Calculation Model of the Flight Trajectory of an Air-to-air Missile
YANG Ling
MAO Dejun
YU Kaize
LIU Tong
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.
Keywords：air-to-air missilestrack calculationmodel
Publication Date：2025-01-19
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：6( 52-57 )