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^*

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

31 Citations (Scopus)

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.

Original language	English
Pages (from-to)	1063-1070
Number of pages	8
Journal	International Journal of Control
Volume	85
Issue number	8
DOIs	https://doi.org/10.1080/00207179.2012.675519
Publication status	Published - 1 Aug 2012

Keywords

hamiltonian
many-to-one guidance
optimal control theory
optimal guidance law

Access to Document

10.1080/00207179.2012.675519

Cite this

@article{a4b120a224f347e5a6316ddf5a0c0339,

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",

year = "2012",

month = aug,

day = "1",

doi = "10.1080/00207179.2012.675519",

language = "English",

volume = "85",

pages = "1063--1070",

journal = "International Journal of Control",

issn = "0020-7179",

publisher = "Taylor and Francis Ltd.",

number = "8",

}

TY - JOUR

T1 - Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory

AU - Sun, Xiao

AU - Xia, Yuanqing

PY - 2012/8/1

Y1 - 2012/8/1

N2 - 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.

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.

KW - hamiltonian

KW - many-to-one guidance

KW - optimal control theory

KW - optimal guidance law

UR - http://www.scopus.com/inward/record.url?scp=84863599394&partnerID=8YFLogxK

U2 - 10.1080/00207179.2012.675519

DO - 10.1080/00207179.2012.675519

M3 - Article

AN - SCOPUS:84863599394

SN - 0020-7179

VL - 85

SP - 1063

EP - 1070

JO - International Journal of Control

JF - International Journal of Control

IS - 8

ER -

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

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this