导弹制导
导弹
弹道
灵敏度(控制系统)
比例导航
法学
弹药
制导系统
点(几何)
控制理论(社会学)
计算机科学
关系(数据库)
工程类
航空航天工程
人工智能
数学
政治学
物理
控制(管理)
地理
数据挖掘
考古
天文
电子工程
几何学
作者
Woosung Park,Joongsup Yun,Chang-Kyung Ryoo,Yong-Ho Kim
出处
期刊:ICCAS 2010
日期:2010-10-01
被引量:3
标识
DOI:10.1109/iccas.2010.5669937
摘要
While the PN (Proportional Navigation) guidance is known generally in the study of the missile guidance, there are not broadly known guidance laws for the munitions. Some guidance laws like the Impact Point Prediction, Modified Proportional Navigation Guidance, and Neural Network are considered currently. In this paper, we suggest the new guidance law of using the sensitivity. The sensitivity is a value about the relationship between the variation of velocity and the impact point error. Finally, we simulate the trajectory correction of the munition through this guidance law.
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