摘要
多发飞航导弹齐射时,各发导弹之间存在碰撞或者相互干扰的可能,为了保证导弹飞行安全,需要对各发导弹的飞行管道进行分析,以此规划各发导弹发射时间。为此在对飞航导弹初段航迹分析的基础上,建立了一种发射时间的快速规划算法,实现了以较小的计算量规划发射时间,并且通过仿真计算证实了该算法是正确的。
When many missiles are launched synchronously, there is probability of hit or disturbance among every missile. For the flying safety of the missiles, it's necessary to analyze the flying conduit of every missile to program the launch times of every missile. So based on the analyses of the winded missile's first segment track, the fast programming arithmetic of launch time is established, it's come out that programming the launch times by small calculating quantity, and it's proved that this arithmetic is correct by simulation.
出处
《火力与指挥控制》
CSCD
北大核心
2009年第9期106-109,113,共5页
Fire Control & Command Control
基金
二炮装备部基金资助项目(EP06404)
关键词
飞航导弹
发射时间
快速规划
航迹交叉
winded missile ,launch time ,fast programming ,track intersection