QFT controller for nonlinear system application to 3-DOF flight control module

In this paper we proposed a new control method based on Quantitative Feedback Theory (QFT) to design practical controller methodology for uncertain characterized with three degree of freedom flight control module. Again linearly least phase systems must sacrifice to desirable feedback control benef...

Full description

Bibliographic Details
Main Authors:	Boby , R. I., Mansor, Hasmah, Za'bah, Nor Farahidah, Abidin, Mohd Shahnan, Gunawan, Teddy Surya, Kazmi, S.A.
Format:	Article
Language:	English
Published:	Asian Research Publishing Network (ARPN) 2016
Subjects:	T Technology (General)
Online Access:	http://irep.iium.edu.my/51105/ http://irep.iium.edu.my/51105/ http://irep.iium.edu.my/51105/1/ARPN2016jeas_0316_3939.pdf

id	iium-51105
recordtype	eprints
spelling	iium-511052016-11-22T03:49:43Z http://irep.iium.edu.my/51105/ QFT controller for nonlinear system application to 3-DOF flight control module Boby , R. I. Mansor, Hasmah Za'bah, Nor Farahidah Abidin, Mohd Shahnan Gunawan, Teddy Surya Kazmi, S.A. T Technology (General) In this paper we proposed a new control method based on Quantitative Feedback Theory (QFT) to design practical controller methodology for uncertain characterized with three degree of freedom flight control module. Again linearly least phase systems must sacrifice to desirable feedback control benefits to avoid an excessive uncertain disturbance. While preserving the robust stability Quantitative Feedback Theory (QFT) controller is proposed to control highly uncertain plants. A 3-DOF flight control system is intrinsically nonlinear, unstable and totally uncertain because of the nature of three individual angles known as pitch, elevation and travel. Most controllers which are designed for 3-DOF helicopter flight systems are base on a minimal linearized model where system variants and uncertainties are not accommodated. Again, the controllers are mostly designed to gratify the gains and phase margin specifications that may not guarantee to handle the sensitivity. In proposed controller QFT may explicitly deal with uncertainty, where large plant parameter uncertainties with lower bandwidth can be achieved by QFT controller. Pre-filter technique may improve both robust stability and robust tracking performance within a desired precision of the individual uncertain parameters of 3-DOF module. This controller may handle large parameter uncertainties and disturbance with rugged stability. The random optimization technique is engaged in the design to optimize the overall performance of the controller. Simulation results and equations are used to show effective result of the proposed control methodology. Asian Research Publishing Network (ARPN) 2016-03-20 Article PeerReviewed application/pdf en http://irep.iium.edu.my/51105/1/ARPN2016jeas_0316_3939.pdf Boby , R. I. and Mansor, Hasmah and Za'bah, Nor Farahidah and Abidin, Mohd Shahnan and Gunawan, Teddy Surya and Kazmi, S.A. (2016) QFT controller for nonlinear system application to 3-DOF flight control module. ARPN Journal of Engineering and Applied Sciences, 11 (6). pp. 4172-4175. ISSN 1819-6608 http://www.arpnjournals.org/jeas/research_papers/rp_2016/jeas_0316_3939.pdf
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) Boby , R. I. Mansor, Hasmah Za'bah, Nor Farahidah Abidin, Mohd Shahnan Gunawan, Teddy Surya Kazmi, S.A. QFT controller for nonlinear system application to 3-DOF flight control module
description	In this paper we proposed a new control method based on Quantitative Feedback Theory (QFT) to design practical controller methodology for uncertain characterized with three degree of freedom flight control module. Again linearly least phase systems must sacrifice to desirable feedback control benefits to avoid an excessive uncertain disturbance. While preserving the robust stability Quantitative Feedback Theory (QFT) controller is proposed to control highly uncertain plants. A 3-DOF flight control system is intrinsically nonlinear, unstable and totally uncertain because of the nature of three individual angles known as pitch, elevation and travel. Most controllers which are designed for 3-DOF helicopter flight systems are base on a minimal linearized model where system variants and uncertainties are not accommodated. Again, the controllers are mostly designed to gratify the gains and phase margin specifications that may not guarantee to handle the sensitivity. In proposed controller QFT may explicitly deal with uncertainty, where large plant parameter uncertainties with lower bandwidth can be achieved by QFT controller. Pre-filter technique may improve both robust stability and robust tracking performance within a desired precision of the individual uncertain parameters of 3-DOF module. This controller may handle large parameter uncertainties and disturbance with rugged stability. The random optimization technique is engaged in the design to optimize the overall performance of the controller. Simulation results and equations are used to show effective result of the proposed control methodology.
format	Article
author	Boby , R. I. Mansor, Hasmah Za'bah, Nor Farahidah Abidin, Mohd Shahnan Gunawan, Teddy Surya Kazmi, S.A.
author_facet	Boby , R. I. Mansor, Hasmah Za'bah, Nor Farahidah Abidin, Mohd Shahnan Gunawan, Teddy Surya Kazmi, S.A.
author_sort	Boby , R. I.
title	QFT controller for nonlinear system application to 3-DOF flight control module
title_short	QFT controller for nonlinear system application to 3-DOF flight control module
title_full	QFT controller for nonlinear system application to 3-DOF flight control module
title_fullStr	QFT controller for nonlinear system application to 3-DOF flight control module
title_full_unstemmed	QFT controller for nonlinear system application to 3-DOF flight control module
title_sort	qft controller for nonlinear system application to 3-dof flight control module
publisher	Asian Research Publishing Network (ARPN)
publishDate	2016
url	http://irep.iium.edu.my/51105/ http://irep.iium.edu.my/51105/ http://irep.iium.edu.my/51105/1/ARPN2016jeas_0316_3939.pdf
first_indexed	2023-09-18T21:12:18Z
last_indexed	2023-09-18T21:12:18Z
_version_	1777411333961023488

QFT controller for nonlinear system application to 3-DOF flight control module

Similar Items