Robust Controller Design for Missile Yaw Channel
سال
: 2008
چکیده: 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.
کلیدواژه(گان): “Robust control”,“QFT”,“Uncertainty”,“Dynamic model”,“Missile”
کالکشن
:
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آمار بازدید
Robust Controller Design for Missile Yaw Channel
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contributor author | مجید معاونیان | en |
contributor author | محمدرضا قریب | en |
contributor author | مهدی شهاب | en |
contributor author | Majid Moavenian | fa |
contributor author | MohammadReza Gharib | fa |
date accessioned | 2020-06-06T13:51:55Z | |
date available | 2020-06-06T13:51:55Z | |
date copyright | 2/21/2008 | |
date issued | 2008 | |
identifier uri | http://libsearch.um.ac.ir:80/fum/handle/fum/3372436 | |
description 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. | en |
language | English | |
title | Robust Controller Design for Missile Yaw Channel | en |
type | Conference Paper | |
contenttype | External Fulltext | |
subject keywords | “Robust control” | en |
subject keywords | “QFT” | en |
subject keywords | “Uncertainty” | en |
subject keywords | “Dynamic model” | en |
subject keywords | “Missile” | en |
identifier link | https://profdoc.um.ac.ir/paper-abstract-1008121.html | |
conference title | The 7th Iranian Aerospace Society Conference | en |
conference location | تهران | fa |
identifier articleid | 1008121 |