[1]朱怀亮,张福祥.车载火箭发射系统柔性效应的仿真与分析[J].南京理工大学学报(自然科学版),1997,(02):45-48.
 ZhuHauiliang ZhangFuxiang.Simulation and Analysis of Effects of Flexibility for a Vehicle based Rocket launcher System[J].Journal of Nanjing University of Science and Technology,1997,(02):45-48.
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车载火箭发射系统柔性效应的仿真与分析()
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
期数:
1997年02期
页码:
45-48
栏目:
出版日期:
1997-04-30

文章信息/Info

Title:
Simulation and Analysis of Effects of Flexibility for a Vehicle based Rocket launcher System
作者:
朱怀亮张福祥
南京理工大学机械学院, 南京210094
Author(s):
ZhuHauiliang ZhangFuxiang
School of Mechanics,NUST,Nanjing 210094
关键词:
火箭 发射装置 动力学 数值仿真
Keywords:
rocket s launcher s dynamics numerical simulat ion
分类号:
V554
摘要:
以车载、多管、大长径比火箭为研究对象,建立火箭—发射装置刚柔耦合系统的动力学模型,进行有效的数值仿真;分析和评价了结构柔性等因素对火箭发射姿态和系统动力特性的影响,获得了一些重要的结论。为精确地计算起始扰动、设计和研制新型远程火箭武器系统提供了理论依据
Abstract:
In this paper , ef fect s o f flex ibility o f the v ehicle-based, larg e size mult iple rocket-launcher system are analysed. An approach is pr esented to simulate the co upled vibr at ion behav io r between the rocket and launcher , and numeral solut ion is dev elo ped. The inf luence of bending f lexibility of the launch sy stem on r ocket’s mot ion at t itude and system’s dy namic char acter ist ics are discussed. Some impo rtant conclusio ns are draw n. The numerical result s are of g reat value to the at t itude co tr ol of ro cket and the design of new type long-range r ocket w eapon system.

参考文献/References:

1 朱怀亮. 柔性火箭发射系统动态仿真与发射特性研究: [ 博士学位论文] . 南京: 南京理工大学, 1995
2 Kim S S , Shaba na A A, Hang E J. Automat ed v ehicle dynamic analy sis with flex ible components. Jour nal of Mechanisms, Tr ansmlssions, and Automation in Desig n, 1984, 106: 126~312

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备注/Memo

备注/Memo:
国家教委固体力学开放研究实验室基金,国防科技预研行业基金
朱怀亮 男 39岁 博士后
更新日期/Last Update: 2013-03-29