|
|||||
|
|
| 卫星磁力矩器磁场效应仿真分析 | |
| 引用本文： | 邓佳欣,易忠,孟立飞,陈金刚,唐小金,王松. 卫星磁力矩器磁场效应仿真分析[J]. 航天器环境工程, 2016, 33(1): 52-57 |
| 作者姓名： | 邓佳欣 易忠 孟立飞 陈金刚 唐小金 王松 |
| 作者单位： | 北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;军械工程学院静电与电磁防护研究所, 石家庄 050003 |
| 基金项目： | 总装备部"十二五"预研基金项目 |
| 摘 要： | 磁力矩器是卫星上磁性较大的部件之一,局部的强磁场是影响卫星周围带电粒子分布的主要原因。为了定量分析磁力矩器与等离子体相互作用,文章基于磁场与运动粒子的耦合模型,利用有限元数值分析软件仿真了典型轨道航天器上磁力矩器工作时周围带电粒子入射轨迹变化及电荷(粒子数)分布。结果表明,受磁场作用,带电粒子在接近磁力矩器本体时会发生偏转,且偏转幅度随电子能量降低而增大;由磁场引起的这种偏转效应导致带电粒子不均匀入射到卫星内。 |
| 关 键 词： | 卫星 磁力矩器 空间等离子体 仿真分析 |
| 收稿时间： | 2015-06-30 |
| 修稿时间： | 2016-01-18 |
Simulation of magnetic effects of satellite magnetorquer |
|
| Deng Jiaxin,Yi Zhong,Meng Lifei,Chen Jin''gang,Tang Xiaojin and Wang Song. Simulation of magnetic effects of satellite magnetorquer[J]. Spacecraft Environment Engineering, 2016, 33(1): 52-57 | |
| Authors: | Deng Jiaxin Yi Zhong Meng Lifei Chen Jin''gang Tang Xiaojin Wang Song |
| Affiliation: | Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Institute for Electrostatic and Electromagnetic Protection, Ordnance Engineering College, Shijiazhuang 050003, China |
| Abstract: | The magnetorquer is an important component to provide relatively intense magnetic fields in a spacecraft. The produced intense magnetic fields play an important role in the distribution of ambient charged particles. In order to make a quantitative analysis of the interaction between the magnetorquer and the ambient plasma, the finite element method is used to simulate the charged particle traces when they fly towards the magnetorquer based on the coupling model of moving electrons in the magnetic field. From the simulation data, we can see notable deflections in the traces of the incoming charged particles when they pass by the magnetorquer, and this kind of deflection is increased as the incoming particle energy decreases. Because of the deflection, there exists an asymmetric distribution of the charged particles injected to a satellite. |
| Keywords: | satellite magnetorquer space plasma simulation analysis |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |
| 点击此处可从《航天器环境工程》浏览原始摘要信息 | |
| 点击此处可从《航天器环境工程》下载全文 | |