Optimized state feedback regulation of 3DOF helicopter system via extremum seeking

In this paper, an optimized state feedback regulation of a 3 degree of freedom (DOF) helicopter is designed via extremum seeking (ES) technique. Multi-parameter ES is applied to optimize the tracking performance via tuning State Vector Feedback with Integration of the Control Error (SVFBICE). Discr...

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Main Authors: Akmeliawati, Rini, Raafat, Safanah M.
Format: Conference or Workshop Item
Language:English
English
Published: 2013
Subjects:
Online Access:http://irep.iium.edu.my/31778/
http://irep.iium.edu.my/31778/
http://irep.iium.edu.my/31778/1/ascc2013.pdf
http://irep.iium.edu.my/31778/4/1371543137RegisteredList03062013_R_Akmeliawati.pdf
id iium-31778
recordtype eprints
spelling iium-317782013-10-02T04:42:32Z http://irep.iium.edu.my/31778/ Optimized state feedback regulation of 3DOF helicopter system via extremum seeking Akmeliawati, Rini Raafat, Safanah M. TJ212 Control engineering In this paper, an optimized state feedback regulation of a 3 degree of freedom (DOF) helicopter is designed via extremum seeking (ES) technique. Multi-parameter ES is applied to optimize the tracking performance via tuning State Vector Feedback with Integration of the Control Error (SVFBICE). Discrete multivariable version of ES is developed to minimize a cost function that measures the performance of the controller. The cost function is a function of the error between the actual and desired axis positions. The controller parameters are updated online as the optimization takes place. This method significantly decreases the time in obtaining optimal controller parameters. Simulations were conducted for the online optimization under both fixed and varying operating conditions. The results demonstrate the usefulness of using ES for preserving the maximum attainable performance. 2013 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/31778/1/ascc2013.pdf application/pdf en http://irep.iium.edu.my/31778/4/1371543137RegisteredList03062013_R_Akmeliawati.pdf Akmeliawati, Rini and Raafat, Safanah M. (2013) Optimized state feedback regulation of 3DOF helicopter system via extremum seeking. In: Asian Control Conference (ASCC 2013), 23-26 June 2013, Istanbul . http://www.ascc.boun.edu.tr/
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
English
topic TJ212 Control engineering
spellingShingle TJ212 Control engineering
Akmeliawati, Rini
Raafat, Safanah M.
Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
description In this paper, an optimized state feedback regulation of a 3 degree of freedom (DOF) helicopter is designed via extremum seeking (ES) technique. Multi-parameter ES is applied to optimize the tracking performance via tuning State Vector Feedback with Integration of the Control Error (SVFBICE). Discrete multivariable version of ES is developed to minimize a cost function that measures the performance of the controller. The cost function is a function of the error between the actual and desired axis positions. The controller parameters are updated online as the optimization takes place. This method significantly decreases the time in obtaining optimal controller parameters. Simulations were conducted for the online optimization under both fixed and varying operating conditions. The results demonstrate the usefulness of using ES for preserving the maximum attainable performance.
format Conference or Workshop Item
author Akmeliawati, Rini
Raafat, Safanah M.
author_facet Akmeliawati, Rini
Raafat, Safanah M.
author_sort Akmeliawati, Rini
title Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
title_short Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
title_full Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
title_fullStr Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
title_full_unstemmed Optimized state feedback regulation of 3DOF helicopter system via extremum seeking
title_sort optimized state feedback regulation of 3dof helicopter system via extremum seeking
publishDate 2013
url http://irep.iium.edu.my/31778/
http://irep.iium.edu.my/31778/
http://irep.iium.edu.my/31778/1/ascc2013.pdf
http://irep.iium.edu.my/31778/4/1371543137RegisteredList03062013_R_Akmeliawati.pdf
first_indexed 2023-09-18T20:45:56Z
last_indexed 2023-09-18T20:45:56Z
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