Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)

This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. Its main advantage is stall avoidance which is achieved through the natural property of the airfo...

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Main Authors: Omar, Ashraf Ali, Kurban, Adel, Baharuddin, Khairun Nisaa, Ibrahim, Idasary
Format: Proceeding Paper
Language:English
Published: 2010
Subjects:
Online Access:http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf
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author Omar, Ashraf Ali
Kurban, Adel
Baharuddin, Khairun Nisaa
Ibrahim, Idasary
author_facet Omar, Ashraf Ali
Kurban, Adel
Baharuddin, Khairun Nisaa
Ibrahim, Idasary
author_sort Omar, Ashraf Ali
collection IIUM
description This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. Its main advantage is stall avoidance which is achieved through the natural property of the airfoil. In constructing the aerial vehicle, the initial weight is estimated and the wing size, fuselage size and aerodynamic forces prediction are determined. Optimization of the aircraft is done through trial and error method. The developed free wing unmanned aerial vehicle (FW-UAV) flew successively. In this study, the free wing has been proven to be a very efficient unmanned aerial vehicle.
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spelling oai:generic.eprints.org:23822011-11-14T00:48:37Z http://irep.iium.edu.my/2382/ Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV) Omar, Ashraf Ali Kurban, Adel Baharuddin, Khairun Nisaa Ibrahim, Idasary TL500 Aeronautics This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. Its main advantage is stall avoidance which is achieved through the natural property of the airfoil. In constructing the aerial vehicle, the initial weight is estimated and the wing size, fuselage size and aerodynamic forces prediction are determined. Optimization of the aircraft is done through trial and error method. The developed free wing unmanned aerial vehicle (FW-UAV) flew successively. In this study, the free wing has been proven to be a very efficient unmanned aerial vehicle. 2010-02-18 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf Omar, Ashraf Ali and Kurban, Adel and Baharuddin, Khairun Nisaa and Ibrahim, Idasary (2010) Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV). In: The 2nd International Conference on Engineering and ICT , 18-20 Feb. 2010, Melaka, Malaysia.
spellingShingle TL500 Aeronautics
Omar, Ashraf Ali
Kurban, Adel
Baharuddin, Khairun Nisaa
Ibrahim, Idasary
Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_full Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_fullStr Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_full_unstemmed Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_short Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_sort development of iium free wing unmanned aerial vehicle iium fwuav
topic TL500 Aeronautics
url http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf
work_keys_str_mv AT omarashrafali developmentofiiumfreewingunmannedaerialvehicleiiumfwuav
AT kurbanadel developmentofiiumfreewingunmannedaerialvehicleiiumfwuav
AT baharuddinkhairunnisaa developmentofiiumfreewingunmannedaerialvehicleiiumfwuav
AT ibrahimidasary developmentofiiumfreewingunmannedaerialvehicleiiumfwuav