Robust backstepping controller for aircraft dynamics

Research output: Contribution to conferencePaper

4 Citations (Scopus)

Abstract

The nonlinear flight dynamics of a rigid body aircraft is stabilized using a modified output feedback linearization control. The perturbations and model uncertainties effects are canceled out by the injection of a compensation term computed by the application of High-Order Sliding Mode Observers-Identifiers. The feedback linearizing controller is designed considering a nominal model of the aircraft dynamic. The resulting controller exhibits a high robustness guaranteeing the stability and maneuverability of the aircraft in the presence of system uncertainties and external perturbations. © 2011 IFAC.
Original languageAmerican English
Pages13840-13845
Number of pages12455
DOIs
StatePublished - 1 Jan 2011
EventIFAC Proceedings Volumes (IFAC-PapersOnline) -
Duration: 1 Dec 2011 → …

Conference

ConferenceIFAC Proceedings Volumes (IFAC-PapersOnline)
Period1/12/11 → …

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Aircraft
Uncertainty
Nonlinear Dynamics
Injections

Cite this

Davila, J. (2011). Robust backstepping controller for aircraft dynamics. 13840-13845. Paper presented at IFAC Proceedings Volumes (IFAC-PapersOnline), . https://doi.org/10.3182/20110828-6-IT-1002.03413
Davila, Jorge. / Robust backstepping controller for aircraft dynamics. Paper presented at IFAC Proceedings Volumes (IFAC-PapersOnline), .12455 p.
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Davila, J 2011, 'Robust backstepping controller for aircraft dynamics', Paper presented at IFAC Proceedings Volumes (IFAC-PapersOnline), 1/12/11 pp. 13840-13845. https://doi.org/10.3182/20110828-6-IT-1002.03413

Robust backstepping controller for aircraft dynamics. / Davila, Jorge.

2011. 13840-13845 Paper presented at IFAC Proceedings Volumes (IFAC-PapersOnline), .

Research output: Contribution to conferencePaper

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Davila J. Robust backstepping controller for aircraft dynamics. 2011. Paper presented at IFAC Proceedings Volumes (IFAC-PapersOnline), . https://doi.org/10.3182/20110828-6-IT-1002.03413