Skip to main content

Development of Requirement Driven Design Concept Selection Process in Aerospace System

  • Conference paper
Computational Science and Its Applications - ICCSA 2006 (ICCSA 2006)

Part of the book series: Lecture Notes in Computer Science ((LNTCS,volume 3984))

Included in the following conference series:

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.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 169.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Park, H.-U., Kim, M.-J., Lee, J.-W., Byun, Y.-H.: Unmanned Helicopter Conceptual Design by Considering Uncertainty of Requirement. In: Proceedings of the 2005 KSAS Spring Conference (2005)

    Google Scholar 

  2. Aerospace vehicle design project, Def. of Aerospace Eng., Konkuk Univ. (2005)

    Google Scholar 

  3. Optimus v5.0, Noesis Solutions Inc. User Manual (2004)

    Google Scholar 

  4. JMP v5.0, SAS Institute Inc. User Manual (2002)

    Google Scholar 

  5. Baker, A.P.: The Rule Of Mission Requirements, Vehicle Attributes, Technologies And Uncertaint In Rotorcraft System Design (2002)

    Google Scholar 

  6. QFD Designer 4, Ideacore (2000)

    Google Scholar 

  7. Kim, M.-J., Park, M.-Y., Lee, J.-W., Byun, Y.-H.: System Requirement Analysis of Multi-Role Helicopter by Implementing Quality Function Deployment. Korean Council On Systems Engineering Review 1(2), 56–62 (2005)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2006 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

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

Download citation

  • 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

  • eBook Packages: Computer ScienceComputer Science (R0)

Publish with us

Policies and ethics