Robust control of bench-top helicopter using quantitative feedback theory

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...

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Main Authors:	Mohd. Hairon, Ameerul Hakeem, Mansor, Hasmah, Gunawan, Teddy Surya, Khan, Sheroz
Format:	Article
Language:	English
Published:	Institute of Advanced Engineering and Science (IAES) in collaboration with Universitas Ahmad Dahlan (UAD) 2015
Subjects:	T Technology (General)
Online Access:	http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/1/7899-17730-1-PBAmeerulTekomnikaJournal.pdf

id	iium-43701
recordtype	eprints
spelling	iium-437012017-11-30T11:51:08Z http://irep.iium.edu.my/43701/ Robust control of bench-top helicopter using quantitative feedback theory Mohd. Hairon, Ameerul Hakeem 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. In this study, Quantitative Feedback Theory (QFT) is proposed to achieve robust control over the helicopter model. It 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 to demonstrate its procedures as well as its performance. Simulation results obtained through MATLAB Simulink software shown us that QFT algorithm managed to reduce percentage of overshoot and settling time about 50% and 30% respectively over the classical PID controller. Institute of Advanced Engineering and Science (IAES) in collaboration with Universitas Ahmad Dahlan (UAD) 2015-06 Article PeerReviewed application/pdf en http://irep.iium.edu.my/43701/1/7899-17730-1-PBAmeerulTekomnikaJournal.pdf Mohd. Hairon, Ameerul Hakeem and Mansor, Hasmah and Gunawan, Teddy Surya and Khan, Sheroz (2015) Robust control of bench-top helicopter using quantitative feedback theory. TELKOMNIKA Indonesian Journal of Electrical Engineering, 14 (3). pp. 500-507. ISSN 2087-278X (O), 2302-4046 (P) http://www.iaesjournal.com/online/index.php/TELKOMNIKA/article/view/7899 10.11591/telkomnika.v14i3.7899
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	T Technology (General)
spellingShingle	T Technology (General) Mohd. Hairon, Ameerul Hakeem Mansor, Hasmah Gunawan, Teddy Surya Khan, Sheroz Robust control of bench-top helicopter using quantitative feedback theory
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. In this study, Quantitative Feedback Theory (QFT) is proposed to achieve robust control over the helicopter model. It 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 to demonstrate its procedures as well as its performance. Simulation results obtained through MATLAB Simulink software shown us that QFT algorithm managed to reduce percentage of overshoot and settling time about 50% and 30% respectively over the classical PID controller.
format	Article
author	Mohd. Hairon, Ameerul Hakeem Mansor, Hasmah Gunawan, Teddy Surya Khan, Sheroz
author_facet	Mohd. Hairon, Ameerul Hakeem Mansor, Hasmah Gunawan, Teddy Surya Khan, Sheroz
author_sort	Mohd. Hairon, Ameerul Hakeem
title	Robust control of bench-top helicopter using quantitative feedback theory
title_short	Robust control of bench-top helicopter using quantitative feedback theory
title_full	Robust control of bench-top helicopter using quantitative feedback theory
title_fullStr	Robust control of bench-top helicopter using quantitative feedback theory
title_full_unstemmed	Robust control of bench-top helicopter using quantitative feedback theory
title_sort	robust control of bench-top helicopter using quantitative feedback theory
publisher	Institute of Advanced Engineering and Science (IAES) in collaboration with Universitas Ahmad Dahlan (UAD)
publishDate	2015
url	http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/ http://irep.iium.edu.my/43701/1/7899-17730-1-PBAmeerulTekomnikaJournal.pdf
first_indexed	2023-09-18T21:02:13Z
last_indexed	2023-09-18T21:02:13Z
_version_	1777410698909843456

Robust control of bench-top helicopter using quantitative feedback theory

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