摘要
基于Simulink仿真环境,以某型空空导弹为仿真对象,对该型空空导弹的打击过程进行了分析,建立了导弹的飞行控制模型,对各个子模块采用Simulink建立单元仿真子模型,通过对单元仿真子模型的集成得到了导弹飞行控制的仿真模型。仿真结果表明该模型能够正确反映出导弹发射后的飞行特点,对空空导弹导弹的分析研究能起到一定的帮助作用。
Based on simulation environment of Simulink, this paper analyze the attack process of certain air-to-air missile。To establish the fly control model,firstly, use the Simulink establish submodel of the submodular,then combine them, we get the total fly control model. The simulation output indicate that the model we established can directly reflect the fly character of missile, is helpful to the research and study of air-to-air missile.
出处
《国防制造技术》
2016年第2期67-72,共6页
Defense Manufacturing Technology