Mathematical Model and Budget Algorithm Design of Land-Based Missile
WANG Shaochun
WANG Zhefeng
CHEN Yvchen
LIU Yanlong
ZHANG Xindan
Abstract：In this paper,a three-dimensional model of the trajectory of the missile is established. Combined with the influ?ence of air resistance,earth rotation and wind force,the influence of various factors is comprehensively analyzed to obtain the guid?ance and strike model of the missile.Through the analysis of the movement law of the missile and the consideration of the correspond?ing performance,the relative parameters of the absolute ballistic position of the missile and the position parameters of the movement process are determined,and the ballistic model of the missile is qualitatively and quantitatively analyzed.
Keywords：missile guidance strike modelair resistancethe rotationwind power factor
Publication Date：2019-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：7( 21-26,40 )