Modern aircraft turboprop engines are generally managed by pilots by using the well-established two-levers approach which allows the pilot to control independently the engine thrust (power lever) and the propeller rotational speed (condition lever). On the other hand, the twolevers governing system presents several disadvantages in terms of pilot training, fuel consumption and aircraft maintenance. The one-lever approach tries to solve such drawbacks regulating at the same time the engine power and the propeller pitch. In the present work a Multi-Agent Fuzzy Logic control algorithm has been proposed to implement the one-lever approach for the control of the variable pitch turboprop aircraft propulsion system. The whole aircraft ecosystem has been developed in Simulink® framework to verify the feasibility and performance of the proposed one-lever approach.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Multi-Agent Fuzzy Logic Controller applied to One Lever Variable Pitch Turboprop Aircraft


    Beteiligte:


    Erscheinungsdatum :

    2021




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    One Lever Control for Variable Pitch Turboprop Aircraft

    Gaudio Giovanni / Dambrosio Lorenzo | DOAJ | 2020

    Freier Zugriff

    Electric variable-pitch turboprop engine

    QIU GUOCAI / HAN GUANGLEI / LU YUQUAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Propeller pitch control system for aircraft turboprop engines

    FUTA JR PAUL W / TILLICH SAMMUEL / LEWIS STEVEN ALAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    PROPELLER PITCH CONTROL SYSTEM FOR AIRCRAFT TURBOPROP ENGINES

    FUTA JR PAUL W / TILLICH SAMMUEL / LEWIS STEVEN ALAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Single Lever Power Management of Turboprop Engines

    Prevallet, L.C. | SAE Technical Papers | 1991