基于拦截任务的飞机作战半径仿真研究  

Research on Simulation of Combat Radius of Fighter Aircraft Based on Intercept Mission

作　　者：胡朝晖 吕跃[2] 徐安[2] HU Zhao-hui;LYU Yue;XU An(College of Mechanical Engineering,Xijing University,Xi’an 710123,China;Engineering College of Aeronautics,Air Force Engineering University,Xi’an 710038,China)

机构地区：[1]西京学院机械工程学院,西安710123 [2]空军工程大学航空工程学院,西安710038

出　　处：《火力与指挥控制》2021年第9期14-19,共6页Fire Control & Command Control

基　　金：国家自然科学基金资助项目(61703427)。

摘　　要：为解决拦截飞机作战半径计算复杂的问题,提出了一种计算作战半径新方法。定义了作战飞机作战半径、最短拦截时间和拦截线等概念;推导了拦截飞机作战半径计算模型,量化了载荷和空战意图对作战半径的影响,实现了多型飞机的作战半径估算;基于最小二乘法实现了对仿真作战半径的修正,验证了该计算方法所得作战半径,能够满足空战仿真、任务规划和效能分析的工程需求。A new calculation method is proposed in order to solve problem of high computing complexity of the combat radius of interceptor aircraft.Firstly,the concepts of combat radius,shortest interception time and blocking line are defined.Secondly,the influences of aircraft stores and combat intention are analyzed,and the combat radius models of interceptor aircraft are derived.At last,the combat radius is modified based on the least square method.The analysis shows that the calculation method can meet the requirements of air combat simulation,mission planning and effectiveness analysis.

关 键 词：拦截飞机 作战半径 系统仿真 航空火控 

分 类 号：TJ85[兵器科学与技术—武器系统与运用工程] V271.4[航空宇航科学与技术—飞行器设计]