Design for a terminal guidance law of the interceptor by combined control

Yin Yongxin; Zhang Yuping; Yang Ming

doi:10.1109/WCICA.2006.1713121

Design for a terminal guidance law of the interceptor by combined control

Yin Yongxin^*
, Zhang Yuping
, Yang Ming

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
Harbin University of Science and Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

A fuzzy variable structure terminal guidance law is presented for combined control interceptor in aerosphere. After constructing the relative movement between the target and interceptor, a fuzzy logic control is designed for tuning the variable structure guidance law. This guidance law needs no information on the motion of the target, it is simple to control the interceptor and is convenient for practical project, which demonstrate the advantage of fuzzy variable structure guidance law. Simulation results show that this guidance law reduces the chattering for high-speed maneuverable target, and it can also implement efficiently the precise guidance of the interceptor as well as preferable robust stability.

Original language	English
Title of host publication	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Pages	3987-3991
Number of pages	5
DOIs	https://doi.org/10.1109/WCICA.2006.1713121
State	Published - 2006
Event	6th World Congress on Intelligent Control and Automation, WCICA 2006 - Dalian, China Duration: 21 Jun 2006 → 23 Jun 2006

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Volume	1

Conference

Conference	6th World Congress on Intelligent Control and Automation, WCICA 2006
Country/Territory	China
City	Dalian
Period	21/06/06 → 23/06/06

Keywords

Fuzzy logic
Guidance law
Interceptor
Variable structure control

Access to Document

10.1109/WCICA.2006.1713121

Cite this

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title = "Design for a terminal guidance law of the interceptor by combined control",

abstract = "A fuzzy variable structure terminal guidance law is presented for combined control interceptor in aerosphere. After constructing the relative movement between the target and interceptor, a fuzzy logic control is designed for tuning the variable structure guidance law. This guidance law needs no information on the motion of the target, it is simple to control the interceptor and is convenient for practical project, which demonstrate the advantage of fuzzy variable structure guidance law. Simulation results show that this guidance law reduces the chattering for high-speed maneuverable target, and it can also implement efficiently the precise guidance of the interceptor as well as preferable robust stability.",

keywords = "Fuzzy logic, Guidance law, Interceptor, Variable structure control",

author = "Yin Yongxin and Zhang Yuping and Yang Ming",

year = "2006",

doi = "10.1109/WCICA.2006.1713121",

language = "英语",

isbn = "1424403324",

series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

pages = "3987--3991",

booktitle = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

note = "6th World Congress on Intelligent Control and Automation, WCICA 2006 ; Conference date: 21-06-2006 Through 23-06-2006",

}

Yongxin, Y, Yuping, Z & Ming, Y 2006, Design for a terminal guidance law of the interceptor by combined control. in Proceedings of the World Congress on Intelligent Control and Automation (WCICA)., 1713121, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), vol. 1, pp. 3987-3991, 6th World Congress on Intelligent Control and Automation, WCICA 2006, Dalian, China, 21/06/06. https://doi.org/10.1109/WCICA.2006.1713121

Design for a terminal guidance law of the interceptor by combined control. / Yongxin, Yin; Yuping, Zhang; Ming, Yang.
Proceedings of the World Congress on Intelligent Control and Automation (WCICA). 2006. p. 3987-3991 1713121 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 1).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Yongxin, Yin

AU - Yuping, Zhang

AU - Ming, Yang

PY - 2006

Y1 - 2006

N2 - A fuzzy variable structure terminal guidance law is presented for combined control interceptor in aerosphere. After constructing the relative movement between the target and interceptor, a fuzzy logic control is designed for tuning the variable structure guidance law. This guidance law needs no information on the motion of the target, it is simple to control the interceptor and is convenient for practical project, which demonstrate the advantage of fuzzy variable structure guidance law. Simulation results show that this guidance law reduces the chattering for high-speed maneuverable target, and it can also implement efficiently the precise guidance of the interceptor as well as preferable robust stability.

AB - A fuzzy variable structure terminal guidance law is presented for combined control interceptor in aerosphere. After constructing the relative movement between the target and interceptor, a fuzzy logic control is designed for tuning the variable structure guidance law. This guidance law needs no information on the motion of the target, it is simple to control the interceptor and is convenient for practical project, which demonstrate the advantage of fuzzy variable structure guidance law. Simulation results show that this guidance law reduces the chattering for high-speed maneuverable target, and it can also implement efficiently the precise guidance of the interceptor as well as preferable robust stability.

KW - Fuzzy logic

KW - Guidance law

KW - Interceptor

KW - Variable structure control

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DO - 10.1109/WCICA.2006.1713121

M3 - 会议稿件

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BT - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

T2 - 6th World Congress on Intelligent Control and Automation, WCICA 2006

Y2 - 21 June 2006 through 23 June 2006

ER -

Design for a terminal guidance law of the interceptor by combined control

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Keywords

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