Field programmable gate array (FPGA) devices, heavily used in spacecraft el
ectronics, have grown substantially in size over the past few years, causin
g designers to work at a higher conceptual level, with computer aided engin
eering (CAE) tools synthesizing and optimizing the logic from a description
. It is shown that the use of commercial-off-the-shelf (COTS) CAE tools can
produce unreliable circuit designs when the device is used in a radiation
environment and a flip-flop is upset. At a lower level, software can be use
d to improve the SEU performance of a flip-flop, exploiting the configurabl
e nature of FPGA technology and on-chip delay, parasitic resistive, and cap
acitive circuit elements.