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未来空域窗射击体制仿真实验验证

Simulation Experiment Verification of Future Airspace Window Firing System
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摘要 为了对比未来空域窗与传统射击模式拦截末端反舰导弹的效能问题,以比例导引规律引导的反舰导弹为例,提出了仿真实验的主要流程,分析在仿真条件生成考虑各类误差的炮弹弹道,在全航路上进行命中判断。仿真实验表明,在探测和预测精度不高的情况下,相较于集火射击体制,未来空域窗确实具有更高的命中率。 In order to compare the different efficiency between future airspace window(FAW)and traditional firing mode,taking the anti-ship missile which is guided by proportional guidance law as an example,the main process of simulation experiment is proposed.Considering various deviations,the projectile trajectory is generated under the simulation conditions.Then the hit judg⁃ment is carried out on the whole voyage.The simulation results show that FAW does have a higher hit rate when the detection and prediction accuracy is not high,compared with the centralized fire system.
作者 陈维义 戴锐彬 CHEN Weiyi;DAI Ruibin(Arms Engineering College,Naval University of Engineering,Wuhan 430033)
出处 《舰船电子工程》 2022年第1期84-88,共5页 Ship Electronic Engineering
关键词 未来空域窗 命中判断 仿真分析 future airspace window hit judgment simulation analysis
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