| 航天器在轨释放安全性分析与仿真研究 |
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| 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. |
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| 作者姓名： | 范高洁 柏林厚 魏传锋 巩朝阳 |
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| 作者单位： | 中国空间技术研究院 载人航天总体部, 北京 100094 |
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| 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。
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| 关 键 词： | 在轨释放 安全性分析建模 ADAMS仿真 |
| 收稿时间： | 2017/5/30 0:00:00 |
| 修稿时间： | 2017/6/11 0:00:00 |
Safety analysis and simulation of spacecraft on-orbit releasing |
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| FAN Gaojie,BO Linhou,WEI Chuanfeng,GONG Chaoyang.Safety analysis and simulation of spacecraft on-orbit releasing[J].Spacecraft Environment Engineering,2017,34(4):403-409. |
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| Authors: | FAN Gaojie BO Linhou WEI Chuanfeng GONG Chaoyang |
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| Institution: | Institute of Manned Space System Engineering, China Academy of Space Technology, Beijing 100094, China |
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| 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. |
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| Keywords: | on-orbit releasing safety analysis and modeling ADAMS simulation |
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