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Although the Space Weather has been directly and indirectly identified as the source for a large percentage of S/C abnormal behaviours (through high radiation levels emissions, solar flares and magnetically induced fields), little can be done by FCT operators up until now to minimize the impact of S/C faults. One of the most common observed faults in S/C, are SEUs (Single Event Upsets), which are mainly caused by S/C exposure to excessive amounts of radiation. These SEUs occur when a single ionising radiation event (direct ionisations/proton-induced nuclear reactions) produces a burst of hole-electron pair in a digital circuit, large enough to cause the circuit to change the state, preventing the execution of nominal operations for a particular unit or resulting in permanent damage of the unit itself. One of the responsibilities of the Flight Control Teams is to try to optimise the operations on the S/C during known occurrences of high radiation levels, in order to prolong the expected operation usage time of the instruments. The most common risk-avoidance procedure consists in reaching a so-called ‘safe configuration’ for the units (e.g. switching off the instruments high-voltages/biases off), or (when available