@article{arxiv.1507.06963,
title = {Controllability of Spacecraft Using Only Magnetic Torques},
author = {Yaguang Yang},
journal= {arXiv preprint arXiv:1507.06963},
year = {2016}
}
Comments
10 pages