电子干扰条件下基于攻击区指挥引导效能评估
发布时间：2018-09-14 08:08
【摘要】：针对传统指挥引导效能评估方法缺少对电子干扰因素定量分析的问题,在基于攻击区空战态势评估的基础上,提出了一种考虑电子干扰因素的超视距空战指挥引导效能评估模型。分析电子干扰对导弹攻击区的影响,从指挥引导目的态势分析入手,选取空战能力指数威胁函数和基于空空导弹攻击区的空战态势威胁函数两个指标,进行加权综合建立指挥引导效能评估函数,通过仿真计算验证了该模型的有效性。
[Abstract]:In view of the lack of quantitative analysis of electronic jamming factors in the traditional command and guidance effectiveness evaluation methods, based on the air combat situation assessment in the attack area, In this paper, a model for evaluating the effectiveness of command and guidance in over-the-horizon air combat is presented, which takes account of electronic interference factors. This paper analyzes the influence of electronic jamming on the missile attack area, starting with the situation analysis of the purpose of command and guidance, selects two indexes: the index threat function of air combat capability and the threat function of air combat situation based on the attack area of air-to-air missile. The evaluation function of command and guidance effectiveness is established by weighted synthesis, and the effectiveness of the model is verified by simulation.
【作者单位】： 空军工程大学空管领航学院;
【基金】：空军装备科研基金资助项目(KJ20150231106B41057)
【分类号】：E91;TN97
，
本文编号：2242082
[Abstract]:In view of the lack of quantitative analysis of electronic jamming factors in the traditional command and guidance effectiveness evaluation methods, based on the air combat situation assessment in the attack area, In this paper, a model for evaluating the effectiveness of command and guidance in over-the-horizon air combat is presented, which takes account of electronic interference factors. This paper analyzes the influence of electronic jamming on the missile attack area, starting with the situation analysis of the purpose of command and guidance, selects two indexes: the index threat function of air combat capability and the threat function of air combat situation based on the attack area of air-to-air missile. The evaluation function of command and guidance effectiveness is established by weighted synthesis, and the effectiveness of the model is verified by simulation.
【作者单位】： 空军工程大学空管领航学院;
【基金】：空军装备科研基金资助项目(KJ20150231106B41057)
【分类号】：E91;TN97
，
本文编号：2242082
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