摘要
为保证飞航导弹末段的突防效果,提高战斗部的杀伤威力,要求导弹在 末段进行跃起俯冲并以一定的弹道倾角命中目标。根据惯导、高度表和雷达提 供的信息,设计了以弹道倾角为被控对象的导引规律,实现了以上目标。对于跃 起俯冲的高度与距离进行了分析计算。通过数值仿真,验证了这种方法的有效 性。
In order to guarantee terminal penetration effect and raise warhead’s lethality, cruise missile should take jump-dive maneuver and obtain specific incident angle to hit the target. Based on the information obtained from INS, altimeter and radar, the guidance law with trajectory inclination angle as its controlled output is designed to achieve the above goal. Jump-dive height and distance are analyzed and calculated. Numerical simulation demonstrates its effectiveness.
出处
《航天控制》
CSCD
北大核心
2005年第1期62-64,共3页
Aerospace Control
关键词
飞航导弹
跃起俯冲
导引
Cruise missile Jump-dive Guidance
