摘要
就机载拖曳式诱饵对对空导弹末制导雷达单脉冲角度跟踪系统进行角度欺骗的三种方式进行了深入分析,建立了机载拖曳式诱饵对雷达进行角度欺骗干扰的三维计算模型,提出导弹在分辨出飞机和诱饵前瞄准的能量中心可能位于载机和诱饵的连线之外,并对三种干扰方式下脱靶量随角度、电压幅度比变化的情况进行了仿真分析,提出了相应的战术运用原则。
Three modes of airborne towed decoys realizing angle deception against the monopulse radar angle tracking system of antiaircraft missile seekers are analyzed,and a three-dimensional calculation model of airborne towed decoys is established.It is presented that the aiming energy center may locate out of connecting line of the aircraft and decoys before they are differentiated.Simulation analysis of conditions that undershoot amounts change with angle and voltage degree ratio varying is done for the three modes,and some corresponding tactics principle for decision-making are provided.
出处
《航天电子对抗》
2011年第4期13-16,共4页
Aerospace Electronic Warfare
