Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers

Recent trend of living is getting modernized rapidly by the involvement of automatic systems. Within the aviation industry, automatic systems had become heavily reliable by the end of the nineteen centuries. The systems usually require controllable devices with desired control...

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Main Authors: Anwar, Farhat, Islam, Rounakul, Mansor, Hasmah, Hussain, Sabahat, Sharmin, Afsah
Format: Article
Language:English
English
Published: Institute of Advanced Engineering and Science 2017
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Online Access:http://irep.iium.edu.my/60105/1/10032-12450-1-PB%20%28IJEECS-NOV-2017%29.pdf
http://irep.iium.edu.my/60105/7/Development%20of%20approximate%20prediction%20model%20for%203-DOF%20helicopter%20and%20benchmarking%20with%20existing%20controllers.pdf
http://irep.iium.edu.my/60105/
http://www.iaesjournal.com/online/index.php/IJEECS/article/view/17168
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Institution: Universiti Islam Antarabangsa Malaysia
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spelling my.iium.irep.601052019-12-04T00:21:11Z http://irep.iium.edu.my/60105/ Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers Anwar, Farhat Islam, Rounakul Mansor, Hasmah Hussain, Sabahat Sharmin, Afsah TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices Recent trend of living is getting modernized rapidly by the involvement of automatic systems. Within the aviation industry, automatic systems had become heavily reliable by the end of the nineteen centuries. The systems usually require controllable devices with desired control algorithm known as controller. Controllers can be replaced with, almost every mechanical automation aspect where, safety is a serious issue. But it is not easy to adapt a controller with a specific model at the beginning. It is important to predict the model before a controller works on the model and the controller parameters need to be adapted to get maximum efficiency. A 3-DOF (Three Degrees of Freedom) airframe model is an advanced benchmark model of real 3-DOF helicopter. It has the same uncommon model dynamics with nonlinearities, strong duel motor cross coupling system, uncertain characteristics, disturbances dependent, unmodeled dynamics and many more. The 3-DOF airframe model is a well-known platform for controller performance benchmarking. This research paper shows the development of an approximate prediction model of a Three Degrees of Freedom helicopter model and uses the proposed approximate model to observe the performance of an existent hybrid controller. The hybrid controller is the combination of two different controllers named Quantitative Feedback Theory (QFT) controller and Adaptive controller.To achieve the research objective, the proposed mathematical model of this airframe was used to develop transfer function and simulate with the hybrid controller in MATLAB. The performance of the controller based on the proposed heliframe model of 3-DOF helicopter have also been reported added within this paper. Institute of Advanced Engineering and Science 2017-11 Article PeerReviewed application/pdf en http://irep.iium.edu.my/60105/1/10032-12450-1-PB%20%28IJEECS-NOV-2017%29.pdf application/pdf en http://irep.iium.edu.my/60105/7/Development%20of%20approximate%20prediction%20model%20for%203-DOF%20helicopter%20and%20benchmarking%20with%20existing%20controllers.pdf Anwar, Farhat and Islam, Rounakul and Mansor, Hasmah and Hussain, Sabahat and Sharmin, Afsah (2017) Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers. Indonesian Journal of Electrical Engineering and Computer Science, 8 (2). pp. 502-510. ISSN 2502-4752 E-ISSN 2502-4760 http://www.iaesjournal.com/online/index.php/IJEECS/article/view/17168 10.11591/ijeecs.v8.i2.pp502-510
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 TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices
spellingShingle TK7800 Electronics. Computer engineering. Computer hardware. Photoelectronic devices
Anwar, Farhat
Islam, Rounakul
Mansor, Hasmah
Hussain, Sabahat
Sharmin, Afsah
Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
description Recent trend of living is getting modernized rapidly by the involvement of automatic systems. Within the aviation industry, automatic systems had become heavily reliable by the end of the nineteen centuries. The systems usually require controllable devices with desired control algorithm known as controller. Controllers can be replaced with, almost every mechanical automation aspect where, safety is a serious issue. But it is not easy to adapt a controller with a specific model at the beginning. It is important to predict the model before a controller works on the model and the controller parameters need to be adapted to get maximum efficiency. A 3-DOF (Three Degrees of Freedom) airframe model is an advanced benchmark model of real 3-DOF helicopter. It has the same uncommon model dynamics with nonlinearities, strong duel motor cross coupling system, uncertain characteristics, disturbances dependent, unmodeled dynamics and many more. The 3-DOF airframe model is a well-known platform for controller performance benchmarking. This research paper shows the development of an approximate prediction model of a Three Degrees of Freedom helicopter model and uses the proposed approximate model to observe the performance of an existent hybrid controller. The hybrid controller is the combination of two different controllers named Quantitative Feedback Theory (QFT) controller and Adaptive controller.To achieve the research objective, the proposed mathematical model of this airframe was used to develop transfer function and simulate with the hybrid controller in MATLAB. The performance of the controller based on the proposed heliframe model of 3-DOF helicopter have also been reported added within this paper.
format Article
author Anwar, Farhat
Islam, Rounakul
Mansor, Hasmah
Hussain, Sabahat
Sharmin, Afsah
author_facet Anwar, Farhat
Islam, Rounakul
Mansor, Hasmah
Hussain, Sabahat
Sharmin, Afsah
author_sort Anwar, Farhat
title Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
title_short Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
title_full Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
title_fullStr Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
title_full_unstemmed Development of approximate prediction model for 3-DOF helicopter and benchmarking with existing controllers
title_sort development of approximate prediction model for 3-dof helicopter and benchmarking with existing controllers
publisher Institute of Advanced Engineering and Science
publishDate 2017
url http://irep.iium.edu.my/60105/1/10032-12450-1-PB%20%28IJEECS-NOV-2017%29.pdf
http://irep.iium.edu.my/60105/7/Development%20of%20approximate%20prediction%20model%20for%203-DOF%20helicopter%20and%20benchmarking%20with%20existing%20controllers.pdf
http://irep.iium.edu.my/60105/
http://www.iaesjournal.com/online/index.php/IJEECS/article/view/17168
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