In this paper we present a project aimed for the designing of a small scale Unmanned Aerial Vehicle (UAV) with Tiltrotor configuration (that uses two rotating rotors). The proposed UAV is build from scratch, based on Commercial Off-The-Shelf (COTS) components. The related development ranges from designing the control algorithms to the wireless communication infrastructure. Our aim is to create an open source project that can be used as reference for future UAV design in industry and academia. The current paper describes the adopted design methodology, the mathematical and computational models created to represent the UAV, the physical components that constitute the UAV, and the results obtained so far.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Small scale UAV with birotor configuration


    Beteiligte:
    Goncalves, F.S. (Autor:in) / Bodanese, J. P. (Autor:in) / Donadel, R. (Autor:in) / Raffo, G. V. (Autor:in) / Normey-Rico, J. E. (Autor:in) / Becker, L. B. (Autor:in)


    Erscheinungsdatum :

    01.05.2013


    Format / Umfang :

    519748 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Hybrid power system based on birotor motor

    GUO MINGMING | Europäisches Patentamt | 2021

    Freier Zugriff


    engin volant birotor à décollage et atterrissage vertical

    VIGUIER FRANÇOIS | Europäisches Patentamt | 2021

    Freier Zugriff

    Radlagereinheiten der zweiten Generation im Citroen GS Birotor

    Druet, C. / Monville, J. | Tema Archiv | 1974


    BAQUET-CHÂSSIS SÉCURISÉ DE PARAMOTEUR À PROPULSION BIROTOR EXPORTÉE ARRIÈRE LATÉRALE

    MARTZ CHRISTOPHE | Europäisches Patentamt | 2025

    Freier Zugriff