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...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Instituto de Aeronautica e Espaco-IAE - Brazil
2012
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| Subjects: | |
| Online Access: | 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 |
| Summary: | 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 |
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