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Knowledge-Based Flight Control System Integration in RAPID
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.ORCID iD: 0000-0002-1301-7931
2015 (English)Report (Other academic)
Abstract [en]

Nowadays, aircraft’s design and development processes are not only time-consuming but also incur high economic cost. In addition, system integration is highly a multi-disciplinary design process, which involves a large number of different discipline teams working at the same time and space. The main objective of this work is to investigate in the early design stages to define and integrate flight control system. The purpose is to improve the functionality of an in house produced aircraft conceptual design tool RAPID carried out at the Division of Fluid and Mechatronic Systems, Linköping University.

Place, publisher, year, edition, pages
2015. , 5 p.
Keyword [en]
Flight control system, RAPID, Knowledge Pattern, Parametrization, Hydraulic aircraft systems.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-113292OAI: oai:DiVA.org:liu-113292DiVA: diva2:780786
Available from: 2015-01-15 Created: 2015-01-15 Last updated: 2015-06-02Bibliographically approved

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Knowledge-Based Flight Control System Integration in RAPID(488 kB)185 downloads
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File name FULLTEXT01.pdfFile size 488 kBChecksum SHA-512
314fc749b5144d8d480a8ad6c0623322f99435e9aa2a0bdab2db89c900245e47336f583ec116c69afe129e295722bdf21b21d3c3df80bf119cb108127d49aa55
Type fulltextMimetype application/pdf

Authority records BETA

Chaitanya Munjulury, Raghu

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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