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Optimal design of the main support structure of space camera aiming at the RMS value of random response
Li, L.; L. Y. Tan; D. Wang and H. B. Yang
2017
发表期刊Journal of Vibroengineering
卷号19期号:4
摘要To explore the optimal design method for main support structure of micro satellite, this paper proposed a method targeting the random acceleration response RMS value of the space camera installation position when design the main support structure of LQ-video satellite in Jilin-1 group satellites. Camera main support structure optimization mathematical model was established, and the thickness and flexible beam position of the flexible beam support structure has been optimized in the establishment of the optimization mathematical model. When the flexible beam thickness is 2.5 mm, and the distance between it and the support structure mounting surface is 94.5 mm, the camera installation point acceleration response root mean square ( RMS) value is minimal. Engineering analysis showed that the maximal random response RMS of the camera installation point is 19.6 grms and the maximal relative magnification is 0.93. The camera mechanics test showed that the maximal relative error of finite element analysis and experimental measurements is 4.0 % and the maximal relative magnification of the response is 1.2 which is less than the overall index 1.5. It proved that the optimization method is effective and feasible.
收录类别sci ; ei
语种英语
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/59009
专题中科院长春光机所知识产出
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Li, L.,L. Y. Tan,D. Wang and H. B. Yang. Optimal design of the main support structure of space camera aiming at the RMS value of random response[J]. Journal of Vibroengineering,2017,19(4).
APA Li, L.,L. Y. Tan,&D. Wang and H. B. Yang.(2017).Optimal design of the main support structure of space camera aiming at the RMS value of random response.Journal of Vibroengineering,19(4).
MLA Li, L.,et al."Optimal design of the main support structure of space camera aiming at the RMS value of random response".Journal of Vibroengineering 19.4(2017).
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