Table of Contents Author Guidelines Submit a Manuscript
The Scientific World Journal
Volume 2014 (2014), Article ID 609027, 12 pages
Research Article

A Comprehensive Robust Adaptive Controller for Gust Load Alleviation

Politecnico di Torino, Dipartimento di Ingegneria Meccanica ed Aerospaziale, Corso Duca degli Abruzzi 24, 10129 Turin, Italy

Received 27 August 2013; Accepted 4 December 2013; Published 4 February 2014

Academic Editors: K.-M. Chung, J. Y. Fu, and A. F. B. A. Prado

Copyright © 2014 Elisa Capello et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


The objective of this paper is the implementation and validation of an adaptive controller for aircraft gust load alleviation. The contribution of this paper is the design of a robust controller that guarantees the reduction of the gust loads, even when the nominal conditions change. Some preliminary results are presented, considering the symmetric aileron deflection as control device. The proposed approach is validated on subsonic transport aircraft for different mass and flight conditions. Moreover, if the controller parameters are tuned for a specific gust model, even if the gust frequency changes, no parameter retuning is required.