防空导弹拦截高速大俯冲机动目标中制导律设计

Design of Midcourse Guidance Law of Air Defence Missile Intercepting High Speed Maneuvering Target with Big Diving Angle

简要分析了高速大俯冲目标的特点以及防空导弹采用传统比例导引拦截此类目标的缺点,提出了对大俯冲机动目标进行实时预测的措施,着重介绍了一种准逆轨拦截的导引方法,并通过仿真实例验证了此方法的有效性。

This paper makes analysis of the characteristics of high speed maneuvering target with large diving angle and the disadvantages of interception of this kind of targets by the missile using traditional proportional guidance.It suggests a real-time prediction measure for this kind of targets and introduces a guidance method of quasi-counter trajectory interception.Simulation tests have also been carried out to verify the effectiveness of this method.