• DocumentCode
    1887235
  • Title

    Towards a continuous build-up process of a reusable requirements-based system model

  • Author

    Glas, Martin ; Sartorius, Sky

  • Author_Institution
    Bauhaus Luftfahrt, Munich, Germany
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    The conceptual development process is the joint effort of designers and future operators to elicit and analyze requirements and to design a system which plausibly meets these requirements. A continuous build-up of a structured product model that explicitly interrelates system design and its metrics to requirements is desirable. However, requirements and system modeling are usually conducted separately using different tools. Moreover, the phases of the development process are often separated in time, personnel, and space. This practice leaves a considerable number of system design decisions untraceable. We address these problems by two propositions: (1) A use case which describes an iterative, concurrent, and continuous refinement process of the requirements and system model, and (2) a framework that allows the creation of an integrated system and requirements model and the gradual application of increasingly rigorous rules on the model. We demonstrate our approach by a simple conceptual aircraft design example and discuss whether our approach is scalable and promotes the reuse of model parts.
  • Keywords
    aerospace computing; aircraft; iterative methods; conceptual aircraft design; conceptual development process; concurrent process; continuous build-up process; continuous refinement process; iterative process; reusable requirements-based system model; structured product model; system design decision; system modeling; Aircraft; Analytical models; Annealing; Atmospheric modeling; Prototypes; Unified modeling language;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187338
  • Filename
    6187338