DocumentCode
391138
Title
Local equilibrium controllability of the triaxial attitude control testbed
Author
Jinglai Shen ; McClamroch, N. Harris ; Bloch, Anthony M.
Author_Institution
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
Volume
1
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
528
Abstract
Local configuration controllability and local equilibrium controllability of the Triaxial attitude control testbed (TACT) are studied. The TACT is controlled only by a class of actuators referred to as shape actuators. This implies that there is a conserved quantity and there is a base body equilibrium manifold at each fixed shape. Thus, the TACT states are not small time locally controllable at equilibrium. But a weaker configuration controllability and equilibrium controllability property may be satisfied at an equilibrium. Important symmetric product formulas and properties are obtained. These properties explicitly show dynamic coupling and symmetry of the TACT. Based on these properties, local equilibrium controllability analysis is carried out for the TACT with fully actuated shape variables. Sufficient conditions for local equilibrium controllability are presented for three examples.
Keywords
aerospace test facilities; attitude control; controllability; space vehicles; symmetry; dynamic coupling; local configuration controllability; local equilibrium controllability; shape actuators; sufficient conditions; symmetric product formulas; symmetry; triaxial attitude control testbed; Actuators; Aerodynamics; Aerospace testing; Control systems; Controllability; Mathematics; Mechanical systems; Shape control; Space vehicles; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1184550
Filename
1184550
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