舰空导弹发射空域低界仿真研究  

Simulation Study of Low Boundary of Ship-to-air Missile Launching Area

作　　者：聂心东[1] 姜文志[1] 李大鹏[1] 徐勤超[1] 

机构地区：[1]海军航空工程学院,山东烟台264001

出　　处：《微计算机信息》2009年第22期165-167,共3页Control & Automation

基　　金：国家十一五预研基金项目;基金申请人:姜文志

摘　　要：为增加舰空导弹拦截低空目标的发射时机,研究了舰载直升机与舰艇协同制导下舰空导弹发射空域的低界。首先分别计算了单舰制导和舰载直升机协同制导下发射区低界;然后通过仿真比较,得出空舰协同制导下比单舰制导下航路捷径增加了270%,发射空域低界的纵深显著增加的结论,为舰艇作战指挥决策提供了较好的理论依据。In order to increase launching opportunities of ship-to-air missile intercepting the low-altitude target, launching area low boundary of ship-to-air missile guided by ship-borne helicopter and warship coordination was researched. In this paper, launching area low boundary of ship-to-air missile guided by one warship and coordinated guidance by ship-borne helicopter were respectively calculated. Then, A comparison of this Coordinated Guidance was given after simulation. This paper gets a conclusion that Ship-to- Air coordinated guidance can effectively increase target course shortcut 270% and enhance the depth of launching area low boundary remarkably. It provides theoretic references for battle commanding decision-making of the warship.

关 键 词：舰空导弹 舰载直升机 协同制导 发射区低界 

分 类 号：TJ761.7[兵器科学与技术—武器系统与运用工程] TP391.9[自动化与计算机技术—计算机应用技术]