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空间主动隔振系统的脐带线刚度测试装置

范涛 任维佳 李宗峰

范涛, 任维佳, 李宗峰. 空间主动隔振系统的脐带线刚度测试装置[J]. 机械科学与技术, 2016, 35(7): 1144-1148. doi: 10.13433/j.cnki.1003-8728.2016.0726
引用本文: 范涛, 任维佳, 李宗峰. 空间主动隔振系统的脐带线刚度测试装置[J]. 机械科学与技术, 2016, 35(7): 1144-1148. doi: 10.13433/j.cnki.1003-8728.2016.0726
Fan Tao, Ren Weijia, Li Zongfeng. A Stiffness Testing System for the Umbilical of the Active Vibration Isolation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2016, 35(7): 1144-1148. doi: 10.13433/j.cnki.1003-8728.2016.0726
Citation: Fan Tao, Ren Weijia, Li Zongfeng. A Stiffness Testing System for the Umbilical of the Active Vibration Isolation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2016, 35(7): 1144-1148. doi: 10.13433/j.cnki.1003-8728.2016.0726

空间主动隔振系统的脐带线刚度测试装置

doi: 10.13433/j.cnki.1003-8728.2016.0726
基金项目: 

载人航天领域预研项目资助

详细信息
    作者简介:

    范涛(1989-),硕士研究生,研究方向为飞行器设计、机械设计及分析,fantao@csu.ac.cn;

    通讯作者:

    任维佳(联系人),研究员,博士,renweijia@csu.ac.cn

A Stiffness Testing System for the Umbilical of the Active Vibration Isolation System

  • 摘要: 空间站上的主动隔振系统是微重力试验的有效保障。作为帮助实现供电和数据通信功能的脐带线,是主动隔振平台主要的扰动传递路径。为了测试脐带线的刚度,并选出最优的脐带线设计方案,设计了一套脐带线刚度测试装置,介绍了其硬件结构设计、软件模型。该测试系统主要由六维组合平台、六维力和力矩传感器、控制器、LabVIEW软件等组成。控制器驱动六维组合平台移动和转动,传感器采集力和力矩值,用LabVIEW软件通信并存储数据,运用Matlab进行数据处理,得出脐带线6×6的刚度矩阵,从而对脐带线缆刚度的理论研究提供实验支持。
  • [1] 李宗峰,任维佳.空间微重力主动隔振技术研究[J].载人航天,2010,16(3):24-32,36 Li Z F, Ren W J. Study on the space microgravity active vibration isolation techniques[J]. Manned Spaceflight, 2010,16(3):24-32,36 (in Chinese)
    [2] DeLomband R, Karchmer A, Bushnell G S, et al. Microgravity environment countermeasures-panel discussion[C]//35th Aerospace Sciences Meeting and Exhibit, Reno, Nevada: AIAA, 1997
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出版历程
  • 收稿日期:  2014-08-08
  • 刊出日期:  2016-07-05

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