空对空导弹飞行航迹计算模型  

Calculation Model of the Flight Trajectory of an Air-to-air Missile

作　　者：杨令 毛德军 于楷泽 刘通 YANG Ling;MAO Dejun;YU Kaize;LIU Tong(Naval Aviation University,Yantai 264001;No.92485 Troops of PLA,Laiyang 265200)

机构地区：[1]海军航空大学,烟台264001 [2]中国人民解放军92485部队,莱阳265200

出　　处：《舰船电子工程》2025年第1期52-57,共6页Ship Electronic Engineering

摘　　要：在空战中,想要摆脱导弹的锁定、跟踪,需要对空空导弹的飞行和速度变化的一般规律进行分析研究,才能对其性能进行更加深入的掌握。论文从导弹飞行速度变化着手,对空空导弹在飞行过程中的速度、距离随时间的变化进行了分析,并分别建立了近似计算模型,对于理解空空导弹的飞行过程有较好的帮助。In air combat,in order to get rid of the locking and tracking of missiles,it is necessary to analyze and study the general laws of flight and speed changes of air-to-air missiles in order to have a deeper grasp of their performance.Starting from the change of missile flight speed,this paper analyzes the changes of speed and distance of air-to-air missiles with time during flight,and establishes approximate calculation models,which are of good help for understanding the flight process of air-to-air missiles.

关 键 词：空空导弹 航迹计算 模型 

分 类 号：E927[军事—军事装备学]