导弹主被动雷达导引头共口径技术研究  

Study on the Techniques of Co-aperture in Missile Positive/Passive Radar Seeker

作　　者：温先福 李刚[1] 田德伟[1] 张兴[1] 

机构地区：[1]空军工程大学防空反导学院,西安710051

出　　处：《弹箭与制导学报》2015年第1期32-36,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：导引头共口径技术是主被动雷达导引头关键技术之一。针对导弹主被动雷达导引头内部空间有限的问题,提出了导引头共口径技术,采取了把微带贴片天线应用到导引头表面的措施,得到了预期的结果。通过对微带贴片天线的设计,研究导弹主被动雷达导引头的性能,经过分析和仿真表明所提出方法的有效性。Rader seeker co-aperture is one of key techniques in research of positive / passive radar seeker,which is aimed at the problem of missile＇s internal space limitation. Furthermore,some applying strip patch antenna in the surface of radar seeker and the property of positive / passive radar seeker by the design of strip patch antenna. The simulation results and data analyses have proved availability of this method.

关 键 词：主被动雷达导引头 共口径 微带贴片天线 

分 类 号：TJ765.332[兵器科学与技术—武器系统与运用工程]