摘要
研究在某些假设条件下绳系卫星展开及剪断过程。根据动量矩守恒和力平衡方程得到一代数方程，用于求解系统展开及剪断后的轨道参数。计算结果表明：绳系卫星系统展开及剪断后，轨道参数将发生变化。
The process of deployment and cut -off of a tethered satellite system is studied under some assumption conditions. According to the moment of momentum conservation and force-balance, the algebraic equation is obtained to seek the solution of the orbital parameters of the system after deployment and cut-off. The calculation results show the changes of the parameters.
出处
《哈尔滨工业大学学报》
EI
CAS
CSCD
北大核心
1995年第1期97-100,共4页
Journal of Harbin Institute of Technology
关键词
卫星
绳系卫星
轨道动力学
轨道参数
Tethered satellite system
orbital dynamics
orbital parameter
