This paper examines a multi-rotor unmanned aerial vehicle and the influence of the ground effect on the aircraft during the landing stage. Theoretical and practical research of other authors and results are described. It is briefly discussed how the position of the high-pressure area changes with changing environmental conditions. The study examined the ground effect on the drone at 1/3R - 2R. Calculations show that the propeller thrust increases up to 7%. Also, discussing the results, it has been hypothesized that an increase in thrust near the ground will reduce engine speed, which may directly impact the drone's stability and landing accuracy. Further research is needed to explore this issue further.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Influence of the Ground Effect on the Precise Landing of an Unmanned Aircraft


    Additional title:

    Lecture Notes in Intelligent Transportation and Infrastructure



    Conference:

    International Conference TRANSBALTICA: Transportation Science and Technology ; 2022 ; Vilnius, Lithuania September 15, 2022 - September 16, 2022



    Publication date :

    2023-02-22


    Size :

    6 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Precise landing unmanned aerodynamic parachute

    JI SHUDE / SHI HAO / REN XUXU et al. | European Patent Office | 2023

    Free access

    Unmanned aircraft landing gear and unmanned aircraft with same

    LI XIAOYU / ZHANG LING | European Patent Office | 2015

    Free access

    Landing gear of unmanned aircraft

    ZHANG PING | European Patent Office | 2015

    Free access

    UNMANNED AIRCRAFT WITH PARACHUTE LANDING SYSTEM

    MALOV YURIJ IVANOVICH / KIBETS DMITRIJ ARKHIPOVICH / KOLDAEV ALEKSANDR VASILEVICH | European Patent Office | 2021

    Free access

    Retractable landing gear of unmanned aircraft

    TANG JIE / YANG JIANJUN | European Patent Office | 2015

    Free access