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.
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)
出处
《舰船电子工程》
2025年第1期52-57,共6页
Ship Electronic Engineering
关键词
空空导弹
航迹计算
模型
air-to-air missiles
track calculation
model
