摘要
提出一种基于自动驾驶仪和被动雷达寻的制导的抗关机制导方案.该方案利用导弹发射时机载定位系统提供的目标位置信息、目标雷达关机前导引头的测量信息及自动驾驶仪提供的导弹姿态信息,在雷达关机后,对目标视线角及视线观测角进行推算,从而达到抗关机目的该方案具有简单、可靠、成本低廉等优点仿真结果证实了该方案的有效性.
A new guidance scheme is presented, in which the angles of line - of - sight, after the target radar being switched off, are calculated on from the target location acquired by mother aircraft, the observed angles of passive radar when the target radar is being turned off and attitude angles supplied by autopilot and it is to understand,mathematics simulation proved the effectiveness of the proposed scheme.
出处
《哈尔滨工业大学学报》
EI
CAS
CSCD
北大核心
1999年第5期8-10,共3页
Journal of Harbin Institute of Technology
关键词
反辐射导弹
寻的制导
抗关机能力
雷达关机
antiradiation missiles
homing guidance
against target radar switching - off