卫星飞轮隔振与吸振联合减振系统设计

虞自飞; 周徐斌; 申军烽; 周春华

doi:10.3788/OPE.20142204.0897

您当前的位置：

首页 >

文章列表页 >

卫星飞轮隔振与吸振联合减振系统设计

微纳技术与精密机械 | 更新时间：2020-08-13

- 卫星飞轮隔振与吸振联合减振系统设计
- Design of joint vibration reduction system combined isolation and absorbtion for flywheel
- 光学精密工程 2014年22卷第4期页码：897-903
- 作者机构：
  
  上海卫星工程研究所空间机热一体化技术实验室上海,200240
- 作者简介：
- 基金信息：
  
  基于光纤测量的航天器健康监测项目()
- DOI：10.3788/OPE.20142204.0897
  中图分类号： V416.1;V474.1
- 收稿日期：2013-07-31，
  
  修回日期：2013-09-21，
  
  纸质出版日期：2014-04-25
- 稿件说明：
移动端阅览
虞自飞, 周徐斌, 申军烽等. 卫星飞轮隔振与吸振联合减振系统设计[J]. 光学精密工程, 2014,22(4): 897-903

YU Zi-fei, ZHOU Xu-bin, SHEN Jun-feng etc. Design of joint vibration reduction system combined isolation and absorbtion for flywheel[J]. Editorial Office of Optics and Precision Engineering, 2014,22(4): 897-903
虞自飞, 周徐斌, 申军烽等. 卫星飞轮隔振与吸振联合减振系统设计[J]. 光学精密工程, 2014,22(4): 897-903 DOI： 10.3788/OPE.20142204.0897.

YU Zi-fei, ZHOU Xu-bin, SHEN Jun-feng etc. Design of joint vibration reduction system combined isolation and absorbtion for flywheel[J]. Editorial Office of Optics and Precision Engineering, 2014,22(4): 897-903 DOI： 10.3788/OPE.20142204.0897.

摘要

分析了抑制卫星飞轮振动的方法，提出了隔振为主、吸振为辅的联合减振方案。研究了会聚式隔振系统参数对其减振性能的影响；针对会聚式隔振系统存在的不足，提出了圆周分布式吸振方法和相应的吸振系统，分析表明会聚式隔振系统在4个方向的隔振效率达90%以上。根据会聚式隔振系统在

平动方向隔振效率较低的问题，建立了会聚式隔振和圆周分布式吸振的联合减振系统仿真模型。仿真结果表明，联合减振系统较单纯的隔振系统在

平动方向减振效率提高近50%，且不改变其他方向的减振性能。因此，联合减振设计方法合理可行，适用于卫星飞轮等主要振源的振动抑制，并为飞轮联合减振系统的工程化设计提供了理论支持。

Abstract

The methods to reduce the vibration of a satellite flywheel were analyzed

and a joint vibration reduction scheme was proposed by combined vibration isolation and vibration absorbing. The effect of the parameters of assembled isolators on its vibration reduction was researched. According to the shortcomings of the system

the circumferential distributed absorbing method and a corresponding system were proposed to reduce the vibration of the flywheel. The simulation shows that the vibration response of main structure subjected to external force dissipates by 90% in all directions except

direction. Then

circumferential distributed absorbers were designed to improve the performance of assembled isolators in

direction

and a simulation model of the joint vibration reduction was also established. Compared with unsophisticated isolators

the conclusion indicates that the performance of the joint vibration reduction is nearly improved 50% in

direction. Consequently

the joint vibration reduction scheme is suitable for reducing the vibration response of flywheel and is proved to be effective and practical in the vibration control for other vibration sources in satellites.

关键词

Keywords

references

LIU K CH, MAGHAMI P. Reaction wheel disturbance modeling, jitter analysis, and validation tests for solar dynamics observatory[C]. AIAA Guidance, Navigation and Control Conference, 2008:18-21.

MILLER S E, KIRCHMAN P, SUDEY J. Reaction wheel operational impacts on the GOES-N jitter environment[C]. AIAA Guidance, Navigation and Control Conference, 2007:20-23.

FIRTH J, BLACK J. Vibration interaction in a multiple flywheel system[D]. American:Air Force Institute of Technology Air University, 2011.

BRONOWICKI A J. Vibration isolator for large space telescopes[C]. 45th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics & Materials Confer., 2004:19-22.

刘天雄, 范本尧, 杨慧. 卫星飞轮扰振控制技术[J]. 航天器工程, 2009, 18(1):53-60. LIU T X, FAN B Y, YANG H. Research on vibration disturbance control of momentum wheel[J]. Spacecraft Engineering, 2009, 18(1):53-60.(in Chinese)

HYUN-UNG O, SHIGEMUNE T. Flywheel vibration isolation test using a variable-damping isolator[J].Smart Mater.Struct., 2006, 15(2):365-370.

ZHANG Y W, FANG B, CHEN Y. Vibration isolation performance evaluation of the discrete whole-spacecraft vibration isolation platform for flexible spacecrafts[J]. Meccanica, 2012, 47:1185-1195.

DAVIS L P, WILSON J F, JEWELL R E, et al.. Hubble space telescope reaction wheel assemble vibration isolation system[C]. NASA Workshop on Structure Dynamics and Control Interaction of Flexible Structures, G. C. Marshall Space Flight Center, 1986:57-64.

PENDERGAST K J, SCHAUWECKER C J. Use of a passive reaction wheel jitter isolation system to meet the advanced X-ray astrophysics facility imaging performance requirements[J]. NASA/CR, 1998, 207926:1078-1094.

朱石坚, 楼京俊. 振动理论与隔振技术[M]. 北京: 国防工业出版社, 2008:191-209. ZHU SH J, LOU J J. Vibration Theory and Vibration Isolation[M]. Beijing: National Defense Industry Press. 2008:191-209.(in Chinese)

浏览量

684

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

飞轮组件微振动对高分辨率光学卫星光轴的影响

储能/姿控一体化飞轮能耗试验研究

单轴飞轮储能与姿态控制系统误差分析