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With increasingly using for spacecraft applications which demand the high reliability, validating the performance of Multicore SoC is extremely important for its significant properties of over-complexity, high integration level, high processing rate and miniaturized feature size. In this paper, we discuss the objective and properties of the Multicore SoC's post-silicon performance validation base...
Historically, spacecraft power system nominal bus voltages have been increasing over time to accommodate increasing bus load demands while reducing spacecraft mass, particularly in electrical harnesses. The use of higher nominal spacecraft bus voltages requires higher rated circuit protection devices as well as a thorough understanding of power system dynamics during fault clearing events. In this...
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