[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]The Research on Unfolding Test and Dynamic Model of Folding-wing
Received date: 2011-07-23
Online published: 2025-05-29
吴俊全 , 孙海文 , 张晓旻 . 折叠翼展开试验与动力学仿真研究[J]. 弹箭与制导学报, 2012 , 32(3) : 164 -166 . DOI: 10.15892/j.cnki.djzdxb.2012.03.052
The research on the parameters of folding-wing's spreading performance is of great significance to the design and improvement of the folding wings. In this paper, performance of the folding-wing's unfolding process was analyzed by using ground test and dynamics imitating analysis by ADAMS. The actual experimental results were compared with the dynamic simulation results, the unfolding dynamic model of the folding-wing structure was proved to be reasonable and applicable. Both the actual experimental results and the dynamic simulation results show that the structure design of the folding-wings is able to meet the demands of flight.
Key words: folding-wings; simulation; test
| [1] | 王俊生. 有翼导弹结构设计图册[M]. 北京: 宇航出版社, 1992. |
| [2] | 赵育善, 余旭东, 马彩霞,等. 折叠翼展开过程仿真研究. 弹箭与制导学报, 1997 (2): 19- 23. |
| [3] | 余旭东, 葛金玉, 段德高,等. 导弹现代结构设计[M]. 北京: 国防工业出版社, 2007. |
| [4] | 李军. ADAMS 实例教程[M]. 北京: 北京理工大学出版社, 2002. |
/
| 〈 |
|
〉 |