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

Direct link
Cite
Citation style
  • apa
  • harvard1
  • 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
Aircraft System Simulation for Preliminary Design
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.ORCID iD: 0000-0002-2315-0680
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.
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.ORCID iD: 0000-0002-6371-1390
2012 (English)In: ICAS 2012 CD-ROM PROCEEDINGS / [ed] Professor I Grant, Optimage Ltd , 2012, Art.nr. ICAS2012-1.9.3- p.Conference paper, Published paper (Other academic)
Abstract [en]

Developments in computational hardware and simulation software have come to a point where it is possible to use whole mission simulation in a framework for conceptual/preliminary design. This paper is about the implementation of full system simulation software for conceptual/preliminary aircraft design. It is based on the new Hopsan NG simulation package, developed at the Linköping University. The Hopsan NG software is implemented in C++. Hopsan NG is the first simulation software that has support for multi-core simulation for high speed simulation of multi domain systems.

In this paper this is demonstrated on a flight simulation model with subsystems, such as control surface actuators.

Place, publisher, year, edition, pages
Optimage Ltd , 2012. Art.nr. ICAS2012-1.9.3- p.
Keyword [en]
aircraft conceptual design, sy stem modeling, mission simulation
National Category
Software Engineering
Identifiers
URN: urn:nbn:se:liu:diva-121484ISBN: 978-0-9565333-1-9 (print)OAI: oai:DiVA.org:liu-121484DiVA: diva2:855676
Conference
28th International Congress of the Aeronautical Sciences, Brisbane, Australia, 23 - 28 September, 2012
Funder
VINNOVA
Available from: 2015-09-22 Created: 2015-09-22 Last updated: 2015-10-05Bibliographically approved

Open Access in DiVA

fulltext(597 kB)301 downloads
File information
File name FULLTEXT01.pdfFile size 597 kBChecksum SHA-512
a6ed155650ecc34bdd364f3fab1af05e2456cc52c1422fc8f86c79c9e2e20643dbff3b18beb5664adaf294ef1ab7708de122b929ddf7578fb0ce868211fd213e
Type fulltextMimetype application/pdf

Other links

Link to publication

Authority records BETA

Krus, PetterBraun, RobertNordin, PeterEriksson, Björn

Search in DiVA

By author/editor
Krus, PetterBraun, RobertNordin, PeterEriksson, Björn
By organisation
Fluid and Mechatronic SystemsThe Institute of Technology
Software Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 301 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: 240 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • 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