首页 | 本学科首页   官方微博 | 高级检索  
     

旋转导弹自旋频率设计
引用本文:邹汝平,张延风.旋转导弹自旋频率设计[J].兵工学报,2007,28(2):220-222.
作者姓名:邹汝平  张延风
作者单位:中国兵器工业第203研究所,陕西,西安,710065;中国兵器工业第203研究所,陕西,西安,710065
摘    要:针对旋转导弹的自旋频率设计,给出了其影响因素,自旋频率选择原则,考虑了导弹动态稳定区等因素,以某导弹为例,计算了其动力系数、固有频率、动态稳定区,通过大量系统计算、系统频率分析,设计了某旋转弹自旋频率。文中提出的方法对同类导弹自旋频率设计有参考价值。

关 键 词:航天器结构与设计  旋转弹  自旋频率  动力系数  动态稳定区
文章编号:1000-1093(2007)02-0220-03
修稿时间:03 29 2006 12:00AM

Design of Self-spin Frequency for Rotating Missiles
ZOU Ru-ping,ZHANG Yan-feng.Design of Self-spin Frequency for Rotating Missiles[J].Acta Armamentarii,2007,28(2):220-222.
Authors:ZOU Ru-ping  ZHANG Yan-feng
Affiliation:No.203 Research Institute of China Ordnance Industries, Xi'an 710065, Shaanxi,China
Abstract:Aimed at the design of rotating missile's self-spin frequency,the factors of influence and principle for the choice of self-spin frequency were presented in consideration of the missile's dynamic stable region.Taking a type of missile as an example,the self-spin frequency of the rotating missile was designed by calculating power factor,intrinsic frequency and dynamic stable region of the missile and analyzing systematic frequency.The method presented in this paper has reference value for self-spin frequency design in the similar kinds of missiles.
Keywords:spacecraft structure and design  rotating missile  self-spin frequency  power factor  dynamic stable region
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《兵工学报》浏览原始摘要信息
点击此处可从《兵工学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号