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A Backstepping Design for Flight Path Angle Control
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 the 39th IEEE Conference on Decision and Control, 2000, 3570-3575 p.Conference paper, Published paper (Refereed)
Abstract [en]

A nonlinear approach to flight path angle control is presented. Using backstepping, a globally stabilizing control law is derived. Although the nonlinear nature of the lift force is considered, the pitching moment to be produced is only linear in the measured states. Thus, the resulting control law is much simpler than if feedback linearization had been used. The free parameters that spring from the backstepping design are used to achieve a desired linear behavior around the operating point.

Place, publisher, year, edition, pages
2000. 3570-3575 p.
Series
Conference on Decision and Control, ISSN 0191-2216 ; vol. 4
Keyword [en]
Aircraft control, Backstepping, Flight path angle, HIRM
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-91215DOI: 10.1109/CDC.2000.912259ISBN: 0-7803-6638-7 (print)OAI: oai:DiVA.org:liu-91215DiVA: diva2:616500
Conference
39th IEEE Conference on Decision and Control, Sydney, Australia, December, 2000
Available from: 2013-04-17 Created: 2013-04-17 Last updated: 2014-12-10

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Härkegård, OlaGlad, Torkel

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  • de-DE
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  • nn-NB
  • sv-SE
  • Other locale
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Output format
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