Abstract
A Design Space Model has been developed to find a design requirements by analyzing design sensitivity and by searching for the feasible design region. In addtion, the best configuration concept that satisfies the design requirements has been identified using Quality Function Deployment and the Configuration Concept Selection Matrix. These Concept Selection Process can contribute to reduce the time and effort during early design stage.
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© 2006 Springer-Verlag Berlin Heidelberg
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Park, HU., Park, MY., Lee, SJ., Lee, JW., Byun, YH. (2006). Development of Requirement Driven Design Concept Selection Process in Aerospace System. In: Gavrilova, M.L., et al. Computational Science and Its Applications - ICCSA 2006. ICCSA 2006. Lecture Notes in Computer Science, vol 3984. Springer, Berlin, Heidelberg. https://doi.org/10.1007/11751649_56
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DOI: https://doi.org/10.1007/11751649_56
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-34079-9
Online ISBN: 978-3-540-34080-5
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