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: Conference or Workshop Item
Language:English
Published: 2010
Subjects:
Online Access:http://irep.iium.edu.my/2382/
http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf
id iium-2382
recordtype eprints
spelling iium-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 Conference or Workshop Item 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.
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TL500 Aeronautics
spellingShingle TL500 Aeronautics
Omar, Ashraf Ali
Kurban, Adel
Baharuddin, Khairun Nisaa
Ibrahim, Idasary
Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
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.
format Conference or Workshop Item
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
title Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
title_short 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_sort development of iium free wing unmanned aerial vehicle (iium-fwuav)
publishDate 2010
url http://irep.iium.edu.my/2382/
http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf
first_indexed 2023-09-18T20:09:59Z
last_indexed 2023-09-18T20:09:59Z
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