现代防御技术2017，Vol.45Issue(1)：18-21,4.DOI:10.3969/j.issn.1009-086x.2017.01.004
一种基于过重力补偿的双角度约束制导律研究
Terminal Impact Angle and Seeker Gimbals Angle Control Based on Proportional Navigation Guidance Law with Over-Gravity Compensation
李锦 1张锐1
作者信息
- 1. 北京电子工程总体研究所,北京100854
- 折叠
摘要
Abstract
In order to improve passive homing missile impact angle to meet large impact angle con straint under the condition of low flat flight trajectory,a method of modified proportional navigation to is designed.Over-gravity compensation is added to proportional navigation,and the seeker gimbals angle control term is also added.The simulation indicates that the modified proportional navigation guidance law can meet the demand of large impact angle and seeker gimbals angle constraint.关键词
反坦克导弹/大落角/导引头框架角/修正比例导引/平飞弹道/重力补偿Key words
antitank missile/large impact angle/seeker gimbals angle/modified proportional guidance law/flat flight trajectory/over-gravity compensation分类
军事科技引用本文复制引用
李锦,张锐..一种基于过重力补偿的双角度约束制导律研究[J].现代防御技术,2017,45(1):18-21,4.
