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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Small scale UAV with birotor configuration


    Contributors:


    Publication date :

    2013-05-01


    Size :

    519748 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Hybrid power system based on birotor motor

    GUO MINGMING | European Patent Office | 2021

    Free access


    engin volant birotor à décollage et atterrissage vertical

    VIGUIER FRANÇOIS | European Patent Office | 2021

    Free access

    Radlagereinheiten der zweiten Generation im Citroen GS Birotor

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