TY  - JOUR
SP  - 1159
N2  - In this paper, an accurate model of an airbrake electro-hydraulic smart actuator is obtained by physical considerations, and then different control strategies (variable-gain proportional control, PT1 control with switching integrator, and second order sub-optimal sliding mode control) are proposed and analyzed. This application is innovative in the avionic field, and is one of the first attempts to realize a fly-by-wire system for airbrakes, oriented to its immediate employment and installation on current aircraft. The project was carried on with the participation of the Italian Ministry of Defense, and was commissioned to MAG, a leading provider of integrated systems and aviation services for aerospace.
Y1  - 2012/09//
PB  - Wiley-Blackwell
VL  - 14
IS  - 5
AV  - none
TI  - Modeling and control of an airbrake electro-hydraulic smart actuator
UR  - http://dx.doi.org/10.1002/asjc.411
ID  - eprints1203
N1  - The intellectual property of the described research project belongs to MAG - Mecaer Aviation Group.
EP  - 1170
JF  - Asian Journal of Control 
SN  - 1561-8625
A1  - Rubagotti, Matteo
A1  - Carminati, Marco 
A1  - Clemente, Giampiero
A1  - Grassetti, Riccardo
A1  - Ferrara, Antonella
KW  - Sliding-mode control; electro-hydraulic actuators; aircraft control
ER  -