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...
| Main Authors: | , , , |
|---|---|
| Format: | Proceeding Paper |
| 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 |
| _version_ | 1848775999723929600 |
|---|---|
| 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 |
| building | IIUM Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-14T14:23:07Z |
| format | Proceeding Paper |
| id | iium-2382 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T14:23:07Z |
| publishDate | 2010 |
| recordtype | eprints |
| repository_type | Digital Repository |
| 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 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/ http://irep.iium.edu.my/2382/1/Full_paper_final__08December2009.pdf |