DocumentCode :
1893119
Title :
Nonlinear Integral Minimum Variance-Like Control with Application to an Aircraft System
Author :
Dimogianopoulos, Dimitrios G. ; Hios, John D. ; Fassois, Spilios D.
Author_Institution :
Dept. of Mech. & Aeronaut. Eng., Patras Univ.
fYear :
2006
fDate :
28-30 June 2006
Firstpage :
1
Lastpage :
6
Abstract :
This paper presents an integral minimum variance-like controller design based upon a specific pooled non-linear autoregressive moving average with exogenous excitation (NARMAX) representation. The controller design introduces suitable modifications to account for the characteristics of the pooled NARMAX representation. The control strategy is subsequently applied to a nonlinear aircraft system in order to obtain regulation of the pitch rate around a predetermined value (zero for the given case). Comparisons with a conventional PID control design are also made under various operating conditions (disturbances due to external input/turbulence)
Keywords :
aircraft control; autoregressive moving average processes; control system synthesis; nonlinear control systems; three-term control; NARMAX representation; PID control design; aircraft system; exogenous excitation; integral minimum variance-like controller design; nonlinear autoregressive moving average process; Aerospace control; Aircraft; Autoregressive processes; Control systems; Equations; Frequency; Neural networks; Nonlinear control systems; Sliding mode control; Three-term control; Integral minimum variance; aircraft operations; nonlinear modelling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation, 2006. MED '06. 14th Mediterranean Conference on
Conference_Location :
Ancona
Print_ISBN :
0-9786720-1-1
Electronic_ISBN :
0-9786720-0-3
Type :
conf
DOI :
10.1109/MED.2006.328838
Filename :
4124964
Link To Document :
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