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Radiated emissions of the power converter module of the polarimetric and helioseismic imager instrument on board of solar orbiter: A case study

Authors :
D. Osorno Caudet
Johann Hirzberger
M. Herranz de la Revilla
M. Balaguer Jiménez
J. L. Gasent Blesa
A. Ferreres Sabater
J. Jordan Martinez
Ph. Laget
E. Sanchis Kilders
R. Meller
A. C. López Jiménez
J.B. Ejea Marti
E. Maset Sancho
V. Esteve Gomez
Source :
2016 ESA Workshop on Aerospace EMC (Aerospace EMC).
Publication Year :
2016
Publisher :
IEEE, 2016.

Abstract

EMC requirements for scientific satellites are usually very stringent and much more demanding than terrestrial standards, mainly because ad-hoc scientific instruments developed for the mission require very quiet electromagnetic environments to perform their science. These requirements will assure the compatibility of all instruments on board and with the platform. The electromagnetic noise generated by the DC/DC converter of the PHI instrument, to be flown on board Solar Orbiter, has been drastically reduced applying several different techniques. One technique has been to change the grounding strategy from a single point grounding to a distributed grounding. Two additional techniques were needed to reach the required noise floor. Experimental measurements show the improvements achieved with each technique.

Details

Database :
OpenAIRE
Journal :
2016 ESA Workshop on Aerospace EMC (Aerospace EMC)
Accession number :
edsair.doi...........01cea541c0a752fe1bf96881860489bb