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.
LEDSAT 1U CubeSat GPS receiver electro-magnetic interference (EMI) analysis / Frezza, L.; Marzioli, P.; Picci, N.; Gianfermo, A.; Bedetti, E.; Amadio, D.; Curiano, F.; Santoni, F.. - (2021), pp. 137-142. (Intervento presentato al convegno 8th IEEE International workshop on metrology for aeroSpace, metroaerospace 2021 tenutosi a Virtual, online) [10.1109/MetroAeroSpace51421.2021.9511714].
LEDSAT 1U CubeSat GPS receiver electro-magnetic interference (EMI) analysis
Frezza L.;Marzioli P.;Picci N.;Gianfermo A.;Bedetti E.;Amadio D.;Santoni F.
2021
Abstract
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.| File | Dimensione | Formato | |
|---|---|---|---|
|
Frezza_LEDSAT_2021.pdf
solo gestori archivio
Tipologia:
Versione editoriale (versione pubblicata con il layout dell'editore)
Licenza:
Tutti i diritti riservati (All rights reserved)
Dimensione
2.78 MB
Formato
Adobe PDF
|
2.78 MB | Adobe PDF | Contatta l'autore |
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
