| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 721626 | IFAC Proceedings Volumes | 2007 | 6 Pages |
Abstract
New approach for modeling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on spacecraft 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
