In this paper analysis the error of meteorological UAV Pitot-static tube wind model, meteorological UAV source of error in measuring the wind model is divided into: airspeed error, ground speed error, structural error, motion state error and angle error of five parts, using error analysis and simulation to research the sensitivity of each error, to improve a good basis for the accuracy of meteorological UAV Pitot-static tube model.


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    Titel :

    Meteorological UAV Pitot-static tube wind error source and sensitivity analysis


    Beteiligte:
    Yanjie Wang, (Autor:in) / Shudao Zhou, (Autor:in) / Hao Li, (Autor:in) / Guotao Zhu, (Autor:in) / Kejing Wei, (Autor:in)


    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    793369 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Further investigation of pitot-static tube

    Merriam, K.G. / Spaulding, E.R. | Engineering Index Backfile | 1935


    PITOT TUBE

    JACOB ROBIN / MAHAPATRA GURU PRASAD / JOHNSON PAUL ROBERT | Europäisches Patentamt | 2020

    Freier Zugriff

    Wind Tunnel and Flight Evaluation Rosemount Shielded Pitot-Static Tube Model 850N

    K. R. Ferrell / J. J. Shapley / J. Mishlof | NTIS | 1970


    Pitot static tube factor at low Reynolds numbers

    Ower, Ernest / Johansen, F. C. | TIBKAT | 1932