滚转弹道导弹耦合特性研究

刘君; 孟云鹤; 程伟民; 汤国建; 陈克俊

doi:10.15892/j.cnki.djzdxb.2011.01.035

弹箭与制导学报 >

2011 , Vol. 31 >Issue 1: 5 - 9

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.01.035

导弹与制导技术

滚转弹道导弹耦合特性研究

刘君 ,
孟云鹤 ,
程伟民 ,
汤国建 ,
陈克俊

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¹ 国防科学技术大学航天与材料工程学院,长沙 410073
² 第二炮兵装备研究院,北京 100085

刘君(1979-),男,湖南常宁人,博士研究生,研究方向:飞行器动力学、制导与控制。

收稿日期: 2010-03-31

网络出版日期: 2025-05-30

基金资助

国家自然科学基金(10702078)资助

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The Research on Coupling Property of Rolling-ballistic Missile

LIU Jun ,
MENG Yunhe ,
CHENG Weimin ,
TANG Guojian ,
CHEN Kejun

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¹ College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China
² The Second Artillery Equipment Academy, Beijing 100085, China

Received date: 2010-03-31

Online published: 2025-05-30

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摘要

研究滚转弹道导弹的耦合特性。从滚转弹道导弹的耦合机理分析出发,运用对角优势度与Gershgor-in带定量的分析了某型滚转弹道导弹耦合特性,并初步分析了滚转弹道导弹耦合特性对控制系统设计的影响。分析结果表明:为了降低控制系统设计难度,滚转弹道导弹滚转速度应小于某一特定值,在起飞开始阶段其主要受运动耦合部分限制,而后则由控制耦合部分所决定。

关键词： 滚转弹道导弹; 耦合特性; 对角优势度; Gershgorin 带

本文引用格式

刘君 , 孟云鹤 , 程伟民 , 汤国建 , 陈克俊 . 滚转弹道导弹耦合特性研究[J]. 弹箭与制导学报, 2011 , 31(1) : 5 -9 . DOI: 10.15892/j.cnki.djzdxb.2011.01.035

Abstract

The coupling property of rolling-ballistic missiles was investigated. Firstly, the coupling mechanism was analyzed. Secondly, the coupling property was analyzed quantitatively with diagonal domination and Gershgorin bands. Finally, the influence of the coupling property on the design of the control system was analyzed primarily. The conclusion was drawn; in order to reduce the design difficulty of control system, the actual rolling speed of the rolling ballistic missiles should be less than the maximum rolling speed, and it is mostly limited by sport coupling at the beginning of flying-off, after that by the control coupling.

Key words： rolling-ballistic missiles; coupling property; diagonal domination; Gershgorin band

参考文献

[1]	袁天保, 刘新建, 秦子增. 自旋弹道导弹模型及运动特性分析[J]. 系统仿真学报, 2004, 16(6): 1125-1127.
[2]	张鸣, 祝学军, 陈海东. 滚转导弹耦合性分析[J]. 导弹与航天运载技术, 2005 (4): 47-51.
[3]	贾沛然, 陈克俊, 何力. 远程火箭弹道学[M]. 长沙: 国防科技大学出版社, 1993.
[4]	钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2006.
[5]	Martin J C. On Magnus effects caused by the Boundary-Layer displacement thickness on bodies of revolution at small angles of attack[J]. Journal of Aeronautical Science, 1957, 24(7): 421-429.
[6]	白方周. 多变量频域理论与设计技术[M]. 北京: 国防工业出版社, 1988.
[7]	Rosenbrock H H. Design of multivariable control system using the inverse Nyquist array[J]. Computer-Aided Design, 1972, 4(5): 222-227.
[8]	Arrow A, Williams D. Comparison of classical and modern autopilot design and analysis techniques for a tactical air-to-air bank-to-turn missile[C]// Proceedings of 1987 AIAA Guidance, Navigation and Control Conference, 1987.

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