An engineering vector-like approach to attitude kinematics and nominal attitude state tracking control.
In dealing with rigid body three-dimensional rotational motion, one is inevitably led to face the fact that rotations are not vector quantities. They may, however, be treated as such when the angle of rotation is (very) small. In this context, i.e. the infinitesimal case analysis, the time derivativ...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | Portuguese |
| Published: |
Instituto Tecnológico de Aeronáutica
2002
|
| Subjects: | |
| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2541 |