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Robust Controller Design for Missile Yaw Channel

Author:
مجید معاونیان
,
محمدرضا قریب
,
مهدی شهاب
,
Majid Moavenian
,
MohammadReza Gharib
Year
: 2008
Abstract: Quantitative design of robust control systems proposes a transparent and practical controller design methodology for uncertain single-input single-output and multivariable plants. There are several steps involved in the design of such controllers. The main steps involved in the design are template generation, loop shaping and pre-filter design. In this paper, a useful method to design a robust controller for yaw channel of a missile, using quantitative feedback theory (QFT) is proposed. Results are used to show the effectiveness of the proposed method.
URI: http://libsearch.um.ac.ir:80/fum/handle/fum/3372436
Keyword(s): “Robust control”,“QFT”,“Uncertainty”,“Dynamic model”,“Missile”
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    Robust Controller Design for Missile Yaw Channel

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contributor authorمجید معاونیانen
contributor authorمحمدرضا قریبen
contributor authorمهدی شهابen
contributor authorMajid Moavenianfa
contributor authorMohammadReza Gharibfa
date accessioned2020-06-06T13:51:55Z
date available2020-06-06T13:51:55Z
date copyright2/21/2008
date issued2008
identifier urihttp://libsearch.um.ac.ir:80/fum/handle/fum/3372436?locale-attribute=en
description abstractQuantitative design of robust control systems proposes a transparent and practical controller design methodology for uncertain single-input single-output and multivariable plants. There are several steps involved in the design of such controllers. The main steps involved in the design are template generation, loop shaping and pre-filter design. In this paper, a useful method to design a robust controller for yaw channel of a missile, using quantitative feedback theory (QFT) is proposed. Results are used to show the effectiveness of the proposed method.en
languageEnglish
titleRobust Controller Design for Missile Yaw Channelen
typeConference Paper
contenttypeExternal Fulltext
subject keywords“Robust control”en
subject keywords“QFT”en
subject keywords“Uncertainty”en
subject keywords“Dynamic model”en
subject keywords“Missile”en
identifier linkhttps://profdoc.um.ac.ir/paper-abstract-1008121.html
conference titleThe 7th Iranian Aerospace Society Conferenceen
conference locationتهرانfa
identifier articleid1008121
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