We propose a novel tilt tri-rotor flying-wing aircraft, which consists of a flying wing and three tilting propellers configured at left, right and rear parts. In order to adapt to different flight scenarios, three flight modes are introduced and the aircraft can transform among them. To design position/attitude controllers in the hover mode, a 6-DOF dynamic model of aircraft is given. Then a cascade proportional-derivative (PD) controller is designed by means of feedback linearization and a novel control allocation method which is conducive to mode transformation is proposed. Finally, the controller is tested in MATLAB/Simulink environment. The experimental results have shown the effectiveness of the controller.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design and Hover Control of a Tilt Tri-rotor Flying-wing Aircraft


    Beteiligte:
    Wu, Zhiyuan (Autor:in) / Wang, Yong (Autor:in) / Zhou, Tong (Autor:in) / Shuai, Jianmei (Autor:in)


    Erscheinungsdatum :

    2021-05-28


    Format / Umfang :

    837252 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    TILT-ROTOR AIRCRAFT WING

    KIM CHEOL WAN / LEE YUNG GYO | Europäisches Patentamt | 2016

    Freier Zugriff

    Tilt rotor broadband hover aeroacoustics

    Coffen, C.D. / George, A.R. | Tema Archiv | 1993


    Hover aircraft rotor and hover aircraft

    ATTILIO COLOMBO | Europäisches Patentamt | 2015

    Freier Zugriff