中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Survivability assessment of spacecraft impacted by orbit debris

文献类型:期刊论文

作者D.-q. Hu,B.-j. Pang,R.-q. Chi,Z.-c. Song and H. Wu
刊名Defence Technology
出版日期2020
页码10
ISSN号22149147
DOI10.1016/j.dt.2020.06.003
英文摘要To help optimize the spacecraft design and reduce the risk of spacecraft mission failure, a new approach to assess the survivability of spacecraft in orbit is presented here, including the following three steps: 1) Sensitivity Analysis of spacecraft. A new sensitivity analysis method, a ray method based on virtual outer wall, is presented here. Using rays to simulate the debris cloud can effectively address the component shadowing issues. 2) Component Vulnerability analysis of spacecraft. A function "Component functional reduction degree Component physical damage degree" is provided here to clearly describe the component functional reduction. 3) System-level Survivability Assessment of spacecraft. A new method based on expert knowledge reasoning, instead of traditional artificial failure tree method, is presented here to greatly improve the efficiency and accuracy of calculation. 2020 The Authors
URL标识查看原文
源URL[http://ir.ciomp.ac.cn/handle/181722/64936]  
专题中国科学院长春光学精密机械与物理研究所
推荐引用方式
GB/T 7714
D.-q. Hu,B.-j. Pang,R.-q. Chi,Z.-c. Song and H. Wu. Survivability assessment of spacecraft impacted by orbit debris[J]. Defence Technology,2020:10.
APA D.-q. Hu,B.-j. Pang,R.-q. Chi,Z.-c. Song and H. Wu.(2020).Survivability assessment of spacecraft impacted by orbit debris.Defence Technology,10.
MLA D.-q. Hu,B.-j. Pang,R.-q. Chi,Z.-c. Song and H. Wu."Survivability assessment of spacecraft impacted by orbit debris".Defence Technology (2020):10.

入库方式: OAI收割

来源:长春光学精密机械与物理研究所

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