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A method for analyzing the shock response characteristics of a satellite with frame-panel configuration | |
2021 | |
发表期刊 | 中国科学(物理学 力学 天文学) (IF:0.5[JCR-2023],0.6[5-Year]) |
ISSN | 1674-7275 |
EISSN | 2095-9478 |
卷号 | 51期号:1 |
发表状态 | 已发表 |
DOI | 10.1360/SSPMA-2020-0244 |
摘要 | The high magnitude and frequency of the shock load generated by the dynamic action of a satellite with a frame-panel configuration Will lead to equipment damage on the satellite. However; the mechanical properties of the plate-rod coupling will result in a significant difference in the transmission and attenuation characteristics of the shock load. Moreover, the accuracy of the response analysis and evaluation of the key components are lacking. In this article, both direct integration and modal superposition methods are used to analyze the transient response of a satellite with frame panel configuration. Furthermore, the advantages and disadvantages of the two methods are compared, and the possible factors affecting the precision and duration of the calculation results are presented. Simulation data show. that the effect of time is very short for this type of explosion shock, and high-frequency modes require a larger proportion of the response provoked. Although the modal superposition method can solve the problem of a large amount of calculation and long computation time by modal order truncation and adjusting the time step, high-order modes are easily ignored; which affect the accuracy of the calculation results. The direct integration method is more suitable for the shock response analysis of the satellite with frame-panel configuration. |
关键词 | satellite with frame-panel configuration shock response analysis direct integration method modal superposition method |
收录类别 | ESCI ; 北大核心 |
语种 | 中文 |
WOS研究方向 | Astronomy & Astrophysics ; Physics |
WOS类目 | Astronomy & Astrophysics ; Physics, Multidisciplinary |
WOS记录号 | WOS:000608584700016 |
出版者 | SCIENCE PRESS |
原始文献类型 | Article |
引用统计 | 正在获取...
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文献类型 | 期刊论文 |
条目标识符 | https://kms.shanghaitech.edu.cn/handle/2MSLDSTB/125645 |
专题 | 信息科学与技术学院_特聘教授组_林宝军组 |
通讯作者 | Lin, BJ |
作者单位 | 1.Chinese Acad Sci, Innovat Acad Microsatellites, Shanghai 201203, Peoples R China; 2.Shanghai Engn Ctr Microsatellites, Shanghai 201203, Peoples R China; 3.ShanghaiTech Univ, Sch Informat Sci & Technol, Shanghai 201210, Peoples R China |
通讯作者单位 | 信息科学与技术学院 |
推荐引用方式 GB/T 7714 | An, Y,Lin, BJ,Liu, JW. A method for analyzing the shock response characteristics of a satellite with frame-panel configuration[J]. 中国科学(物理学 力学 天文学),2021,51(1). |
APA | An, Y,Lin, BJ,&Liu, JW.(2021).A method for analyzing the shock response characteristics of a satellite with frame-panel configuration.中国科学(物理学 力学 天文学),51(1). |
MLA | An, Y,et al."A method for analyzing the shock response characteristics of a satellite with frame-panel configuration".中国科学(物理学 力学 天文学) 51.1(2021). |
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