H2 control of singularly perturbed aircraft system

The objective of this research is to develop an analytical approach to control two-time-scale systems operating under certain noise parameters. This approach addresses two important design criteria: augmentation of large-scale system with disturbance model and its two-time-scale representation, and...

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Main Author: Zaveri, Viral Shailesh
Other Authors: Pendse, Ravi
Format: Others
Language:en_US
Published: Wichita State University 2012
Subjects:
Online Access:http://hdl.handle.net/10057/5025
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spelling ndltd-WICHITA-oai-soar.wichita.edu-10057-50252013-04-19T21:00:09ZH2 control of singularly perturbed aircraft systemZaveri, Viral ShaileshElectronic dissertationsThe objective of this research is to develop an analytical approach to control two-time-scale systems operating under certain noise parameters. This approach addresses two important design criteria: augmentation of large-scale system with disturbance model and its two-time-scale representation, and order reduction of the large-scale systems for reduced controller design complexity. The problem of large-scale system with Gaussian noises is solved as the stochastic system implementing linear-quadratic Gaussian control. Order reduction method uses singular perturbation techniques for the simplicity of control algorithms. Control law design process for a singularly perturbed stochastic system includes implementation and comparative analysis of optimal, composite, and reduced controller techniques. Practical model, longitudinal dynamics of digital fly-by-wire F-8C fighter aircraft, illustrates the validation of the proposed concepts.Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Electrical Engineering and Computer Science.Wichita State UniversityPendse, Ravi2012-04-02T18:35:15Z2012-04-02T18:35:15Z20112011-07Thesisxiv, 70 p.t11086http://hdl.handle.net/10057/5025en_US© Copyright 2011 by Viral Shailesh Zaveri. All rights reserved
collection NDLTD
language en_US
format Others
sources NDLTD
topic Electronic dissertations
spellingShingle Electronic dissertations
Zaveri, Viral Shailesh
H2 control of singularly perturbed aircraft system
description The objective of this research is to develop an analytical approach to control two-time-scale systems operating under certain noise parameters. This approach addresses two important design criteria: augmentation of large-scale system with disturbance model and its two-time-scale representation, and order reduction of the large-scale systems for reduced controller design complexity. The problem of large-scale system with Gaussian noises is solved as the stochastic system implementing linear-quadratic Gaussian control. Order reduction method uses singular perturbation techniques for the simplicity of control algorithms. Control law design process for a singularly perturbed stochastic system includes implementation and comparative analysis of optimal, composite, and reduced controller techniques. Practical model, longitudinal dynamics of digital fly-by-wire F-8C fighter aircraft, illustrates the validation of the proposed concepts. === Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Electrical Engineering and Computer Science.
author2 Pendse, Ravi
author_facet Pendse, Ravi
Zaveri, Viral Shailesh
author Zaveri, Viral Shailesh
author_sort Zaveri, Viral Shailesh
title H2 control of singularly perturbed aircraft system
title_short H2 control of singularly perturbed aircraft system
title_full H2 control of singularly perturbed aircraft system
title_fullStr H2 control of singularly perturbed aircraft system
title_full_unstemmed H2 control of singularly perturbed aircraft system
title_sort h2 control of singularly perturbed aircraft system
publisher Wichita State University
publishDate 2012
url http://hdl.handle.net/10057/5025
work_keys_str_mv AT zaveriviralshailesh h2controlofsingularlyperturbedaircraftsystem
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