DocumentCode :
158544
Title :
Temperature control of an aeronautical pneumatic system using feedback linearization and PID
Author :
Dias da Silva, Dayvis ; Turcio, Wallace ; Aoun Tannuri, Eduardo
Author_Institution :
Embraer - Eng. & Technol. (Syst. Simulation), São José dos Campos, Brazil
fYear :
2014
fDate :
16-19 June 2014
Firstpage :
942
Lastpage :
947
Abstract :
This work presents a simplified nonlinear model for an aeronautical pneumatic system. A methodology for designing the system temperature control is proposed using the feedback linearization theory combined with a PID. Simulation results performed with Matlab/Simulink® are presented and discussed.
Keywords :
aircraft control; feedback; linearisation techniques; nonlinear control systems; pneumatic systems; temperature control; three-term control; Matlab/Simulink; PID; aeronautical pneumatic system; feedback linearization theory; nonlinear model; system temperature control; Heating; Pistons; Pneumatic systems; Temperature measurement; Temperature sensors; Valves;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation (MED), 2014 22nd Mediterranean Conference of
Conference_Location :
Palermo
Print_ISBN :
978-1-4799-5900-6
Type :
conf
DOI :
10.1109/MED.2014.6961495
Filename :
6961495
Link To Document :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=158544
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