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Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique

A three degree of freedom (3-DOF) bench-top helicopter is a simplified aerial vehicle which is used to study the behaviors of the helicopter as well as testing multiple flight control approaches for their efficiency. Designing helicopter’s dynamic control is a challenging task due to the presence of...

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Main Authors: Mohd Hairon, A. H., Mansor, Hasmah, Gunawan, Teddy Surya, Khan, Sheroz
Format: Article
Language:English
English
Published: Institute of Advanced Engineering and Science (IAES) 2016
Subjects:
T Technology (General)
Online Access:http://irep.iium.edu.my/49983/1/252-116-1-PB_Telkonminika_Published.pdf
http://irep.iium.edu.my/49983/4/49983_Travel%20angle%20control%20of%20quanser_SCOPUS.pdf
http://irep.iium.edu.my/49983/
http://www.iaesjournal.com/online/index.php/TELKOMNIKA/article/view/9723
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spelling my.iium.irep.499832017-04-12T04:21:56Z http://irep.iium.edu.my/49983/ Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique Mohd Hairon, A. H. Mansor, Hasmah Gunawan, Teddy Surya Khan, Sheroz T Technology (General) A three degree of freedom (3-DOF) bench-top helicopter is a simplified aerial vehicle which is used to study the behaviors of the helicopter as well as testing multiple flight control approaches for their efficiency. Designing helicopter’s dynamic control is a challenging task due to the presence of high uncertainties and non-linear behavior. The main objective of this research is to achieve robust control over the helicopter model regardless parameter variation and disturbances using robust control technique, Quantitative Feedback Theory (QFT). QFT utilizes frequency domain methodology which ensures plant’s stability by considering the feedback of the system and thus removing the effect of disturbances and reducing sensitivity of parameter’s variation. The proposed technique is tested against LQR-tuned PID controller in both simulation and real hardware environment to verify its performance. The results obtained shown us that QFT algorithm managed to reduce settling time and steady state error of about 80% and 33% respectively over the classical PID controller. Institute of Advanced Engineering and Science (IAES) 2016-02 Article REM application/pdf en http://irep.iium.edu.my/49983/1/252-116-1-PB_Telkonminika_Published.pdf application/pdf en http://irep.iium.edu.my/49983/4/49983_Travel%20angle%20control%20of%20quanser_SCOPUS.pdf Mohd Hairon, A. H. and Mansor, Hasmah and Gunawan, Teddy Surya and Khan, Sheroz (2016) Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique. Indonesian Journal of Electrical Engineering and Computer Science, 1 (2). pp. 310-318. ISSN 2502-4752 http://www.iaesjournal.com/online/index.php/TELKOMNIKA/article/view/9723 10.11591/ijeecs.v1.i2.pp310-318
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic T Technology (General)
spellingShingle T Technology (General)
Mohd Hairon, A. H.
Mansor, Hasmah
Gunawan, Teddy Surya
Khan, Sheroz
Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
description A three degree of freedom (3-DOF) bench-top helicopter is a simplified aerial vehicle which is used to study the behaviors of the helicopter as well as testing multiple flight control approaches for their efficiency. Designing helicopter’s dynamic control is a challenging task due to the presence of high uncertainties and non-linear behavior. The main objective of this research is to achieve robust control over the helicopter model regardless parameter variation and disturbances using robust control technique, Quantitative Feedback Theory (QFT). QFT utilizes frequency domain methodology which ensures plant’s stability by considering the feedback of the system and thus removing the effect of disturbances and reducing sensitivity of parameter’s variation. The proposed technique is tested against LQR-tuned PID controller in both simulation and real hardware environment to verify its performance. The results obtained shown us that QFT algorithm managed to reduce settling time and steady state error of about 80% and 33% respectively over the classical PID controller.
format Article
author Mohd Hairon, A. H.
Mansor, Hasmah
Gunawan, Teddy Surya
Khan, Sheroz
author_facet Mohd Hairon, A. H.
Mansor, Hasmah
Gunawan, Teddy Surya
Khan, Sheroz
author_sort Mohd Hairon, A. H.
title Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
title_short Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
title_full Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
title_fullStr Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
title_full_unstemmed Travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
title_sort travel angle control of quanser bench-top helicopter based on quantitative feedback theory technique
publisher Institute of Advanced Engineering and Science (IAES)
publishDate 2016
url http://irep.iium.edu.my/49983/1/252-116-1-PB_Telkonminika_Published.pdf
http://irep.iium.edu.my/49983/4/49983_Travel%20angle%20control%20of%20quanser_SCOPUS.pdf
http://irep.iium.edu.my/49983/
http://www.iaesjournal.com/online/index.php/TELKOMNIKA/article/view/9723
_version_ 1643613638076923904
score 13.211869

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