While Electro-Magnetic Compatibility testing is not often considered for CubeSat projects, the increasing complexity of nano-satellite platforms is suggesting to include such tests in their standard verification processes. This paper reports the followed approach and measurements set-up for an EMC anomaly regarding the LEDSAT 1U CubeSat Proto-Flight Model on-board GPS antenna. The anomaly was discovered and solved during functional testing campaign in 2020 and the satellite has been successfully qualified for flight.


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    Titel :

    LEDSAT 1U CubeSat GPS receiver Electro-Magnetic Interference (EMI) analysis


    Beteiligte:
    Frezza, Lorenzo (Autor:in) / Marzioli, Paolo (Autor:in) / Picci, Niccolo (Autor:in) / Gianfermo, Andrea (Autor:in) / Bedetti, Emanuele (Autor:in) / Amadio, Diego (Autor:in) / Curiano, Federico (Autor:in) / Santoni, Fabio (Autor:in)


    Erscheinungsdatum :

    2021-06-23


    Format / Umfang :

    2846790 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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