DocumentCode
641217
Title
Configuration optimization and analysis of the parallel adjustment platform for Satellite Integrated Assembly
Author
Jiantao Yao ; Guowang Wu ; Yongsheng Zhao
Author_Institution
Parallel Robot & Mechatron. Syst. Lab. of Hebei Province, Yanshan Univ., Qinhuangdao, China
fYear
2013
fDate
29-31 July 2013
Firstpage
317
Lastpage
320
Abstract
For the real-time adjustment of the Satellite Integrated Assembly, Stewart platform-based mechanism is adopted. This paper presents the optimization design of the parallel adjustment platform for satellite integrated assembly and the analysis of the configuration is optimized. The actual working conditions and real limit of system size is considered when optimizing the configuration. Placing the moving platform to the limit postures when analysis the force. The contents of this paper possess theoretical significance and engineering value for the development of the parallel adjustment platform for satellite integrated assembly.
Keywords
artificial satellites; optimisation; robotic assembly; Stewart platform-based mechanism; moving platform; optimization; parallel adjustment platform; satellite integrated assembly; Assembly; Force; Joints; Kinematics; Optimization; Satellites; Vectors; Optimization Analysis; Parallel adjustment platform; Satellite Integrated Assembly;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Informatics (INDIN), 2013 11th IEEE International Conference on
Conference_Location
Bochum
Type
conf
DOI
10.1109/INDIN.2013.6622902
Filename
6622902
Link To Document