基于改进两步裁定法的内埋空空导弹作战效能评估  

Operational effectiveness evaluation method for the buried air-to-air missile based on an improved two-step adjudication method

作　　者：徐洋 伍友利[1] 黄晨 刘同鑫[1] XU Yang;WU Youli;HUANG Chen;LIU Tongxin(Aeronautics Engineering College, Air Force Engineering University, Xi’an 710038, China;Unit 95972 of the PLA, Jiuquan 735000, China)

机构地区：[1]空军工程大学航空工程学院,陕西西安710038 [2]中国人民解放军95972部队,甘肃酒泉735000

出　　处：《系统工程与电子技术》2019年第12期2763-2771,共9页Systems Engineering and Electronics

基　　金：国家自然科学基金重大项目(61627901);博士后创新基金(BX201700104)资助课题

摘　　要：针对内埋空空导弹的作战效能评估问题,本文通过将编队方式、态势信息以及目标分配模型融入到传统多步裁定法中,提出了一种更加完善的两步裁定法用以评估内埋空空导弹作战效能。通过分析战场实际情况,分别从方位角和进入角的角度建立优势函数,并引入串联系统构建载机角度优势函数。根据作战高度对导弹攻击区远界的影响,构建了空空导弹优势函数;结合高度优势函数,将上述3种优势函数聚合为空战优势函数,并依此建立了先敌发射概率模型、导弹毁伤概率模型和综合威胁指数模型,从而完成目标分配。仿真结果表明,改进算法的评估结果与客观态势一致性较强,可为研究内埋空空导弹的作战效能提供理论参考。Aiming at the problem of operational effectiveness evaluation of buried air-to-air missiles, a more perfect two-step ruling method is proposed by integrating the formation mode, situation information and target allocation model into the traditional multi-step ruling method. By analyzing the actual situation of the battlefield, the advantage function is established from the angle of azimuth and the entry angle respectively, and the series system is introduced to construct the carrier angle advantage function. According to the influence of the combat altitude on the far-end of the missile attack area, the air-to-air missile advantage function is constructed. Combined with the high-potential function, the above three dominant functions are aggregated into the air-war advantage function, and the first enemy launch probability model, missile damage probability and the integrated threat index model are established accordingly, then the target allocation is completed. The simulation results show that the evaluation results of the improved algorithm are in good agreement with the objective situation, which can provide theoretical reference for studying the operational effectiveness of the buried air-to-air missile.

关 键 词：内埋空空导弹 作战效能 两步裁定法 空战优势函数 目标分配 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]