Abstract
Transportation is an important part of spacecraft launching mission. Container is the most important equipment to ensure transportation tasks. In order to overcome the shortcomings of the physical dynamic test of spacecraft container, based on the theory of rigid-flexible coupling dynamics, the dynamic model of the container-based spacecraft transport system is established. External excitation of the dynamic model is determined by obtaining track spectrum and identifying track condition. Using modular design, C/S architecture and navigation process, a simulation platform is built, which is designed for whole container lifecycle used in spacecraft missions.
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