This paper presents an overall control system for the automatic landing of a quadrotor UAV on a moving platform. Herein, the vehicle control system comprises a nonlinear inner loop attitude control and an outer loop velocity control system based on static inversion. The vehicle control system is finally realized in an experimental prototype and first test flights proof the performance of this novel nonlinear approach. The landing controller consists of a linear altitude controller and a nonlinear 2D-tracking controller. Simulation results finally underline the performance of the landing control system.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear landing control for quadrotor UAVs


    Weitere Titelangaben:

    Nichtlineares Steuern des Landevorgangs von Quadrotor UAV (unbemannte Flugobjekte)


    Beteiligte:
    Voos, Holger (Autor:in)


    Erscheinungsdatum :

    2009


    Format / Umfang :

    8 Seiten, 6 Bilder, 8 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Integrating Backstepping Control of Outdoor Quadrotor UAVs

    Bodó, Zsófia / Lantos, Béla | BASE | 2019

    Freier Zugriff

    Nonlinear Adaptive Control of Quadrotor UAVs with Run-Time Safety Assurance

    Avram, Remus / Zhang, Xiaodong / Muse, Jonathan A. et al. | AIAA | 2017


    A Binocular Vision-Assisted Method for the Accurate Positioning and Landing of Quadrotor UAVs

    Jie Yang / Kunling He / Jie Zhang et al. | DOAJ | 2025

    Freier Zugriff

    A Review of Control Methods for Quadrotor UAVs

    Guo, Xitong / Hou, Shengjie / Niu, Pingjuan et al. | IEEE | 2022


    Randomized approaches and adaptive control for quadrotor UAVs

    Capello, Elisa / Quagliotti, Fulvia / Tempo, Roberto | IEEE | 2013