空天防御2019，Vol.2Issue(1)：29-32,4.
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
束川良 1朱迪 1钟永建 1孟万里 1郝莲英1
作者信息
- 1. 上海机电工程研究所, 上海 201109
- 折叠
摘要
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.关键词
机动目标/防空导弹/导引律/中制导律Key words
maneuvering target/air defence missile/guidance law/midcourse guidance law分类
航空航天引用本文复制引用
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):29-32,4.
