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空间碎片碰撞风险评估模型及其应用

梁彦刚 秦政

国防科技大学学报2017,Vol.39Issue(6):19-24,6.
国防科技大学学报2017,Vol.39Issue(6):19-24,6.DOI:10.11887/j.cn.201706004

空间碎片碰撞风险评估模型及其应用

Space debris impact risk assessment model and its application

梁彦刚 1秦政1

作者信息

  • 1. 国防科技大学空天科学学院,湖南长沙 410073
  • 折叠

摘要

Abstract

A space debris impact risk assessment model was developed on the basis of the existing space debris environment model.The framework of the model consists of space debris environment module,spacecraft model module,geometry shading module and impact probability module.The impact risk by space debris for three generic spacecraft geometries were offered by IADC in order to validate different models.The result was proved to be effective by comparing with other models.The space debris impact risk for the spacecraft of cube was assessed and analyzed using the developed risk assessment model,and the effect of orbital altitude,inclination and attitude parameters to the space debris impact risk was presented.

关键词

空间碎片/风险评估/航天器/几何遮挡

Key words

space debris/risk assessment/spacecraft/geometry shading

分类

航空航天

引用本文复制引用

梁彦刚,秦政..空间碎片碰撞风险评估模型及其应用[J].国防科技大学学报,2017,39(6):19-24,6.

基金项目

国家自然科学基金资助项目(51405499) (51405499)

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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