舰船电子工程2019，Vol.39Issue(9)：21-26,40,7.DOI:10.3969/j.issn.1672-9730.2019.09.006
陆基导弹的数学模型预算法设计∗
Mathematical Model and Budget Algorithm Design of Land-Based Missile
王少纯 1王哲峰 1陈昱辰 2刘艳龙 1张馨丹3
作者信息
- 1. 沈阳航空航天大学航空宇航学院 沈阳 110000
- 2. 沈阳大学环境工程学院 沈阳 110044
- 3. 沈阳航空航天大学航空发动机学院 沈阳 110000
- 折叠
摘要
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.关键词
导弹制导打击模型/空气阻力/地球自转/风力因素Key words
missile guidance strike model/air resistance/the rotation/wind power factor分类
信息技术与安全科学引用本文复制引用
王少纯,王哲峰,陈昱辰,刘艳龙,张馨丹..陆基导弹的数学模型预算法设计∗[J].舰船电子工程,2019,39(9):21-26,40,7.
