舰船电子工程2025，Vol.45Issue(1)：52-57,6.DOI:10.3969/j.issn.1672-9730.2025.01.011
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
杨令 1毛德军 1于楷泽 1刘通2
作者信息
- 1. 海军航空大学 烟台 264001
- 2. 中国人民解放军92485部队 莱阳 265200
- 折叠
摘要
Abstract
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Key words
air-to-air missiles/track calculation/model引用本文复制引用
杨令,毛德军,于楷泽,刘通..空对空导弹飞行航迹计算模型[J].舰船电子工程,2025,45(1):52-57,6.
