The research on aircraft RDT&E cost based on gray correlation analysis theory and equalation-Engineering-value-rate

Xie Jianxi, Song Bifeng, Liu Dongxia

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Recently, technology advance in aerospace industry and the introduction of factors as life cycle cost (LCC) make a change of design ideas and design emphases for aircraft. Aircraft design is making a shift from traditional "optimum design for performance" to "design for affordability and quality". Aircraft design is shifting and extending the tradeoffs between traditional disciplines as aerodynamics, propulsion, structure etc to the tradeoffs between these traditional disciplines and nonconventional disciplines including subjects like reliability, maintainability, safety and survivability, as well as crossover disciplines as economics and stability. Economics is becoming a key factor that decision makers judge optimal scheme from some feasible design concepts of aircraft. As the economics metrics, life cycle cost of aircraft is an important design index for modern aircraft system and is one of the key metrics of evaluating the goodness of design scheme for aerospace product. Furthermore, the analysis of life cycle cost is the basis of costeffectiveness analysis on aircraft. The research, development, test, and evaluation (RDT&E) cost are an important part that makes up the total life cycle cost (LCC) of an aircraft. A method based on gray correlation analysis theory and equalation-engineeringvalue-rate method for estimating RDT&E cost of aircraft especially in early conceptual design stage is presented. The first task of establishing cost model in the parametric method of life cycle cost is to determine the cost drive factor. Based on large amount of historical data at home and abroad, using the method of gray correlation analysis in gray system theory, the article establishes the determination method of cost drive factor, which overcomes the shortcoming of the lack of data. Combining the features of less known knowledge in early conceptual design stage for aircraft design, the authors propose the definition of equalationengineering-value-rate and study the RDT&E cost for aircraft by applying the method of equalation-Engineering-value-rate to modify the existed cost model on the basis of the determined cost drive factor and historical data. The method proposed provides a new theory for the establishment of LCC model for aircraft toplevel design. Furthermore, the method provides the decision gist for the decision tradeoffs of early stage in aircraft design, and establishes the basis for cost/effectiveness analysis in aircraft design.

Original languageEnglish
Title of host publicationICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
PublisherInternational Council of The Aeronautical Sciences (ICAS)
Pages3820-3829
Number of pages10
ISBN (Print)9781604232271
StatePublished - 2006
Event25th Congress of the International Council of the Aeronautical Sciences 2006 - Hamburg, Germany
Duration: 3 Sep 20068 Sep 2006

Publication series

NameICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
Volume6

Conference

Conference25th Congress of the International Council of the Aeronautical Sciences 2006
Country/TerritoryGermany
CityHamburg
Period3/09/068/09/06

Keywords

  • Aircraft top-level design
  • Cost drive factor
  • Equalation-engineering-value-rate
  • Gray correlation analysis theory
  • Life cycle cost

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