DocumentCode :
645927
Title :
A new approach to the solution of free rigid body motion for attitude maneuvers
Author :
Pagnozzi, Daniele ; Maclean, Craig ; Biggs, James D.
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Adv. Space Concepts Lab., Univ. of Strathclyde, Glasgow, UK
fYear :
2013
fDate :
17-19 July 2013
Firstpage :
664
Lastpage :
669
Abstract :
A Hamiltonian formulation of free rigid body motion defined on the Special Unitary Group SU(2) is used to integrate the system to obtain a convenient quaternion representation for attitude engineering applications. Novel content of this paper concerns applying a modern approach, based on geometric control theory to obtain the kinematic solution in an elegant and compact form. Moreover, this integration leads to an attitude representation which is not Euler-angle-like, thus enhancing its applicability (e.g. to attitude motion design).
Keywords :
attitude control; motion control; space vehicles; Hamiltonian formulation; Special Unitary Group; attitude engineering applications; attitude maneuvers; attitude motion design; attitude quaternion representation; free rigid body motion; geometric control theory; kinematic solution; Angular velocity; Attitude control; Equations; Jacobian matrices; Quaternions; Space vehicles; Tracking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 2013 European
Conference_Location :
Zurich
Type :
conf
Filename :
6669123
Link To Document :
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