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 DOI: 10.12126/see.2017.04.011
引用本文: 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 DOI: 10.12126/see.2017.04.011
FAN Gaojie,. Safety analysis and simulation of spacecraft on-orbit releasing[J]. Spacecraft Environment Engineering, 2017, 34(4): 403-409. DOI: 10.12126/see.2017.04.011
Citation: FAN Gaojie,. Safety analysis and simulation of spacecraft on-orbit releasing[J]. Spacecraft Environment Engineering, 2017, 34(4): 403-409. DOI: 10.12126/see.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

  • 摘要: 针对航天器舱内在轨释放任务,文章建立了大型航天器与伴随卫星的动力学模型和运动学模型,并分析了影响释放安全性的主要因素;从保证航天器在轨安全的角度,得到描述释放安全性的最小相对距离计算方法,并利用ADAMS软件对航天器在轨释放过程进行了仿真研究。

     

    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.

     

/

返回文章
返回