Title :
Modeling and simulation of electromechanical actuators for aircraft nacelles
Author :
Bennouna, Ouadie ; Langlois, Nicolas
Author_Institution :
IRSEEM, ESIGELEC, St. Etienne du Rouvray, France
Abstract :
Future flight control system architectures will be based on “More Electric” or even “All Electric” concepts promising benefits mainly in terms of efficiency, weight and maintenance. This paper concerns the modeling and simulation of aircraft nacelle and especially the electromechanical actuator of the thrust reverser. This modeling is quite complex because it involves several disciplines; it was achieved using the software LMS AMESIM, while the control part has been configured on MATLAB / SIMULINK.
Keywords :
aircraft control; control engineering computing; electromechanical actuators; LMS AMESIM software; Matlab; Simulink; aircraft nacelle; all electric concept; electromechanical actuator; flight control efficiency; flight control maintenance; flight control system; flight control weight; more electric concept; thrust reverser; Actuators; Aerospace control; Aerospace electronics; Aircraft; Atmospheric modeling; Electron tubes; Mathematical model;
Conference_Titel :
Mechatronics and its Applications (ISMA), 2013 9th International Symposium on
Conference_Location :
Amman
Print_ISBN :
978-1-4673-5014-3
DOI :
10.1109/ISMA.2013.6547389
