垂直发射中远程导弹攻击机动目标弹道研究  

Research on the trajectory of vertical launching long-range missile attacks the maneuvering target

作　　者：赵娜[1] 司锡才[1] 陈涛[1] 

机构地区：[1]哈尔滨工程大学信息与通信工程学院,黑龙江哈尔滨150001

出　　处：《应用科技》2011年第1期39-43,共5页Applied Science and Technology

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.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 background, improved proportional guidance law was applied in the terminal guidance, establish the mathematical model of ballistic missiles, using matlab as simulation method and established numerical simulation model, through the simulation analyzed the characteristics of the missile.

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 

分 类 号：TJ762.3[兵器科学与技术—武器系统与运用工程]