A systematic, analytical methodology for aircraft system safety assessment is explained. A try-out on a software controlled digital avionics system is summarized. Analysis of software components is emphasized. It is concluded that the same methodology can be applied to software and hardware. Conditions that have to be met to perform a successful hardware/software safety assessment are described.
Hardware/Software Failure Mode Effect Analysis (FMEA) Applied to Airplane Safety
1984
9 pages
Report
Keine Angabe
Englisch
Hardware/software FMEA applied to airplane safety
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