This paper deals with the experimental validation of linear controllers for a fixed-wing Miniature Air Vehicle (MAV). We are interested to realize a comparative analysis of two linear controllers, Proportional Integral Derivative (PID) and Proportional Derivative (PD), in order to know what controller has a better performance when they are used on an autonomous flight (altitude, yaw and roll). Experimental results are obtained in order to analyze the controllers and validate the performance of the fixed-wing MAV in presence of perturbations like wind gusts.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Linear controllers implementation for a fixed-wing MAV


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


    Erscheinungsdatum :

    2014-05-01


    Format / Umfang :

    1053899 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


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

    Espinoza, T. / Dzul, A. / Lozano, R. et al. | IEEE | 2013


    FIXED WING DRONE FIXED WING DRONE

    Europäisches Patentamt | 2021

    Freier Zugriff

    Wing and fixed-wing aircraft

    HUANG JINGTAO / MA XIWANG / WANG CHEN'AN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    FIXED WING ENHANCER (MINI-WING)

    Europäisches Patentamt | 2015

    Freier Zugriff