| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 4637074 | Applied Mathematics and Computation | 2006 | 4 Pages |
Abstract
Satellite orientation is usually expressed in terms of euler rotations about the three principal axes. Usually, the orientation is determined using the measurements of at least two known vectors. A variant to this problem is considered in this note.
Related Topics
Physical Sciences and Engineering
Mathematics
Applied Mathematics
Authors
M.P. Ramachandran,