| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 709133 | IFAC Proceedings Volumes | 2013 | 5 Pages |
Abstract
In the paper the attitude stabilization system of the unstable flexible launcher with saturating input is considered. It is demonstrated that due to actuator saturation the system performance can significantly degrade. The analytical-numerical method is applied to demonstrate possibility of hidden oscillations and localize their attractor.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
