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Flywheel micro-vibration characters of a high resolution optical satellite
Li, L.; L. Y. Tan; L. Kong; H. B. Yang and D. Wang
2017
发表期刊Journal of Vibroengineering
卷号19期号:6
摘要According to the pictures of a sub-meter resolution optical satellite which were acquired on orbit, there is a phenomenon of jitter in the process of taking pictures. As the main attitude control component of the satellite, the flywheel will produce the disturbance in its normal work, which has great influence on the high resolution optical satellite. This paper has respectively researched the flywheel components' disturbance mechanism from four parts, including uneven rotator, rotator friction, bearing disturbance, foundation loose, and builds the mathematical model of disturbance to analyze the characteristics of disturbance. We have simulated and tested the flywheel components' disturbance. The disturbance force of flywheel components is 2 N magnitude and the torque of disturbance is 1.5 N.m magnitude in time domain. The flywheel's infrastructure should be more inflexible especially around 90-100 Hz. For this target high resolution optical satellite, there should be effective damping measures around 48.6 Hz, 190.4 Hz and 285.4 Hz to decrease the flywheel disturbance to guarantee the high precision of the satellite. The result would offer guidance for system optimization design and vibration isolation compensation of the later type of improved satellite or other same type of satellites.
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/181722/59007
专题中科院长春光机所知识产出
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GB/T 7714
Li, L.,L. Y. Tan,L. Kong,et al. Flywheel micro-vibration characters of a high resolution optical satellite[J]. Journal of Vibroengineering,2017,19(6).
APA Li, L.,L. Y. Tan,L. Kong,&H. B. Yang and D. Wang.(2017).Flywheel micro-vibration characters of a high resolution optical satellite.Journal of Vibroengineering,19(6).
MLA Li, L.,et al."Flywheel micro-vibration characters of a high resolution optical satellite".Journal of Vibroengineering 19.6(2017).
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