摘要
本文提出一种能够实现导弹对活动目标全方位攻击的基本原理,并讨论了工程上实现的途径。通过平面及空间导引弹道仿真,初步证明了它的正确性及可实现性。
This paper presents a thcory which can make missiles attack moving targets in all azimuths and discusses the way of putting it in engineering prentice.The validity and reality of this theory arc primtryly demonstrate 1 by the simulation of guidance trajectories of missiles.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1989年第3期87-95,共9页
Journal of Beijing University of Aeronautics and Astronautics
关键词
末制导
全向攻击
导弹
制导
terminal guidance,all aspects attack,guidance system,optimal guidance law,trajectory simulation.
