Design optimization of Micro Air Launch Vehicle using differential evolution
In this paper, we have used the differential evolution to optimize the design of a Micro Air Launch Vehicle and its launch trajectory. Since trajectory design of a launch vehicle requires prior knowledge of the masses and propulsion performance parameters of the Micro Air Launch Vehicle, whereas t...
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Instituto de Aeronautica e Espaco-IAE - Brazil
2012
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iium-438352015-07-21T06:12:39Z http://irep.iium.edu.my/43835/ Design optimization of Micro Air Launch Vehicle using differential evolution Aldheeb, Mohammed Kafafy, Raed Idres, Moumen Omar, Hanafy Abido, Mohammad TJ Mechanical engineering and machinery In this paper, we have used the differential evolution to optimize the design of a Micro Air Launch Vehicle and its launch trajectory. Since trajectory design of a launch vehicle requires prior knowledge of the masses and propulsion performance parameters of the Micro Air Launch Vehicle, whereas the vehicle design requires prior knowledge of the required velocity Instituto de Aeronautica e Espaco-IAE - Brazil 2012-04 Article PeerReviewed application/pdf en http://irep.iium.edu.my/43835/1/2012-Design_Optimization_of_Micro_Air_Launch_Vehicle_Using_Differential_Evolution_PublishedPaper.pdf Aldheeb, Mohammed and Kafafy, Raed and Idres, Moumen and Omar, Hanafy and Abido, Mohammad (2012) Design optimization of Micro Air Launch Vehicle using differential evolution. Journal of Aerospace Technology and Management, 4 (2). pp. 185-196. ISSN 1984-9648, 2175-9146 http://www.jatm.com.br/ 10.5028/jatm.2012.04020112 |
repository_type |
Digital Repository |
institution_category |
Local University |
institution |
International Islamic University Malaysia |
building |
IIUM Repository |
collection |
Online Access |
language |
English |
topic |
TJ Mechanical engineering and machinery |
spellingShingle |
TJ Mechanical engineering and machinery Aldheeb, Mohammed Kafafy, Raed Idres, Moumen Omar, Hanafy Abido, Mohammad Design optimization of Micro Air Launch Vehicle using differential evolution |
description |
In this paper, we have used the differential evolution to optimize the design of a Micro Air Launch Vehicle and
its launch trajectory. Since trajectory design of a launch vehicle requires prior knowledge of the masses and propulsion
performance parameters of the Micro Air Launch Vehicle, whereas the vehicle design requires prior knowledge of the
required velocity |
format |
Article |
author |
Aldheeb, Mohammed Kafafy, Raed Idres, Moumen Omar, Hanafy Abido, Mohammad |
author_facet |
Aldheeb, Mohammed Kafafy, Raed Idres, Moumen Omar, Hanafy Abido, Mohammad |
author_sort |
Aldheeb, Mohammed |
title |
Design optimization of Micro Air Launch Vehicle using differential evolution |
title_short |
Design optimization of Micro Air Launch Vehicle using differential evolution |
title_full |
Design optimization of Micro Air Launch Vehicle using differential evolution |
title_fullStr |
Design optimization of Micro Air Launch Vehicle using differential evolution |
title_full_unstemmed |
Design optimization of Micro Air Launch Vehicle using differential evolution |
title_sort |
design optimization of micro air launch vehicle using differential evolution |
publisher |
Instituto de Aeronautica e Espaco-IAE - Brazil |
publishDate |
2012 |
url |
http://irep.iium.edu.my/43835/ http://irep.iium.edu.my/43835/ http://irep.iium.edu.my/43835/ http://irep.iium.edu.my/43835/1/2012-Design_Optimization_of_Micro_Air_Launch_Vehicle_Using_Differential_Evolution_PublishedPaper.pdf |
first_indexed |
2023-09-18T21:02:24Z |
last_indexed |
2023-09-18T21:02:24Z |
_version_ |
1777410711242145792 |