Four rotary-wing micro air vehicles use four motors as the power unit, by adjusting the motor speed control flight of underactuated systems [. In order to achieve four-rotor autonomous vehicle autonomous flight control, preliminary design of flight control system, and use F5F100LEA single-chip as computer control unit, Proposed the flight system hardware design. Vehicle has the advantages of light weight, small size, low power consumption. After several laboratory tests, the design and reliable performance, to meet the aircraft take off, hover, landing flight mode control requirements.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Four-Rotor Autonomous Vehicle



    Erschienen in:

    Erscheinungsdatum :

    2014-01-16


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Four-Rotor Autonomous Vehicle

    Wu, S.Y. / Lv, X.H. | British Library Conference Proceedings | 2014


    Autonomous Aerial Vehicle Rotor Configurations

    THOMPSON BENJAMIN SCOTT / BRY ADAM PARKER / ROBBINS-ROTHMAN ASHER MENDEL et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Autonomous cruise four-rotor aircraft and control system

    PAN YUZHI / ZHOU HAO | Europäisches Patentamt | 2021

    Freier Zugriff

    Four-rotor unmanned aerial vehicle

    WEI XIN | Europäisches Patentamt | 2015

    Freier Zugriff

    Folding four-rotor unmanned aerial vehicle

    WEI CHEN / FEI FAN / HE YIJIANG | Europäisches Patentamt | 2023

    Freier Zugriff