DocumentCode :
993541
Title :
A Full Envelope Small Commercial Aircraft Flight Control Design Using Multivariable Proportional-Integral Control
Author :
Mattei, Massimiliano ; Scordamaglia, Valerio
Author_Institution :
Univ. degli Studi Mediterranea di Reggio Calabria, Reggio Calabria
Volume :
16
Issue :
1
fYear :
2008
Firstpage :
169
Lastpage :
176
Abstract :
This brief deals with the application of linear parameter varying control concepts to the design of a full envelope flight control system for commercial aircrafts. The proposed controller is fixed to have a multivariable proportional-integral structure. A linear matrix inequalities-based technique is proposed to account for variations both in the reference model and in the plant. Some numerical simulations show the effectiveness of the proposed technique all over the aircraft operating envelope.
Keywords :
PI control; aircraft control; control system synthesis; linear matrix inequalities; multivariable control systems; aircraft operating envelope; commercial aircraft flight control design; full envelope flight control; linear matrix inequalities; linear parameter varying control; multivariable proportional-integral control; numerical simulation; reference model; Aerospace control; Aircraft; Control system synthesis; Control systems; Linear matrix inequalities; Nonlinear systems; Pi control; Proportional control; Three-term control; Uncertainty;
fLanguage :
English
Journal_Title :
Control Systems Technology, IEEE Transactions on
Publisher :
ieee
ISSN :
1063-6536
Type :
jour
DOI :
10.1109/TCST.2007.903098
Filename :
4392490
Link To Document :
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