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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)In: Proceedings of Reglermöte 2000, 2000, 143-148 p.Conference paper, Published paper (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
2000. 143-148 p.
Keyword [en]
Nonlinear control, Backstepping, Aircraft control, Local approximation
National Category
Engineering and Technology Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-91131OAI: oai:DiVA.org:liu-91131DiVA: diva2:618401
Conference
Reglermöte 2000, Uppsala, Sweden, June, 2000
Available from: 2013-04-27 Created: 2013-04-17 Last updated: 2013-04-27

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Glad, TorkelHärkegård, Ola

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CiteExportLink to record
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  • apa
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  • ieee
  • modern-language-association-8th-edition
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Language
  • de-DE
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Output format
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  • text
  • asciidoc
  • rtf