A linear quadratic regulator (LQR) based adaptive optimal control method for aircraft engine is presented. Firstly, an LQR controller is designed for the nominal system, based on which, a adaptive controller is designed by using the back-stepping technique. With the proposed method, the system uncertainties and external disturbances can be compensated, and the actual controller can converge to the LQR controller as close as possible. Finally, a turbofan engine simulation is considered to illustrate the effectiveness of the proposed method.


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    Titel :

    LQR-Based Adaptive Optimal Control for Aircraft Engine


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Jia, Yingmin (Herausgeber:in) / Zhang, Weicun (Herausgeber:in) / Fu, Yongling (Herausgeber:in) / Wang, Jiqiang (Herausgeber:in) / Zhao, Jinsong (Autor:in) / Lin, Yan (Autor:in) / Li, Lin (Autor:in)

    Kongress:

    Chinese Intelligent Systems Conference ; 2023 ; Ningbo, China October 14, 2023 - October 15, 2023



    Erscheinungsdatum :

    08.10.2023


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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