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Aircraft Pitch Attitude Control using Backstepping
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
2000 (English)Report (Other academic)
Abstract [en]

A nonlinear approach to the automatic pitch attitude control problem for a generic fighter aircraft is presented. A nonlinear model describing the longitudinal equations of motion in strict feedback form is derived. Backstepping is utilized for the construction of a globally stabilizing controller with a number of free design parameters. Two tuning schemes are proposed based on the desired locally linear controller properties. The controller is evaluated using the HIRM fighter aircraft model.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2000. , 13 p.
Series
LiTH-ISY-R, ISSN 1400-3902 ; 2243
Keyword [en]
Nonlinear control, Aircraft control, Backstepping, Local approximation
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-55671ISRN: LiTH-ISY-R-2243OAI: oai:DiVA.org:liu-55671DiVA: diva2:316399
Available from: 2010-04-30 Created: 2010-04-30 Last updated: 2014-08-21Bibliographically approved

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Härkegård, OlaGlad, Torkel

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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