Abstract
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, PT 1 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.
| Original language | English |
|---|---|
| Pages (from-to) | 1159-1170 |
| Number of pages | 12 |
| Journal | Asian Journal of Control |
| Volume | 14 |
| Issue number | 5 |
| DOIs | |
| Publication status | Published - Sep 1 2012 |
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Keywords
- aircraft control
- electro-hydraulic actuators
- Sliding-mode control
ASJC Scopus subject areas
- Control and Systems Engineering
Cite this
Modeling and control of an airbrake electro-hydraulic smart actuator. / Rubagotti, Matteo; Carminati, Marco; Clemente, Giampiero; Grassetti, Riccardo; Ferrara, Antonella.
In: Asian Journal of Control, Vol. 14, No. 5, 01.09.2012, p. 1159-1170.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Modeling and control of an airbrake electro-hydraulic smart actuator
AU - Rubagotti, Matteo
AU - Carminati, Marco
AU - Clemente, Giampiero
AU - Grassetti, Riccardo
AU - Ferrara, Antonella
PY - 2012/9/1
Y1 - 2012/9/1
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, PT 1 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.
AB - 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, PT 1 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.
KW - aircraft control
KW - electro-hydraulic actuators
KW - Sliding-mode control
UR - http://www.scopus.com/inward/record.url?scp=84866722949&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84866722949&partnerID=8YFLogxK
U2 - 10.1002/asjc.411
DO - 10.1002/asjc.411
M3 - Article
VL - 14
SP - 1159
EP - 1170
JO - Asian Journal of Control
JF - Asian Journal of Control
SN - 1561-8625
IS - 5
ER -