多机空战指挥引导优势量化评估模型研究  

Research on Quantitative Evaluation Model of Multi-aircraft Air Combat Command and Guidance Superiority

作　　者：高阳阳 余敏建[1] 杨杰[1] GAO Yang-yang;YU Min-jian;YANG Jie(Air Traffic Control and Navigation College,Air Force Engineering University,Xi＇an 710051,China)

机构地区：[1]空军工程大学空管领航学院,陕西西安710051

出　　处：《航空计算技术》2018年第4期33-36,45,共5页Aeronautical Computing Technique

基　　金：空军装备科研项目资助

摘　　要：针对目前多机空战指挥引导优势量化评估模型少的现状,以单机空战指挥引导优势评估模型为基础,分析了角度、速度、距离、高度等对空空导弹攻击区的影响,结合指挥引导实际,建立了单机的角度、距离、速度、高度优势指标,确定了单机指挥引导综合优势函数,在单机指挥引导综合优势函数的基础上,建立了多机空战指挥引导综合优势函数,最后进行了二对二的仿真验证。仿真结果表明了模型的可靠性和可行性,为多机空战指挥引导进行优势评估拓展了思路。Aiming at the present situation that the quantitative evaluation model of multi-aircraft air combat command and guidance superiority is few,based on the evaluation model of single-aircraft air combat command and guidance superiority,the influence of angle,speed,distance and altitude on air-to-air missile attack area is analyzed,the angle,distance,speed and altitude superiority index of single-aircraft air combat command and guidance is established according to the actual command and guidance,and the comprehensive superiority function of single-aircraft air combat command and guidance is established on the basis of the comprehensive superiority function of single-aircraft air combat command and guidance.Finally,the simulation verification of two to two is carried out. The simulation results show the reliability and feasibility of the model,which expands the idea for the superiority evaluation of multi-aircraft air combat command and guidance.

关 键 词：多机空战 指挥引导 优势函数 仿真验证 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]