Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)

In this project the first IIUM-Micro Aerial Vehicle (IIUM-MAV) model was successfully designed, built and tested by team from the Department of Mechanical Engineering, IIUM. Problems related to stability, weight management, component selection, and thrust to weight ratio were faced during the ea...

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Autori principali: Omar, Ashraf Ali, Cheong, Zi Jian
Natura: Proceeding Paper
Lingua:English
Pubblicazione: 2009
Soggetti:
Accesso online:http://irep.iium.edu.my/6528/1/
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author Omar, Ashraf Ali
Cheong, Zi Jian
author_facet Omar, Ashraf Ali
Cheong, Zi Jian
author_sort Omar, Ashraf Ali
collection IIUM
description In this project the first IIUM-Micro Aerial Vehicle (IIUM-MAV) model was successfully designed, built and tested by team from the Department of Mechanical Engineering, IIUM. Problems related to stability, weight management, component selection, and thrust to weight ratio were faced during the early development of models, namely MAV1 to MAV5. Those problems were solved with the flying wing configuration incorporated into the latest models, i.e. MAV6 and MAV7. The span dimensions for the IIUM-MAV6 and -MAV7 were, 1 m and 0.5 m, respectively. The total weight of MAV6 is 197 grams, while MAV7 is 157 grams. The foam was the main material used to construct the IIUM-MAV. The electric micro R/C engine with maximum weight of 19 grams and maximum power output of 80 W was used. Both MAV6 and MAV7 were successfully tested and flew. The performance of MAV7 had been proven to be better than MAV6 in term of stability and maneuverability.
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spelling oai:generic.eprints.org:65282011-11-21T18:17:43Z http://irep.iium.edu.my/6528/ Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV) Omar, Ashraf Ali Cheong, Zi Jian TL500 Aeronautics In this project the first IIUM-Micro Aerial Vehicle (IIUM-MAV) model was successfully designed, built and tested by team from the Department of Mechanical Engineering, IIUM. Problems related to stability, weight management, component selection, and thrust to weight ratio were faced during the early development of models, namely MAV1 to MAV5. Those problems were solved with the flying wing configuration incorporated into the latest models, i.e. MAV6 and MAV7. The span dimensions for the IIUM-MAV6 and -MAV7 were, 1 m and 0.5 m, respectively. The total weight of MAV6 is 197 grams, while MAV7 is 157 grams. The foam was the main material used to construct the IIUM-MAV. The electric micro R/C engine with maximum weight of 19 grams and maximum power output of 80 W was used. Both MAV6 and MAV7 were successfully tested and flew. The performance of MAV7 had been proven to be better than MAV6 in term of stability and maneuverability. 2009 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/6528/1/ Omar, Ashraf Ali and Cheong, Zi Jian (2009) Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV). In: 2nd CUTSE International Conference, 24-25 Nov 2009, Miri, Sarawak. http://www.curtin.edu.my/cutse2009/
spellingShingle TL500 Aeronautics
Omar, Ashraf Ali
Cheong, Zi Jian
Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title_full Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title_fullStr Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title_full_unstemmed Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title_short Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
title_sort development of international islamic university malaysia micro aerial vehicle iium mav
topic TL500 Aeronautics
url http://irep.iium.edu.my/6528/1/
work_keys_str_mv AT omarashrafali developmentofinternationalislamicuniversitymalaysiamicroaerialvehicleiiummav
AT cheongzijian developmentofinternationalislamicuniversitymalaysiamicroaerialvehicleiiummav