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Flight Control Design 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.
2001 (English)In: Proceedings of the 5th IFAC Symposium Nonlinear Control Systems, 2001, 259-264 p.Conference paper, Published paper (Refereed)
Abstract [en]

Today's prevailing nonlinear design method for aircraft flight control is feedback linearization. This paper presents a new method to deal with the nonlinear aerodynamic forces and moments acting on the aircraft: backstepping. Specically, we derive backstepping control laws for angle of attack and sideslip control that require less knowledge of the lift and side forces compared to feedback linearization designs. The control laws are made adaptive to errors in the aerodynamic moment coefficients using nonlinear observer techniques.

Place, publisher, year, edition, pages
2001. 259-264 p.
Keyword [en]
Aircraft control, Backstepping, Lyapunov functions, Inverse optimality
National Category
Engineering and Technology Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-90808OAI: oai:DiVA.org:liu-90808DiVA: diva2:616392
Conference
5th IFAC Symposium on Nonlinear Control Systems, St. Petersburg, Russia, July, 2001
Available from: 2013-04-16 Created: 2013-04-07 Last updated: 2013-04-16

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Glad, TorkelHärkegård, Ola

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