摘要
建立复合控制导弹的末制导回路;研究了天线罩折射率、目标机动、目标角闪烁对气动力控制和复合控制时的末制导精度影响。研究表明复合控制对天线罩折射误差率的要求更为严格;复合控制对拦截大机动目标更为有效,但只考虑目标角闪烁时,空气动力控制的效果更好;综合目标机动和角闪烁的影响,复合控制可提高制导精度。
The terminal guidance loop of compound control interception missile is established.The effects caused by the radome slopes,target maneuver and target glint noise are analyzed.Simulation shows the compoud control interception missile is more sensitivity to radome slopes and more efficient for intercepting target bearing large maneuver than the aerodynamics control,however,only considering target glint noise,the aerodynamics control is better.Considering target maneuver and glint noise,the guidance accuracy o...
出处
《现代防御技术》
北大核心
2008年第2期55-60,共6页
Modern Defence Technology
关键词
拦截弹
直接力控制
复合控制
制导精度
interception missile
side-jet control
compound control
guidance accuracy
