The paper is devoted to the review of controlled motion of the unmanned aerial vehicle (UAV) with vertical takeoff and landing, the convertiplane type, with three tilt rotors. The UAV is equipped with a swept wing, the calculation of aerodynamic parameters of which has been carried out in the software program XFLR5, taking into consideration the weight and size requirements. There have been determined the lift and resistance coefficients of the UAV depending on the angle of attack on the basis of the vortex method. There has been done the analysis of the influence of wing profile on the calculated aerodynamic characteristics. There also has been realized the synthesis of the traction energy-efficient options of the drive propellers that reduce power consumption, increasing the accuracy of the automatic control system.


    Access

    Download


    Export, share and cite



    Title :

    The Synthesis of Electric Drives Characteristics of the UAV of “Convertiplane–Tricopter” Type


    Contributors:


    Publication date :

    2017




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    CONVERTIPLANE

    ZIMENSKAYA ELLINA VLADIMIROVNA | European Patent Office | 2021

    Free access

    Convertiplane

    WANG JAMES | European Patent Office | 2016

    Free access

    Convertiplane

    BIANCO MENGOTTI RICCARDO / CASSINELLI CARLO / SCANDROGLIO ALESSANDRO et al. | European Patent Office | 2024

    Free access

    CONVERTIPLANE

    SABADASH ANDREJ ANDREEVICH / MILEVSKIJ ALEKSANDR VLADIMIROVICH | European Patent Office | 2020

    Free access

    Convertiplane (variants)

    RAZROEV ELDAR ALI OGLY | European Patent Office | 2017

    Free access