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/ http://irep.iium.edu.my/49983/ http://irep.iium.edu.my/49983/ 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

id	iium-49983
recordtype	eprints
spelling	iium-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 PeerReviewed 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 E-ISSN 2502-4760 http://www.iaesjournal.com/online/index.php/TELKOMNIKA/article/view/9723 10.11591/ijeecs.v1.i2.pp310-318
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
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/ http://irep.iium.edu.my/49983/ http://irep.iium.edu.my/49983/ 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
first_indexed	2023-09-18T21:10:38Z
last_indexed	2023-09-18T21:10:38Z
_version_	1777411228320137216

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

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