liu.seSearch for publications in DiVA
Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • oxford
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Integration of On-Board Power Systems Simulation in Conceptual Aircraft Design
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.
2013 (English)In: Proceedings of the 4th CEAS Conference in Linköping / [ed] Tomas Melin, Petter Krus,Emil Vinterhav, Knut Övrebö, Linköping, Sweden: Linköping University Electronic Press, 2013, p. 709-718Conference paper, Published paper (Other academic)
Abstract [en]

This paper describes the methodology of generating simulation models out of basic information, available during conceptual design phase. The implementation of an aircraft system is shown as an example using the simulation software HOPSAN.

Because of the limited direct project-related data available at the conceptual stage, the traditional method of creating physical simulation models by the bottom up approach with the help of (standard) component libraries is not applicable. Instead, the respective systems’ architecture as well as their composition has to be descriptively predefined in a flexible, wide-range applicable manner, known as the knowledge base (KB) approach. These system technology driven design declarations – combined with project related data – result in roughly pre-tuned system simulation models, which may help when conducting more detailed investigations of the project such as performance analysis.

This (system architecture) knowledge-based approach is shown on the whole aircraft system level down to the detailed implementation of the control surface actuator systems of the primary flight control system.

Place, publisher, year, edition, pages
Linköping, Sweden: Linköping University Electronic Press, 2013. p. 709-718
Keywords [en]
Conceptual aircraft design, system simulation, onboard power systems, knowledge based engineering
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-103197ISBN: 78-91-7519-519-3 (print)OAI: oai:DiVA.org:liu-103197DiVA, id: diva2:687700
Conference
4th European Air & Space Conference (CEAS 2013), 16-19 September 2013, Linköping, Sweden
Funder
Vinnova, NFFP5Available from: 2014-01-15 Created: 2014-01-15 Last updated: 2014-02-12Bibliographically approved

Open Access in DiVA

CEAS_IngoStaack_MetaSimulationmodel(575 kB)668 downloads
File information
File name FULLTEXT01.pdfFile size 575 kBChecksum SHA-512
13e8aec1907a97236601a353dc15cae86ccc7eb27c743b976f4f52e11428a56f6f955816eac0d6397af7e87cae6401e9139d23d56532f79110dc9b7b37e90d94
Type fulltextMimetype application/pdf

Other links

http://www.ceas2013.org

Authority records

Staack, IngoKrus, Petter

Search in DiVA

By author/editor
Staack, IngoKrus, Petter
By organisation
Fluid and Mechatronic SystemsThe Institute of Technology
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 668 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

isbn
urn-nbn

Altmetric score

isbn
urn-nbn
Total: 496 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • oxford
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf