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Computational Questions of Equilibrium Calculation with Application to Nonlinear Aircraft Dynamics
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.
1997 (English)Report (Other academic)
Abstract [en]

The computation of possible stationary orientations of an aircraft subjected to constraints on actuators is treated using methods from computer algebra. The same techniques are also used to investigate possible turn maneuvers of a missile subjected to actuator constraints. The paper also gives a brief introduction to the utilized algebraic methods, cylindricalalgebraic decomposition and quantifier elimination.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 1997. , 12 p.
Series
LiTH-ISY-R, ISSN 1400-3902 ; 1990
Keyword [sv]
Mekanik Fluidmekanik
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-55407ISRN: LiTH-ISY-R-1990OAI: oai:DiVA.org:liu-55407DiVA: diva2:316198
Funder
Swedish Research Council
Available from: 2010-04-30 Created: 2010-04-30 Last updated: 2014-09-18Bibliographically approved

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Glad, Torkel

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Automatic ControlThe Institute of Technology
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CiteExportLink to record
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Citation style
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  • harvard1
  • ieee
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Language
  • de-DE
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  • nn-NO
  • nn-NB
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