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Robust MRAC augmentation of fiight control laws for center of gravity adaptation
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
2016 (English)Conference paper (Refereed)
Abstract [en]

When an aircraft is flying and burning fuel the center of gravity (c.g.) of the aircraft shifts slowly. The c.g. can also be shifted abruptly when e.g. a ghter aircraft releases a weapon. The shift in c.g. is difficult to measure or estimate so the flight control systems need to be robustly designed to cope with this variation. However for fighter aircrafts with high manoeuvrability there is room for improvements. In this paper we investigate if the use of adaptive control law augmentation can be used to better cope with the change in c.g. We augment a baseline controller with a robust Model Reference Adaptive Control (MRAC) design and analyse its benets and possible issues.

Place, publisher, year, edition, pages
2016.
Keyword [en]
Adaptive Control, Flight Control
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-134242OAI: oai:DiVA.org:liu-134242DiVA: diva2:1069587
Conference
Aerospace Technology Congress, Stockholm, Oktober 11-12, 2016
Funder
VINNOVA, 2013-01226
Available from: 2017-01-30 Created: 2017-01-30 Last updated: 2017-01-30

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CiteExportLink to record
Permanent link

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Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • 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