DocumentCode :
3046363
Title :
Kinematics and simulations of space manipulator in three work modes
Author :
Zhang, Fuhai ; Fu, Yili ; Yan, Shibo ; Wang, Shuguo
Author_Institution :
State Key Lab. of Robot. & Syst., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
572
Lastpage :
577
Abstract :
In recent years, research on space robotics has attracted considerable attention. Kinematics of the free-flying or free-floating space manipulator system, including a spacecraft and a manipulator mounted on the spacecraft, is a significant problem. In free-floating work mode, the spacecraft will move freely in response to the disturbances caused by the manipulator motions. From the view of application, change of the spacecraft attitude for the space manipulator system is not desirable. Therefore, it is of significance to adopt the free-floating with zero-disturbance spacecraft attitude work mode. This paper presents an overview of the kinematics of the space manipulator system. Position and velocity kinematics solutions in three work modes are analyzed. The kinematics differences among the three work modes are formulated. The simulation results validate the effectiveness of the kinematics solutions in the three work modes.
Keywords :
aerospace control; manipulator kinematics; motion control; position control; space vehicles; velocity control; free floating space manipulator system; free flying space manipulator system; manipulator motions; position kinematics solutions; space manipulator; space robotics; spacecraft attitude; three work modes; velocity kinematics solutions; Aerospace electronics; Jacobian matrices; Joints; Kinematics; Manipulator dynamics; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5633417
Filename :
5633417
Link To Document :
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