| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 716076 | IFAC Proceedings Volumes | 2010 | 6 Pages |
Abstract
New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on communication satellite attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
