| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10680858 | Acta Astronautica | 2014 | 12 Pages |
Abstract
⺠Very flexible structures are considered in an orbital environment. ⺠Time varying moment of inertia due to flexibility are studied. ⺠Attitude control robustness to structural uncertainties is addressed.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
P. Gasbarri, R. Monti, C. De Angelis, M. Sabatini,