Design and experiment of a large-scale space micro-vibration simulator

被引:2
|
作者
Zhu, He [1 ,2 ]
He, Shuai [1 ,3 ]
Shen, Junli [1 ]
Xia, Mingyi [1 ]
Qin, Chao [1 ]
Wang, Xiaoming [1 ]
Sun, Xiangyang [1 ,2 ]
Xu, Zhenbang [1 ]
机构
[1] Chinese Acad Sci, Changchun Inst Opt Fine Mech & Phys, Space Robot Engn Ctr, Innovat Lab Space Robot Syst, Changchun, Peoples R China
[2] Univ Chinese Acad Sci, Beijing, Peoples R China
[3] Chinese Acad Sci, Changchun Inst Opt Fine Mech & Phys, 3888 Dong Nanhu Rd, Changchun 130033, Jilin, Peoples R China
基金
加拿大自然科学与工程研究理事会;
关键词
space micro-vibration; simulator; transfer function; ISOLATION SYSTEM; CAMERA;
D O I
10.1177/10775463221150825
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
To solve the problems of difficult vibration sources simulation in the ground test of the on-orbit optical load, a multi-dimensional micro-vibration simulator based on the improved Gough-Stewart platform was designed, which can effectively reproduce the characteristics of wide frequency distribution and small vibration magnitude of space micro-vibration. The analytical formula was derived by using the virtual frequent principle and the Newton-Euler equation for the natural frequency of the system, and the simulator's configuration was optimized. The structure of legs was designed and optimized according to the optimal configuration parameters. Finally, the micro-vibration simulator was tested, and the test results showed that the output bandwidth of the simulator was 5-300 Hz and the maximum magnitude error was 8%, thus demonstrating the multi-dimensional micro-vibration simulation platform has the characteristics of large frequent bandwidth, high load carrying capacity, and small vibration magnitude.
引用
收藏
页码:740 / 752
页数:13
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