航天器环境工程2017，Vol.34Issue(4)：403-409,7.DOI:10.3969/j.issn.1673-1379.2017.04.011
航天器在轨释放安全性分析与仿真研究
Safety analysis and simulation of spacecraft on-orbit releasing
范高洁 1柏林厚 1魏传锋 1巩朝阳1
作者信息
- 1. 中国空间技术研究院载人航天总体部,北京 100094
- 折叠
摘要
Abstract
For the mission of spacecraft on-orbit releasing, dynamic and kinematic models are established for both the main spacecraft and the concomitant satellite in this paper. By analyzing the main force model that affects the releasing safety during the process, the closest distance between two spacecrafts can be calculated, under the condition of assuring the on-orbit safety of two spacecrafts. The software ADAMS is used for simulating the releasing process.关键词
在轨释放/安全性分析建模/ADAMS仿真Key words
on-orbit releasing/safety analysis and modeling/ADAMS simulation分类
航空航天引用本文复制引用
范高洁,柏林厚,魏传锋,巩朝阳..航天器在轨释放安全性分析与仿真研究[J].航天器环境工程,2017,34(4):403-409,7.
