This paper describes the design and development of a feedback system for controlling the dynamics of a flapping wing nano air vehcile (NAV). A model of the vehicle dynamics and models of sensors and unique actuator mechanisms are built. An extended Kalman filter is designed to eliminate the effects of sensor bias on state estimation. Results of this study demonstrate stability and yield responses that are approaching desired performance capabilities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Onboard Stability Control System for a Flapping Wing Nano Air Vehicle


    Beteiligte:
    J. Geder (Autor:in)

    Erscheinungsdatum :

    2009


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flapping-wing air vehicle driving device and flapping-wing air vehicle

    WU ZHIYI / HU SHUANGTING / WANG ZHONGLIN | Europäisches Patentamt | 2022

    Freier Zugriff

    FLAPPING WING AERIAL VEHICLE

    KARASEK MATEJ | Europäisches Patentamt | 2020

    Freier Zugriff

    Flapping wing air vehicle

    LI ZHIGUO | Europäisches Patentamt | 2020

    Freier Zugriff

    Flapping wing air vehicle

    LI SHUFAN / MA PENGPENG / HOU DAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    FLAPPING WING AERIAL VEHICLE

    KARASEK MATEJ | Europäisches Patentamt | 2018

    Freier Zugriff