Dynamic Modeling and Simulation of Thermal Vacuum Test Platform for Spacecrafts Docking

DOI

10.2991/meic-14.2014.32How to use a DOI?

Keywords

spacecraft docking; thermal vacuum; buffering characteristic; dynamic modeling; dynamic simulation

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.

Copyright

© 2014, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yanhe Zhu
AU  - Yu Zhang
AU  - Jie Zhao
PY  - 2014/11
DA  - 2014/11
TI  - Dynamic Modeling and Simulation of Thermal Vacuum Test Platform for Spacecrafts Docking
BT  - Proceedings of the 2014 International Conference on Mechatronics, Electronic, Industrial and Control Engineering
PB  - Atlantis Press
SP  - 143
EP  - 146
SN  - 2352-5401
UR  - https://doi.org/10.2991/meic-14.2014.32
DO  - 10.2991/meic-14.2014.32
ID  - Zhu2014/11
ER  -