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Modeling and simulating aircraft stability & control - The SimSAC project
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
2010 (English)In: AIAA Atmospheric Flight Mechanics Conference 2010, 2010Conference paper, Published paper (Refereed)
Abstract [en]

This paper overviews the SimSAC Project, Simulating Aircraft Stability And Control Characteristics for Use in Conceptual Design. It reports on the three major tasks: Development of design software, validating the software on benchmark tests and applying the software to design exercises. CEASIOM, the Computerized Environment for Aircraft Synthesis and Integrated Optimization Methods, is a framework tool that integrates discipline-specific tools for conceptual design. At this early stage of the design it is very useful to be able to predict the flying and handling qualities of this design. In order to do this, the aerodynamic database needs to be computed for the configuration being studied which then has to be coupled to the stability and control tools to carry out the analysis. The benchmarks for validation are the F12 windtunnel model of a generic long-range airliner and the TCR windtunnel model of a sonic-cruise passenger transport concept. The design, simulate and evaluate (DSE) exercise demonstrates how the software works as a design tool. The exercise begins with a design specification and uses conventional design methods to prescribe a baseline configuration. Then CEASIOM improves upon this baseline by analyzing its flying and handling qualities. Six such exercises are presented.

Place, publisher, year, edition, pages
2010.
Keyword [en]
Aerodynamic database, Baseline configurations, Computerized environment, Conventional design methods, Design specification, Integrated optimization, Modeling and simulating, Stability and control, Aerodynamic configurations, Aircraft, Benchmarking, Conceptual design, Electric reactors, Tools, Wind tunnels, Flight control systems
National Category
Vehicle Engineering
Identifiers
URN: urn:nbn:se:kth:diva-148916Scopus ID: 2-s2.0-84880828321ISBN: 978-162410151-9 (print)OAI: oai:DiVA.org:kth-148916DiVA: diva2:738135
Conference
AIAA Atmospheric Flight Mechanics Conference 2010, 2 August 2010 through 5 August 2010, Toronto, ON, Canada
Note

QC 20140815

Available from: 2014-08-15 Created: 2014-08-14 Last updated: 2014-08-15Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
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  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
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  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf