Configuration optimization and analysis of the parallel adjustment platform for Satellite Integrated Assembly

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.