DocumentCode :
425146
Title :
Orbit dynamics and kinematics with full quaternions
Author :
Andreis, Davide ; Canuto, Enrico S.
Author_Institution :
Dipt. di Autom. e Inf., Politecnico di Torino, Italy
Volume :
4
fYear :
2004
fDate :
June 30 2004-July 2 2004
Firstpage :
3660
Abstract :
Full quaternions constitute a compact notation for describing the generic motion of a body in the space. One of the most important results about full quaternions is that they can be partitioned into a unit quaternion (which describes the orientation with respect to a suitable reference), and a modulus (which represents the translational motion along the direction indicated by the unit quaternion). Since vectors and scalars are also full quaternions, the equations of motion of the body can be rewritten in quaternion form. In this paper the orbit dynamics and kinematics of a point mass moving in the space are transformed in quaternion form. Simple application examples are also presented.
Keywords :
artificial satellites; attitude control; celestial mechanics; dynamics; kinematics; matrix algebra; vectors; equations of motion; full quaternions; orbit dynamics; orbit kinematics; translational motion; vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2004. Proceedings of the 2004
Conference_Location :
Boston, MA, USA
ISSN :
0743-1619
Print_ISBN :
0-7803-8335-4
Type :
conf
Filename :
1384480
Link To Document :
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