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...
Main Author: | |
---|---|
Other Authors: | |
Format: | Others |
Language: | en_US |
Published: |
Wichita State University
2012
|
Subjects: | |
Online Access: | http://hdl.handle.net/10057/5025 |
id |
ndltd-WICHITA-oai-soar.wichita.edu-10057-5025 |
---|---|
record_format |
oai_dc |
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 |
_version_ |
1716583183535833088 |