IIUM Geobat flying saucer: design, fabrication and testing

In this work, the first IIUM circular planform unmanned Aerial vehicle (IIUM-CPUAV), also known as Geobat flying saucer, was successfully designed, built and tested by the team from the Department of Mechanical Engineering, IIUM. The designing process started with gathering historical data and perfo...

Full description

Bibliographic Details
Main Author: Omar, Ashraf Ali E.
Format: Monograph
Language:English
Published: s.n. 2012
Subjects:
Online Access:http://irep.iium.edu.my/33516/1/EDW_A11-056.pdf
_version_ 1796878404426924032
author Omar, Ashraf Ali E.
author_facet Omar, Ashraf Ali E.
author_sort Omar, Ashraf Ali E.
collection IIUM
description In this work, the first IIUM circular planform unmanned Aerial vehicle (IIUM-CPUAV), also known as Geobat flying saucer, was successfully designed, built and tested by the team from the Department of Mechanical Engineering, IIUM. The designing process started with gathering historical data and performing the conceptual design calculations. The maximum diameter and weight of IIUM-CPUAV are 1 m and 900 grams, respectively and foam was the main material used for fabrication. Flight tests were successfully conducted and IIUM-CPUAV was found to be stable. Based on the flight tests results, design modifications were carried out on the prototype to improve the stability and the performance. The final configuration of the IIUM-CPUAV was successfully tested.
first_indexed 2024-03-05T23:20:59Z
format Monograph
id oai:generic.eprints.org:33516
institution International Islamic University Malaysia
language English
last_indexed 2024-03-05T23:20:59Z
publishDate 2012
publisher s.n.
record_format dspace
spelling oai:generic.eprints.org:335162014-02-02T10:07:11Z http://irep.iium.edu.my/33516/ IIUM Geobat flying saucer: design, fabrication and testing Omar, Ashraf Ali E. TL500 Aeronautics In this work, the first IIUM circular planform unmanned Aerial vehicle (IIUM-CPUAV), also known as Geobat flying saucer, was successfully designed, built and tested by the team from the Department of Mechanical Engineering, IIUM. The designing process started with gathering historical data and performing the conceptual design calculations. The maximum diameter and weight of IIUM-CPUAV are 1 m and 900 grams, respectively and foam was the main material used for fabrication. Flight tests were successfully conducted and IIUM-CPUAV was found to be stable. Based on the flight tests results, design modifications were carried out on the prototype to improve the stability and the performance. The final configuration of the IIUM-CPUAV was successfully tested. s.n. 2012-05 Monograph NonPeerReviewed application/pdf en http://irep.iium.edu.my/33516/1/EDW_A11-056.pdf Omar, Ashraf Ali E. (2012) IIUM Geobat flying saucer: design, fabrication and testing. Research Report. s.n., Kuala Lumpur. (Unpublished) EDW A11-056-0847
spellingShingle TL500 Aeronautics
Omar, Ashraf Ali E.
IIUM Geobat flying saucer: design, fabrication and testing
title IIUM Geobat flying saucer: design, fabrication and testing
title_full IIUM Geobat flying saucer: design, fabrication and testing
title_fullStr IIUM Geobat flying saucer: design, fabrication and testing
title_full_unstemmed IIUM Geobat flying saucer: design, fabrication and testing
title_short IIUM Geobat flying saucer: design, fabrication and testing
title_sort iium geobat flying saucer design fabrication and testing
topic TL500 Aeronautics
url http://irep.iium.edu.my/33516/1/EDW_A11-056.pdf
work_keys_str_mv AT omarashrafalie iiumgeobatflyingsaucerdesignfabricationandtesting