This paper focus the property and application on an innovative yawing control effector for unmanned aerial vehicles (UAV) named all moving wing tips (AMT). The prospective application area of AMT is flying wing and other kind of stealth fighters. In terms of performance, it has a linearly drag output through a deflection from 20° to 60°, which is friendly to control methodology, and the yawing control efficiency is at a same order of magnitude with the traditional rudder. The AMT has a good prospect of application on future UAVs.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Development of the AMT in yawing control of flying wing UAVs


    Contributors:
    Bie, Dawei (author) / Gan, Wenbiao (author) / Ma, Tielin (author) / Zhang, Qinling (author) / Zhang, Xiaoou (author)


    Publication date :

    2017-10-01


    Size :

    493736 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Control characteristics analysis of drag yawing control devices of flying wing configuration

    Zhongjian, L. / Dongli, M. | British Library Online Contents | 2014



    Multicopter Yawing Control System

    CHOI JONG PIL | European Patent Office | 2021

    Free access

    Multicopter Yawing Control System

    European Patent Office | 2021

    Free access

    Flying-wing development

    Taylor, J.W.R. | Engineering Index Backfile | 1947