The stability control of unmanned aerial vehicle (UAV) is the most important technology when it is on the duty of taking area photos. This paper aims at analyzing the structures, the corresponding channel of control and control modes in small fixed-wing UAV, and focuses on flight control system, which systematically reveals the running rules of UAV. According to the control theories in UVA, the paper explains the method of stability controlling UAV from two major aspects, the longitudinal and lateral movement control, based on the UAV flight operation process. By understanding the structures, the modes, the rules and the theories, the paper achieves the goal that can catch the method of fully controlling UAV.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Stability control of small fixed-wing UAV


    Beteiligte:
    Yuan Cheng (Autor:in) / Shouzhi Xu (Autor:in) / Zhiyong Huang (Autor:in) / Biao Xiong (Autor:in) / Chao Wang (Autor:in)


    Erscheinungsdatum :

    01.06.2014


    Format / Umfang :

    1576631 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    COVER FOR SMALL FIXED-WING AIRCRAFT

    ISHIZUKA MASAO | Europäisches Patentamt | 2018

    Freier Zugriff


    Adaptive Control for Small Fixed-Wing Unmanned Air Vehicles

    Kahn, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010


    FIXED WING DRONE FIXED WING DRONE

    Europäisches Patentamt | 2021

    Freier Zugriff

    FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY

    HUBSCHWERLEN FRÉDÉRIC | Europäisches Patentamt | 2018

    Freier Zugriff