指挥控制与仿真2016，Vol.38Issue(5)：119-122,4.DOI:10.3969/j.issn.1673-3819.2016.05.026
助推段反导的动能拦截弹导引律设计
Guidance Law Design for Kinetic Interceptor for Antimissile in Boost P hase
董杰 1张正成 1刘宗福1
作者信息
- 1. 解放军92785部队，河北 秦皇岛 066200
- 折叠
摘要
Abstract
In order to decrease the required overload, the air⁃based kinetic interceptor�s guidance law for boost phase anti⁃missile was analyzed and researched. The navigation guidance system model and correction factor were proposed to analyze the required overload at the impact intercept point. Distinguishing the situations with or without the distance error of predicted intercept point, the interception trajectory and the overload dynamic response were analyzed and simulated. The simulation results showed that, the guidance law can reduce the available overload and accomplish interception and collision.关键词
空基反导/助推段/动能拦截弹/修正比例导引Key words
air-based antimissile/boost phase/kinetic interceptor/amendatory proportional navigation分类
军事科技引用本文复制引用
董杰,张正成,刘宗福..助推段反导的动能拦截弹导引律设计[J].指挥控制与仿真,2016,38(5):119-122,4.
