Citation: | Han Wei, Huang Yiyong, Zhang Xiang, Chen Xiaoqian. Research and Development of an Impact Testing System for Space Docking Mechanism[J]. Chinese Journal of Space Science, 2013, 33(5): 548-553. doi: 10.11728/cjss2013.05.548 |
[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
|