Micro-vibration Experiment and Analysis on Characteristic of Satellite Payload Isolation Device

被引：0
|
作者：
Luo J. [1 ]
Tan L. [1 ]
Luo M. [1 ]
Yin X. [1 ]
机构：
[1] Beijing Institute of Spacecraft System Engineering, Mechanical System Business Department, Beijing
来源：
Zhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosis | 2019年 / 39卷 / 03期
关键词：
Micro-vibration; Modal characteristic; Payload isolation device; Transmissibility characteristic; Vibration isolation effect;
D O I：
10.16450/j.cnki.issn.1004-6801.2019.03.030
中图分类号：
V476.2 [宇宙飞船];
学科分类号：
摘要：
Payload isolation device is a new design structure of high precision and high stability, which is adapting for the high resolution satellite optical payload with high precision and high stability working environment. It is an urgent problem to be solved that how to validate its characteristic effectively by ground test and quantitatively evaluate its vibration isolation effect. In order to test the modal characteristic and transmissibility characteristic of payload isolation device, a set of micro-vibration experiment system is designed and built, through which effective test data can be obtained. Through comparison and analysis, the vibration isolation effect of payload isolation device is quantified. The experimental investigation result provides important basic data and valuable engineering experience for the development of payload isolation device, and provides a wide range of reference value for the vibration isolation system design of satellite. © 2019, Editorial Department of JVMD. All right reserved.
引用
收藏
页码：659 / 678
页数：19
相关论文
共 10 条
  • [1] Zhang Y., Zhang J.R., Zhai G., Et al., High imaging performance of optical payload by vibration isolation system, AAIA Guidance, Navigation, and Control Conference 2012, (2012)
  • [2] Oh H.U., Izawa K., Taniwaki S., Development of variable-damping isolator using bio-metal fiber for reaction wheel vibration isolation, Smart Materials and Structures, 14, 5, pp. 928-933, (2005)
  • [3] Wang J., Zhao S., Wu D., Et al., A test method of dynamic parameters of vibration isolators, Journal of Vibration Engineering, 27, 6, pp. 885-892, (2014)
  • [4] Wang J., Zhao S., Wu D., Et al., The mechanism study of a micro-vibration isolator based on viscous fluid, Journal of Vibration Engineering, 28, 2, pp. 237-247, (2015)
  • [5] Allen J.B., Vibration isolator for large space telescopes, Joural of Spacecraft and Rockets, 43, pp. 45-53, (2006)
  • [6] Wang G., Zhou D., Zhao Y., Data analysis of micro-vibration on-orbit measurement for remotesensing satellite, Journal of Astronautics, 36, 3, pp. 261-267, (2015)
  • [7] Pang S., Pan T., Mao Y., Et al., Study and verification of micro-vibration test for a satellite, Spacecraft Environment Engineering, 33, 3, pp. 305-311, (2016)
  • [8] McMickell M.B., Kreider T., Hansen E., Et al., Optical payload isolation using the miniature vibration isolation system, Industrial and Commercial Application of Smart Structures Technologies, (2007)
  • [9] Zhang Q., Wang G., Zheng G., Micro-vibration attenuation methods and key techniques for optical remote sensing satellite, Journal of Astronautics, 36, 2, pp. 125-132, (2015)
  • [10] Zhou D., Cao R., Zhao Y., Micro-vibration measurement and analysis of a series of remote sensing satellites in-orbit, Spacecraft Environment Engineering, 30, 6, pp. 627-630, (2013)
1