search-head

Sie sind hier: Homepage >  Suche

    Pseudomeasurement-Aided Estimation of Angle of Attack in Mini Unmanned Aerial Vehicle

    Pseudomeasurement-Aided Estimation of Angle of Attack in Mini Unmanned Aerial Vehicle


    This work focuses on a novel pseudomeasurement-aided estimation scheme for angle of attack (AOA) in a mini unmanned aerial vehicle with a 1.61 m wingspan. A scale-reduced model of the same is used in a wind tunnel, and the necessary measurements are recorded. Wind-tunnel measurements are used to write down the C L and C D equations of the flight vehicle. A pseudomeasurement-aided scheme for estimation of AOA is established using an aerodynamic model extracted from wind-tunnel experiments. Computational analysis of the estimation scheme is performed, followed by flight tests and postflight analysis. The flight vehicle is instrumented with all the necessary sensors, along with a commercially available AOA vane probe (Swiss Air data smart miniature vane SMV-1) for direct measurements of AOA. Using flight recorded data in a MATLAB program, the estimated AOA is compared with actual measurements of Alpha α , and estimation schemes performances are evaluated.

    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €

    Exportieren, teilen und zitieren

    Dokumentinformationen

    Titel :

    Pseudomeasurement-Aided Estimation of Angle of Attack in Mini Unmanned Aerial Vehicle

    Beteiligte:
    Prem, S. (Autor:in) / Sankaralingam, L. (Autor:in) / Ramprasadh, C. (Autor:in)
    Erschienen in:

    Journal of Aerospace Information Systems ; 17 , 11 ; 603-614

    Erscheinungsdatum :

    2020-08-06

    Format / Umfang :

    12 pages

    ISSN :

    2327-3097

    DOI :

    https://doi.org/10.2514/1.I010783

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    Remotely Piloted Aircraft , Aerodynamic Angle , Flight Test Vehicle , Onboard Sensors , Wind Tunnel Models , Flight Vehicle , MATLAB , Level Flight , Climbing Flight , Extended Kalman Filter

    Ähnliche Titel

    TO DESIGN AND BUILD OF A SURVEILLANCE/ATTACK MINI UNMANNED AERIAL VEHICLE (UAV)

    A.Serkan AKGÜL / Abdurrahman HACIOĞLU | DOAJ | 2010

    Freier Zugriff

    Wind tunnel test unmanned aerial vehicle attack angle automatic adjusting system

    LIU WENSHUAI / YAO XIAOMIN / HAN WENTING | Europäisches Patentamt | 2021

    Freier Zugriff

    FIXED-WING UNMANNED AERIAL VEHICLE CAPABLE OF HIGH ANGLE-OF-ATTACK MANEUVERING

    MOORE JOSEPH L / BASESCU MAX R / POLEVOY ADAM C et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Reconnaissance and attack integrated unmanned aerial vehicle

    PEI ZHONGJUN / XIONG XIN / XIONG YIFA et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Detachable reconnaissance and attack unmanned aerial vehicle

    WAN MINGQUAN / ZHANG ZHIQI / LIU TIANYU et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €

    Seitennavigation

    Dokumentinformationen

    Ähnliche Titel

    Exportieren, teilen und zitieren