[1]杨富锋,芮筱亭,王强,等.多管火箭起始扰动控制研究[J].南京理工大学学报(自然科学版),2010,(01):61-65.
 YANG Fu-feng,RUI Xiao-ting,WANG Qiang,et al.Initial Disturbance Control for Multiple Launching Rocket System[J].Journal of Nanjing University of Science and Technology,2010,(01):61-65.
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多管火箭起始扰动控制研究
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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:
2010年01期
页码:
61-65
栏目:
出版日期:
2010-02-28

文章信息/Info

Title:
Initial Disturbance Control for Multiple Launching Rocket System
作者:
杨富锋;芮筱亭;王强;王国平;
南京理工大学发射动力学研究所
Author(s):
YANG Fu-feng1RUI Xiao-ting1WANG Qiang2WANG Guo-ping1
1.Institute of Launch Dynamics,NUST,Nanjing 210094,China;2.School of Mechatronic Engineering,Beijing Institute of Technology,Beijing 100081,China
关键词:
起始扰动 控制 多体系统传递矩阵法 射击精度
Keywords:
initial disturbance control transfer matrix method of multibody system firing accuracy
分类号:
TJ415
摘要:
为解决火箭弹起始扰动对多管火箭射击精度具有重大影响的问题,该文采用通过控制定向管角运动来减小火箭弹起始扰动的方案提高多管火箭射击精度。应用受控多体系统传递矩阵法和发射动力学理论,建立了受控多管火箭发射控制动力学模型,数值仿真获得多管火箭定向管角运动对起始扰动的影响规律及多管火箭定向管角运动的控制规律。该文控制火箭弹起始扰动的方法为提高射击精度提供了手段。
Abstract:
In order to solve the problem that the initial disturbance of the rocket projectile has a serious effect on firing accuracy of the multiple launching rockets system(MLRS),this paper uses launcher angular motion control to reduce the initial disturbance of rocket projectile for improving the MLRS firing accuracy.The transfer matrix method of controlled multibody system and the theory of launch dynamics are used to establish a model of launch dynamics with control for multiple launch rockets.The effect law of launcher angular motion on initial disturbance and the control law of the launcher angular motion are obtained by numerical simulation.The method of controlling the initial disturbance of rocket provides a new means to improve firing accuracy of MLRS.

参考文献/References:

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备注/Memo

备注/Memo:
基金项目: 江苏省自然科学基金攀登计划资助项目( BK2008046); 国家自然科学基金( 10902051)作者简介: 杨富锋( 1978- ), 男, 博士, 副教授, 主要研究方向: 兵器发射理论与技术, Em a il: fufengyang@ yahoo.com. cn。
更新日期/Last Update: 2012-11-02