飞航导弹齐射发射时间的一种快速规划算法  

An Fast Programming Arithmetic of Launch Time When Many Winded Missiles are Launched Synchronously

作　　者：孟海东[1,2] 廖洪昌[2] 郭荆燕[2] 慕春棣[1] 

机构地区：[1]清华大学,北京100084 [2]第二炮兵装备研究院,北京100085

出　　处：《火力与指挥控制》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)

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.

关 键 词：飞航导弹 发射时间 快速规划 航迹交叉 

分 类 号：V324[航空宇航科学与技术—人机与环境工程]