DE-based robust controller design for helicopter cruise control

This paper presents a robust state feedback controller tuning via constrained optimization using DE (differential evolution). The controller gain is optimized based on the plant model such that the closed-loop system achieves maximum stability radius. The desired control performance is specified by...

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Main Authors: Mahmud, Iwan, Akmeliawati, Rini, Budiyono, Agus
Format: Article
Language:English
Published: UNSYS digital 2014
Subjects:
Online Access:http://irep.iium.edu.my/41757/
http://irep.iium.edu.my/41757/
http://irep.iium.edu.my/41757/1/iwanIJRM2014.pdf
id iium-41757
recordtype eprints
spelling iium-417572015-04-17T02:03:54Z http://irep.iium.edu.my/41757/ DE-based robust controller design for helicopter cruise control Mahmud, Iwan Akmeliawati, Rini Budiyono, Agus TJ212 Control engineering This paper presents a robust state feedback controller tuning via constrained optimization using DE (differential evolution). The controller gain is optimized based on the plant model such that the closed-loop system achieves maximum stability radius. The desired control performance is specified by assigning closed-loop poles region which is handled as a constraint in the DE-based optimization. The proposed controller design technique is applied to a longitudinal cruise control of a small-scale helicopter. The control of small-scale helicopter is a MIMO problem which increases the complexity of the controller design task. The proposed controller design attempts to simplify this complicated task where the automated design is employed via DE-based modern optimization. The effectiveness of the proposed controller design technique is presented by comparing its performance with that of conventional LQR-based controllers in computer simulation. UNSYS digital 2014 Article PeerReviewed application/pdf en http://irep.iium.edu.my/41757/1/iwanIJRM2014.pdf Mahmud, Iwan and Akmeliawati, Rini and Budiyono, Agus (2014) DE-based robust controller design for helicopter cruise control. International Journal of Robotics and Mechatronics, 1 (4). pp. 145-151. ISSN 2288-5889 http://ojs.unsysdigital.com/index.php/ijrm
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TJ212 Control engineering
spellingShingle TJ212 Control engineering
Mahmud, Iwan
Akmeliawati, Rini
Budiyono, Agus
DE-based robust controller design for helicopter cruise control
description This paper presents a robust state feedback controller tuning via constrained optimization using DE (differential evolution). The controller gain is optimized based on the plant model such that the closed-loop system achieves maximum stability radius. The desired control performance is specified by assigning closed-loop poles region which is handled as a constraint in the DE-based optimization. The proposed controller design technique is applied to a longitudinal cruise control of a small-scale helicopter. The control of small-scale helicopter is a MIMO problem which increases the complexity of the controller design task. The proposed controller design attempts to simplify this complicated task where the automated design is employed via DE-based modern optimization. The effectiveness of the proposed controller design technique is presented by comparing its performance with that of conventional LQR-based controllers in computer simulation.
format Article
author Mahmud, Iwan
Akmeliawati, Rini
Budiyono, Agus
author_facet Mahmud, Iwan
Akmeliawati, Rini
Budiyono, Agus
author_sort Mahmud, Iwan
title DE-based robust controller design for helicopter cruise control
title_short DE-based robust controller design for helicopter cruise control
title_full DE-based robust controller design for helicopter cruise control
title_fullStr DE-based robust controller design for helicopter cruise control
title_full_unstemmed DE-based robust controller design for helicopter cruise control
title_sort de-based robust controller design for helicopter cruise control
publisher UNSYS digital
publishDate 2014
url http://irep.iium.edu.my/41757/
http://irep.iium.edu.my/41757/
http://irep.iium.edu.my/41757/1/iwanIJRM2014.pdf
first_indexed 2023-09-18T20:59:42Z
last_indexed 2023-09-18T20:59:42Z
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