@inproceedings{d2c1c751c220487b80421f216b8efcf5,
title = "Dynamic modeling and simulation of thermal vacuum test platform for spacecrafts docking",
abstract = "Spacecraft docking technology play an important role in the aerospace technology. Due to the spacecraft with variable attitude, so the docking process is complex and variable. Therefore, a comprehensive and systematic study of the spacecraft docking process is very necessary. This paper proposed the equivalent-mass principle and the test platform of spacecraft docking is established based on the equivalent-mass principle through the analysis of environmental characteristics of thermal vacuum. Furthermore, dynamic simulation on the test platform and the results data of simulation is obtained. These studies will facilitate the understanding of the spacecraft docking process and provide solid theoretical foundation for further study.",
keywords = "Buffering characteristic, Dynamic modeling, Dynamic simulation, Spacecraft docking, Thermal vacuum",
author = "Yanhe Zhu and Jie Zhao and Yu Zhang",
note = "Publisher Copyright: {\textcopyright} 2014. The authors - Published by Atlantis Press.; 2014 International Conference on Mechatronics, Electronic, Industrial and Control Engineering, MEIC 2014 ; Conference date: 15-11-2014 Through 17-11-2014",
year = "2014",
doi = "10.2991/meic-14.2014.32",
language = "英语",
series = "2014 International Conference on Mechatronics, Electronic, Industrial and Control Engineering, MEIC 2014",
publisher = "Atlantis Press",
pages = "143--146",
booktitle = "2014 International Conference on Mechatronics, Electronic, Industrial and Control Engineering, MEIC 2014",
}