.png){kind=icon}
返回
Active target defense using first order missile models
.png){kind=icon}
PRE
AI
DOI：10.1016/j.automatica.2016.12.032.png)
.png){kind=icon}
原文求助.png){kind=icon}
分享.png){kind=icon}
收藏
摘要
En 中文
In this note the active target defense scenario is analyzed. This entails a Target aircraft being pursued by an Attacker missile while a Defender missile is launched by the Target or by a Target-friendly platform to intercept the Attacker missile. The missiles are modeled using first order dynamics and implement Pure Pursuit guidance laws but are subject to turning rate constraints. The Target's optimal heading is obtained such that the Defender intercepts the Attacker and the terminal Target/Attacker separation is maximized. This work offers more realistic results compared to previous work where simple motion kinematics were used, that is, it was assumed that the missiles are able to turn infinitely fast. Published by Elsevier Ltd.
Keyword:
Optimal control
Missile guidance
Cooperative control
AI总结
对已上传原文的论文进行重点信息的提取，主要内容包括：简要概述、研究摘要、背景介绍、关键亮点、图文解析、展望与总结。
期刊
IF:
5.9
论文数:
1.2W
被引数:
5.2W
机构
引用论文
Interfacial treatment effects on behavior of soft nano-composites for highly stretchable dielectrics.png)
Polymer
OAAI
PolymerIF0
OAAI分享收藏
查看更多内容