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垂直发射中远程导弹攻击机动目标弹道研究
引用本文:赵娜,司锡才,陈涛. 垂直发射中远程导弹攻击机动目标弹道研究[J]. 应用科技, 2011, 38(1): 39-43. DOI: 10.3969/j.issn.1009-671X.2011.01.010
作者姓名:赵娜  司锡才  陈涛
作者单位:哈尔滨工程大学,信息与通信工程学院,黑龙江,哈尔滨,150001
摘    要:中远程导弹攻击机动目标复合制导弹道仿真是导弹精确制导系统建模与仿真的一个重要组成部分.对导弹弹道进行建模和仿真是研究导弹武器性能的重要手段.该文主要针对中远程导弹特性,并针对目标机动特性,以某型垂直发射中远程复合制导反辐射导弹为研究背景建立导弹的弹道数学模型,在末制导段应用改进的比例导引律进行制导,并采用Matlab对所建立的模拟弹道模型进行了数值仿真验证,通过仿真来分析导弹特性.

关 键 词:垂直发射中远程导弹  模拟弹道模型  改进的比例导引律  数值仿真

Research on the trajectory of vertical launching long-range missile attacks the maneuvering target
ZHAO Na,SI Xi-cai,CHEN Tao. Research on the trajectory of vertical launching long-range missile attacks the maneuvering target[J]. Applied Science and Technology, 2011, 38(1): 39-43. DOI: 10.3969/j.issn.1009-671X.2011.01.010
Authors:ZHAO Na  SI Xi-cai  CHEN Tao
Affiliation:ZHAO Na,SI Xi-cai,CHEN Tao (College of Information and Communication,Harbin Engineering University,Harbin 150001,China)
Abstract:The long-range,against maneuvering targets,multi-mode compound guidance missile trajectory simulation is an important part in precision-guided missile system modeling and simulation.The trajectory modeling and simulation is an important means to study the performance of missile weapons.This article features the characters of long-range missile,meanwhile with the maneuvering characteristics of the target,to a certain type of vertical launching long-range guided anti-radiation missile in complex battlefield b...
Keywords:Long-range missile vertical launching  trajectory model Simulation  Improved proportional guidance law  Numerical simulation  
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