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舰空导弹发射空域低界仿真研究 被引量:1

Simulation Study of Low Boundary of Ship-to-air Missile Launching Area
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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.
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
关键词 舰空导弹 舰载直升机 协同制导 发射区低界 ship-to-air missile ship-borne helicopter coordinated guidance launching area low boundary
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