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Longitudinal Aircraft Control using Backstepping
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
1999 (English)In: Proceedings of the Second Conference on Computer Science and Systems Engineering, 1999, 69-73 p.Conference paper, Published paper (Other academic)
Abstract [en]

Aircraft control constitutes a classical control design challenge. The nonlinear dynamical contributions from the aerodynamics are often dealt with by linearization around one or several working points. This paper addresses the task of global stabilization, considering the longitudinal motions of a combat aircraft. A nonlinear, recursive design technique called backstepping is described and utilized for constructing a control law, which is then used for simulation.

Place, publisher, year, edition, pages
1999. 69-73 p.
Keyword [en]
Backstepping, Aircraft control, Linearization
National Category
Engineering and Technology Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-91195OAI: oai:DiVA.org:liu-91195DiVA: diva2:617150
Conference
Second Conference on Computer Science and Systems Engineering, Norrköping, Sweden, October, 1999
Available from: 2013-04-22 Created: 2013-04-17 Last updated: 2013-04-23

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Härkegård, Ola

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CiteExportLink to record
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Output format
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