自寻的反坦克导弹攻顶弹道仿真研究  

Simulation Research on Large Impact Angle Trajectory of Homing Guidance Anti-tank Missile

作　　者：王真[1] 高凤岐[1] 高敏[1] 卢志才[1] 任海龙[1] 

机构地区：[1]军械工程学院,石家庄050003

出　　处：《战术导弹技术》2015年第5期90-96,共7页Tactical Missile Technology

基　　金：装备预研共用技术基金项目(9140A05040213JB34069)

摘　　要：针对自寻的反坦克导弹需求,分析推导了导弹数学模型,包括坐标系与几何关系、导弹受力情况、运动学模型。围绕攻顶弹道进行了设计,探讨了弹道参数选择问题,给出了调试后的五种弹道参数取值。建立了制导控制系统仿真模型,对攻顶弹道进行了Simulink仿真。仿真结果表明,弹道设计合理可行、制导精度高,可对300 m^2500m的目标实施攻顶攻击,脱靶量在0.5 m以内。Aiming at homing guidance man-portable anti-tank missile,the mathematical model is deduced,including coordinate,geometric relation,force analysis and kinematics model. With designing the trajectory scheme with large impact angle,the parameters selection is discussed,the values of parameters are ascertained. The simulation model of guidance and control system is built,and the simulation of trajectory scheme based on Simulink is processed. The simulation results show that,the trajectory scheme is effective and with high guidance accuracy,with miss distance less than 0. 5m against targets at distance between 300 m and 2500 m.

关 键 词：反坦克导弹 攻顶弹道 参数选择 

分 类 号：TJ761.1[兵器科学与技术—武器系统与运用工程]