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Analysis of Actuator Cross Coupling in Aircraft
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
1999 (English)Report (Other academic)
Abstract [en]

When several control signals share the same physical actuators, actuator saturation has the effect of giving coupling between control loops which are otherwise decoupled. This effect occurs e.g. in aircraft control where the elevator and aileron functions often use the same physical control surfaces. The effect is particularly important when one of the loops is open loop unstable. The paper consider the effects on the stabilizable region of cross coupling with another control loop. To give further insight simple optimal control problems are considered.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 1999. , 8 p.
Series
LiTH-ISY-R, ISSN 1400-3902 ; 2137
Keyword [en]
Actuator saturation, Input saturation, Nonlinear control, Aircraft control
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-55709ISRN: LiTH-ISY-R-2137OAI: oai:DiVA.org:liu-55709DiVA: diva2:316486
Available from: 2010-04-30 Created: 2010-04-30 Last updated: 2014-09-08Bibliographically approved

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Analysis of Actuator Cross Coupling in Aircraft(169 kB)93 downloads
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Glad, Torkel

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Automatic ControlThe Institute of Technology
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CiteExportLink to record
Permanent link

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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