DocumentCode :
475040
Title :
Dynamics of a 3-DOF parallel mechanism used for orientation applications
Author :
Itul, T. ; Pisla, D.
Author_Institution :
Tech. Univ. of Cluj-Napoca, Cluj-Napoca
Volume :
2
fYear :
2008
fDate :
22-25 May 2008
Firstpage :
398
Lastpage :
403
Abstract :
In the paper dynamic studies regarding the possibility to use a 3-DOF parallel mechanism for the TV satellite antenna orientation or sun tracker are presented. The advantage to use a parallel mechanism consists of their good stiffness, very high accuracy and their capability to manipulate heavy loads. The algorithms for the kinematic models are solved. Dynamic equations are obtained by using the Newton-Euler formalism in two steps. The first step is to determine the relations between the spherical joint reaction forces and the kinematic parameters of the mobile platform. The second step is to determine the generalized active torques. Using a numerical and graphical simulation, the diagrams for the dynamics representation are computed.
Keywords :
artificial satellites; manipulator dynamics; satellite antennas; 3-DOF parallel mechanism dynamics; Newton-Euler formalism; TV satellite antenna orientation; heavy loads manipulation; mobile platform; spherical joint reaction forces; sun tracker; Aerodynamics; Artificial satellites; Earth; Equations; Lagrangian functions; Robot kinematics; Satellite antennas; Satellite broadcasting; Sun; TV broadcasting;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Automation, Quality and Testing, Robotics, 2008. AQTR 2008. IEEE International Conference on
Conference_Location :
Cluj-Napoca
Print_ISBN :
978-1-4244-2576-1
Electronic_ISBN :
978-1-4244-2577-8
Type :
conf
DOI :
10.1109/AQTR.2008.4588862
Filename :
4588862
Link To Document :
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