空间对接机构碰撞试验系统的开发研究

韩伟; 黄奕勇; 张翔; 陈小前

doi:10.11728/cjss2013.05.548

空间对接机构碰撞试验系统的开发研究

doi: 10.11728/cjss2013.05.548 cstr: 32142.14.cjss2013.05.548

国防科学技术大学航天科学与工程学院长沙 410073

基金项目: 国家自然科学基金项目资助(50975280)

详细信息

作者简介:

韩伟, E-mail: hanwei1984@hotmail.com

中图分类号: V416.6
计量
- 文章访问数: 2308
- HTML全文浏览量: 170
- PDF下载量: 1232
- 被引次数:
  0(来源:Crossref)
  
  0(来源:其他)
出版历程
- 收稿日期: 2012-05-11
- 修回日期: 2013-04-16
- 刊出日期: 2013-09-15

Research and Development of an Impact Testing System for Space Docking Mechanism

College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073

摘要

摘要: 为研究空间对接机构在对接过程中的碰撞现象,研制了碰撞试验系统.探讨了试验系统方案;依据Hertz弹性接触理论,仿真计算了加速度频率特性,确定了加速度传感器的选择原则;利用该系统开展了低速碰撞试验.试验结果表明,该系统能够满足测量对接碰撞力的要求.
- 空间对接机构 /
- 气浮导轨 /
- 碰撞试验系统 /
- Hertz弹性接触理论 /
- 加速度传感器
Abstract: In the paper, a new ground based impact experiment system is designed to study the impact phenomenon of probe-cone docking mechanism in the course of spacecraft docking. Firstly, the whole scheme of the system, which includes the composition of the experiment system, experiment process, experimental sample and design of related devices, is given. Then, the frequency characteristic of acceleration and the effect of initial velocity on the impact time are summarized by numerical simulation on the basis of Hertz contact law, and the essential principle to choose the accelerometer for the experiment system is concluded. At last, the experiments of low speed impact are carried out. The experimental results show that the design scheme can meet the demand for measuring the docking impact force.
- Space docking mechanism /
- Aerostatic guideway /
- Impact testing system /
- Hertz contact law /
- Accelerometer

HTML全文

参考文献(6)

[1]	Chen Xiaoqian, Yuan Jianping, Yao Wen, et al. On-orbit Servicing of Spacecrafts[M]. Beijing: China Astronautic Publishing House, 2009. In Chinese (陈小前, 袁建平, 姚雯, 等. 航天器在轨服务技术[M]. 北京: 中国宇航出版社, 2009)
[2]	Yu Dengyun, Qu Guangji, Zeng Xin, et al. Contact-impact dynamic analysis of spacecraft in the course of space docking[J]. Chin. J. Space Sci., 1998, 18(1):62-68. In Chinese (于登云, 曲广吉, 曾辛, 等. 航天器对接接触过程撞击动力学分析[J]. 空间科学学报, 1998, 18(1):62-68)
[3]	Yang Yongqiang, Li Shuang, Xie Lili. Numerical simulation of component-dropping-collision[J]. J. Vibrat. Shock, 2010, 29(6):54-58. In Chinese (杨永强, 李爽, 谢礼立. 构件跌落碰撞的数值模拟研究[J]. 振动与冲击, 2010, 29(6):54-58)
[4]	Zhang Xiang, Huang Yiyong, Han Wei, et al. Numerical simulation of accelerometer sensor characteristics of an impact testing system[J]. Spacecr. Envir. Eng., 2010, 27(4):477-480. In Chinese (张翔, 黄奕勇, 韩伟, 等. 碰撞试验系统中加速度传感器特性仿真研究[J]. 航天器环境工程, 2010, 27(4):477-480)
[5]	Xing Lijuan, Yang Shizhong. Design for piezoelectric accelerometer measurement system[J]. Piezoelectr. Acoustoopt., 2009, 31(2):215-217. In Chinese (邢丽娟, 杨世忠. 压电加速度测量系统的设计[J]. 压电与声光, 2009, 31(2):215-217)
[6]	Her S C, Liang Y C. The finite element analysis of composite laminates and shell structures subjected to low velocity impact[J]. Compos. Struct., 2004, 66:277-285