Massive module redocking is a key technology of space station on-orbit assembly, due to test condition limit, it is difficult to perform effective experiment on the ground. In order to simulate the assembly process, here taking a simplified four rigid bodies space station model as an example, first, its dynamic equation is established based on Kane method, then numerical simulation compared to other methods is provided to verify model validation.
Simulation and Analysis of Space Station Redocking
2014
7 Seiten
Conference paper
English
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