DocumentCode
3174468
Title
Development of a General 2-DOF Space Module
Author
Zhiyu, Shao ; Hanxu, Sun ; Qingxuan, Jia ; Ping, Ye ; Yuesheng, Tan
Author_Institution
Sch. of Mech. Eng. & Autom., Beijing Univ. of Aeronaut. & Astronaut.
fYear
2006
fDate
Oct. 2006
Firstpage
1002
Lastpage
1007
Abstract
This paper presents the concept of a general two degrees-of-freedom space module or TODOM. General TODOM is made up of three basic modules: one link module and two revolving modules. The reliability of the TODOM is improved by mutual backup of the control systems of the two revolving modules. Every revolving module corresponds to one degree-of-freedom (DOF). The two axes of the revolving modules can be configured to different orientations or positions by specific design of the mechanical interfaces between the three basic modules. Several such differently configured TODOMs can be assembled into some needed kinds of space manipulators that have even numbered DOF. By using integration design method, the mass and volume of the TODOM is dramatically reduced, and the system reliability of the manipulator can be improved. The rationality and feasibility of the TODOM concept is testified by the development of a 2-DOF wrist whose two joint axes are orthogonal
Keywords
aerospace robotics; manipulator dynamics; reliability; general 2-DOF space module; integration design method; mechanical interfaces; space manipulators; Control systems; Design automation; Hardware; Manipulators; Mechanical engineering; Orbital robotics; Reluctance motors; Robotic assembly; Robotics and automation; Satellites; 2-DOF; Integration; Space manipulator; Space module; TODOM;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Robots and Systems, 2006 IEEE/RSJ International Conference on
Conference_Location
Beijing
Print_ISBN
1-4244-0259-X
Electronic_ISBN
1-4244-0259-X
Type
conf
DOI
10.1109/IROS.2006.281782
Filename
4058494
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