• 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.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=158544