The take-off control of UAV with fly wing layout is limited by its relatively lower pitch moment. This paper gained the state parameters of a few groups of taking off model by means of numerical simulation. The influence of different models on take-off distance, take-off angle of attack (AOA), take-off safe speed and c.g. location was then analyzed. Based on the analysis, a new fly wing constitution was designed and the corresponding take-off control scheme was suggested as well. Finally, the flight test results shows that this fly wing constitution can gain better take-off control characteristics.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution



    Erschienen in:

    Erscheinungsdatum :

    2012-02-10


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution

    Mo, Song / Huang, Jun / Chai, Xue et al. | Tema Archiv | 2012


    Letting Thoughts Take Wing

    Jorgensen, Chuck / Wheeler, Kevin | NTRS | 2002


    ROTARY-WING AIRCRAFT WITH VERTICAL TAKE-OFF

    PARASTAYEV ANDREY ZELIMKHANOVICH | Europäisches Patentamt | 2015

    Freier Zugriff

    Research on Aerodynamic Characteristics of General Long Endurance Vertical Take-Off and Landing Fixed Wing UAV

    Li, Zhan-ke / Zhang, Liang-yang / Zhang, Si-jia et al. | Springer Verlag | 2022


    VERTICAL TAKE-OFF BOX WING AIRCRAFT

    TAYLOR ALEXANDER JAMES | Europäisches Patentamt | 2022

    Freier Zugriff