Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory

Xiao Sun; Yuanqing Xia

doi:10.1080/00207179.2012.675519

Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory

Xiao Sun
, Yuanqing Xia^*

^*此作品的通讯作者

自动化学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

32 引用（Scopus）

摘要

This article considers the problem of optimal guidance laws for cooperative attack of multiple missiles based on the optimal control theory. New guidance laws are presented such that multiple missiles attack a single target simultaneously. Simulation results show the effectiveness of the proposed algorithms.

源语言	英语
页（从-至）	1063-1070
页数	8
期刊	International Journal of Control
卷	85
期	8
DOI	https://doi.org/10.1080/00207179.2012.675519
出版状态	已出版 - 1 8月 2012

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title = "Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory",

abstract = "This article considers the problem of optimal guidance laws for cooperative attack of multiple missiles based on the optimal control theory. New guidance laws are presented such that multiple missiles attack a single target simultaneously. Simulation results show the effectiveness of the proposed algorithms.",

keywords = "hamiltonian, many-to-one guidance, optimal control theory, optimal guidance law",

author = "Xiao Sun and Yuanqing Xia",

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AB - This article considers the problem of optimal guidance laws for cooperative attack of multiple missiles based on the optimal control theory. New guidance laws are presented such that multiple missiles attack a single target simultaneously. Simulation results show the effectiveness of the proposed algorithms.

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KW - optimal guidance law

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Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory

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