To read this content please select one of the options below:

Neuro‐fuzzy synthesis of flight control electrohydraulic servo

Ioan Ursu (“Eli Carafoli” National Institute for Aerospace Research, Bucharest, Romania)
Felicia Ursu (“Eli Carafoli” National Institute for Aerospace Research, Bucharest, Romania)
Lucian Iorga (“Eli Carafoli” National Institute for Aerospace Research, Bucharest, Romania)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 2001

538

Abstract

Presents a switching type neuro‐fuzzy control synthesis. The control algorithm supposes as a component part a neurocontrol designed to optimize a performance index. Whenever the neurocontrol saturates or a certain performance parameter of the system decreases, the scheme of control switches to a feasible and reliable fuzzy logic control. Describes the procedure of return to the optimizing neurocontrol which is essential. This methodology of control synthesis ensures antisaturating, antichattering and robustness properties of the controlling system, as illustrated by numerical simulation in the case of a primary flight controls electrohydraulic servo actuator

Keywords

Citation

Ursu, I., Ursu, F. and Iorga, L. (2001), "Neuro‐fuzzy synthesis of flight control electrohydraulic servo", Aircraft Engineering and Aerospace Technology, Vol. 73 No. 5, pp. 465-472. https://doi.org/10.1108/00022660110403014

Publisher

:

MCB UP Ltd

Copyright © 2001, MCB UP Limited

Related articles