摘要
在对舰艇摇摆状态下垂直发射型舰空导弹发射姿态的计算方法及其典型飞行弹道分析的基础上,将导弹运动学弹道分成无控段、初制导段、初末制导交接段和末制导段,根据导弹各飞行阶段的制导特征分别建立了飞行弹道的仿真模型,并对不同发射姿态的导弹弹道特征进行了仿真分析。运用该模型可进一步确定舰艇摇摆状态下,舰空导弹的杀伤区、战斗部的毁伤能力及导弹的发射时机,为指挥员进行防空作战指挥提供了理论参考依据。
On the basis of the calculation method and typical flight trajectory analysis of the vertical launching ship to air missile launching state under the swaying state of the ship,the ballistic trajectory of the missile is divided into non control,initial guidance,transition section and terminal guidance section.It establishes the simulation of the flight trajectory according to the characteristics of the missile's flight stages.The real model is simulated and the ballistic characteristics of different launching state are simulated.This model can be used to further determine the damage area of the ship to air missile,the damage capacity of the warship and the launching time of the missile,and provide a theoretical reference for the commander to conduct air defense operation command.
作者
王光源
毛世超
孙涛
蔡蕾
WANG Guang-yuan;MAO Shi-chao;SUN Tao;CAI Lei(Naval Aviation University,Yantai 264001,China;Unit 92852 of PLA,Ningbo 315033,China)
出处
《火力与指挥控制》
CSCD
北大核心
2020年第3期64-68,74,共6页
Fire Control & Command Control
基金
全军军事类研究生基金资助项目(2016JY254)。
关键词
舰空导弹
弹道仿真
舰艇摇摆
比例导引法
ship to air missile
trajectory simulation
warship swaying
proportional guidance method
