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NASA NTRS · 19890030741

Impact of device level faults in a digital avionic processor

Abstract

This paper describes an experimental analysis of the impact of gate and device-level faults in the processor of a flight control system. Via mixed mode simulation faults were injected both at the gate (stuck-at) and at the transistor levels, and their propagation through the chip to the output pins was measured. The results show that there is little correspondence between a stuck-at and a device-level fault model insofar as error activity or detection within a functional unit is concerned. Insofar as error activity outside the injected unit and at the output pins are concerned, the stuck-at and device models track each other, although the stuck-at model overestimates, by over one hundred percent, the probability of fault propagation to the output pins. The stuck-at model significantly underestimates the impact of an internal chip fault on the output pins.

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BibTeXRIS

Kim, S., Iyer, R. K.. 1988-01-01. Impact of device level faults in a digital avionic processor. https://ntrs.nasa.gov/citations/19890030741

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