A method able to analyze and optimize subsystems could be useful to reduce project cost, increase subsystem reliability, improve overall aircraft safety and reduce subsystem weight. The earlier the optimization of development of an aircraft in the design phase can be performed, the better the yield of the optimization becomes. This master thesis was formed in order to construct an automatic analysis method, implementing a Matlab script, evaluating devices forming aircraft subsystems using a Genetic Algorithm. In addition to aircraft subsystems, the method constructed in the work is compatible with systems of various industries with minor modifications of the script.
Identifer | oai:union.ndltd.org:UPSALLA1/oai:DiVA.org:liu-119950 |
Date | January 2015 |
Creators | Bergström, Joakim, Nilsson-Sundén, Hampus |
Publisher | Linköpings universitet, Fysik och elektroteknik, Linköpings universitet, Tekniska högskolan, Linköpings universitet, Fysik och elektroteknik, Linköpings universitet, Tekniska högskolan |
Source Sets | DiVA Archive at Upsalla University |
Language | English |
Detected Language | English |
Type | Student thesis, info:eu-repo/semantics/bachelorThesis, text |
Format | application/pdf |
Rights | info:eu-repo/semantics/openAccess |
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