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作 者:徐航 郑红星 左非 蒋艳国 肖和业 XU Hang;ZHENG Hongxing;ZUO Fei;JIANG Yanguo;XIAO Heye(Xi’an Modern Control Technology Research Institute,Xi’an 710065,China)
出 处:《弹箭与制导学报》2019年第6期29-32,共4页Journal of Projectiles,Rockets,Missiles and Guidance
摘 要:制导弹药在飞行过程中,在受到激励源EMP辐照时会受到干扰产生感应电场。文中应用CST软件对制导弹药飞行时所受外部条件的影响时的微波效应特性进行了仿真分析。仿真结果显示,导弹头部相对于其他部件更为敏感;对于整弹而言,激励源侧方入射比其他方向入射对舱内产生更大的影响。根据仿真分析的结果得到弹上的敏感部位和敏感器件的耦合状态,从而为整弹的防护设计提供了设计指导。Missiles will generate induced electric field when irradiated by electromagnetic pulses during the flight.In this paper,the CST software is used to simulate the microwave effect characteristics of missiles when they are affected by external conditions.The results show that the head of missile is more sensitive than other parts;For the whole missile,electromagnetic pulse in side direction will generate grater influences to the cabin than pulses in other directions.According to the results of the simulation analysis,the sensitive parts of the missile and the coupling states of these parts are obtained,which provides a good design guidance for the design of the missile.
分 类 号:TJ410[兵器科学与技术—火炮、自动武器与弹药工程]
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