Abstract：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.
束川良, 朱迪, 钟永建, 孟万里, 郝莲英. 防空导弹拦截高速大俯冲机动目标中制导律设计[J]. 空天防御, 2019, 2(1): 29-32.
SHU Chuanliang, ZHU Di, ZHONG Yongjian, MENG Wanli, HAO Lianying. Design of Midcourse Guidance Law of Air Defence Missile Intercepting High Speed Maneuvering Target with Big Diving Angle. Air & Space Defense, 2019, 2(1): 29-32.
