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|Title: ||On automating failure mode analysis and enforcing its integrity|
|Authors: ||Tai, Ann T.|
Tso, Kam S.
Chau, Savio N.
|Keywords: ||design for safety|
failure mode analysis
design source code
failure mode, cause, and effect analysis (FMECA)
|Issue Date: ||16-May-2005 |
|Publisher: ||Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005.|
|Citation: ||11th International Symposium of Pacific Rim Dependable Computing, Hunan, China, December 12 - 14, 2005.|
|Abstract: ||This paper reports our experience on the development of a design-for-safety (DFS) workbench called Risk Assessment and Management Environment (RAME) for microelectronic avionics systems. Our objective is to transform DFS practice from an ad-hoc, inefficient, error-prone approach to a stringent engineering process such that DFS can keep up with the rapidly growing complexity of avionics systems. In particular, RAME is built upon an information infrastructure that comprises a fault model, a knowledge base, and a failure reporting/tracking system. This infrastructure permits systematic learning from prior projects and enables the automation of failure modes, effects and criticality analysis (FMECA). Among other unique features, the most important advantage of RAME is its capability of directly accepting design source code in hardware description languages (HDLs) for automated failure mode analysis...|
|Appears in Collections:||JPL TRS 1992+|
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