On Stability of the Linearized Spacecraft Attitude Control System
Dynamical Systems
2015-04-02 v1
Abstract
This note is concerned with the stability and stabilization of the linearized spacecraft attitude control system. Necessary and sufficient conditions are respectively provided to guarantee that the considered systems are polynomially stable and stable in the Lyapunov sense. These two classes of conditions guarantee that the linearized spacecraft attitude control system can be respectively stabilized semi-globally and globally by saturated linear state feedback.
Cite
@article{arxiv.1504.00114,
title = {On Stability of the Linearized Spacecraft Attitude Control System},
author = {Bin Zhou},
journal= {arXiv preprint arXiv:1504.00114},
year = {2015}
}
Comments
7 pages