Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718630 | Aerospace Science and Technology | 2010 | 13 Pages |
Abstract
As an original alternative to dynamic inversion techniques, a non-standard anti-windup control strategy is developed in this paper in order to improve the on-ground control system of a civilian aircraft. Using a linear fractional representation (LFR) of the aircraft in combination with an original approximation of the nonlinear ground forces by saturation-type nonlinearities, the proposed design method delivers low-order and robust controllers, which are automatically adapted to the runway state and to the aircraft longitudinal velocity. The efficiency of the design scheme is assessed by several nonlinear simulations.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Clément Roos, Jean-Marc Biannic, Sophie Tarbouriech, Christophe Prieur, Matthieu Jeanneau,