Survivability assessment of spacecraft impacted by orbit debris |
| |
Authors: | Di-qi Hu Bao-jun Pang Run-qiang Chi Zhang-chi Song Hao Wu |
| |
Affiliation: | Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Beijing Institute of Aerospace Automatic Control,100854,Beijing,China;Hypervelocity Impact Research Center,Harbin Institute of Technology,150080,Harbin,China;Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,130033,Changchun,China |
| |
Abstract: | 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. |
| |
Keywords: | Survivability Hypervelocity impact Orbit debris Ray method |
本文献已被 万方数据 等数据库收录! |
|