Modeling and control of an airbrake electro-hydraulic smart actuator

被引：9
|
作者：
Rubagotti, Matteo [1 ]
Carminati, Marco [2 ]
Clemente, Giampiero [3 ]
Grassetti, Riccardo [4 ]
Ferrara, Antonella [5 ]
机构：
[1] Univ Trento, Dept Mech & Struct Engn, I-38123 Trento, Italy
[2] Politecn Milan, Dept Elect & Informat, I-20133 Milan, Italy
[3] MAG, I-28021 Borgomanero, NO, Italy
[4] Log Spa, I-20060 Cassina De Pecchi, MI, Italy
[5] Univ Pavia, Dept Comp Engn & Syst Sci, I-27100 Pavia, Italy
来源：
ASIAN JOURNAL OF CONTROL | 2012年 / 14卷 / 05期
关键词：
Sliding-mode control; electro-hydraulic actuators; aircraft control;
D O I：
10.1002/asjc.411
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
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. Copyright (c) 2011 John Wiley and Sons Asia Pte Ltd and Chinese Automatic Control Society
引用
收藏
页码：1159 / 1170
页数：12
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