This paper deals with the design of four controllers, based on Backstepping and Sliding Modes, which are applied to a fixed-wing unmanned aerial vehicle (UAV). We are interested to realize a comparative analysis of such methodologies in order to know what controller has a better performance when they are used to the autonomous flight (altitude, yaw and roll) of a fixed-wing UAV. The designed controllers are: Backstepping, sliding mode control (SMC), Backstepping with sliding mode control, and Backstepping with two sliding mode control. Simulation results are obtained in order to analyze the controllers. We finally present an experimental result, in open-loop, with the purpose of validate the magnitud of the control signals obtained in the simulations.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Backstepping — Sliding mode controllers applied to a fixed-wing UAV


    Beteiligte:
    Espinoza, T. (Autor:in) / Dzul, A. (Autor:in) / Lozano, R. (Autor:in) / Parada, P. (Autor:in)


    Erscheinungsdatum :

    01.05.2013


    Format / Umfang :

    1071712 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Nonlinear Controllers Applied to Fixed-Wing UAV

    Espinoza, Tadeo / Dzul, Alejandro / Garcia, Luis et al. | IEEE | 2012


    Neural-Network-Based Incremental Backstepping Sliding Mode Control for Flying-Wing Aircraft

    Liu, Shiqian / Lyu, Weizhi / Zhang, Qian et al. | AIAA | 2025


    Longitudinal Control of Agile Fixed-Wing UAV Using Backstepping

    Sajith Kumar, K. K. / Arya, Hemendra / Joshi, Ashok | IEEE | 2019



    Backstepping sliding mode control for formation flying spacecraft

    Guo, Yong / Song, Shen-Min / Li, Xue-Hui | Emerald Group Publishing | 2018