| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 9823227 | Acta Astronautica | 2005 | 12 Pages |
Abstract
For an absolute worst case the attitude determination error can be held below 2â. In a nominal case it is better than 1â.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Pontus Appel,