DocumentCode :
1604960
Title :
Onboard diagnostics of avionics for fault tolerance and maintenance
Author :
Hammett, Robert
Author_Institution :
C.S. Draper Lab., Cambridge, MA, USA
fYear :
1992
Firstpage :
323
Abstract :
Summary form only given. Emerging modular avionics systems will require excellent onboard fault diagnosis, both to support flight critical functions and to provide for cost effective maintenance. The approach to fault isolation discussed makes use of multiple indications of failures, known as failure signatures or syndromes. A computer-aided design tool that can analyze the architecture and generate syndrome data for inclusion in embedded software algorithms has been developed. This tool performs automatic failure dependency analysis using as input a graphical schematic of the system to be analyzed. A further complication arises with the syndrome approach when detection tests fail to operate correctly. A method of mitigating this problem using partial pattern matching techniques on the pattern of test failure indication has also been developed. Other benefits of this approach are outlined.<>
Keywords :
aircraft instrumentation; automatic test equipment; electronic equipment testing; failure analysis; fault location; maintenance engineering; automatic failure dependency analysis; computer-aided design tool; cost effective maintenance; embedded software algorithms; failure signatures; fault isolation; fault tolerance; flight critical functions; maintenance; modular avionics; multiple indications of failures; onboard fault diagnosis; partial pattern matching; syndromes; Aerospace electronics; Algorithm design and analysis; Computer architecture; Cost function; Design automation; Failure analysis; Fault diagnosis; Fault tolerance; Performance analysis; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
AUTOTESTCON '92. IEEE Systems Readiness Technology Conference, Conference Record
Conference_Location :
Dayton, OH, USA
Print_ISBN :
0-7803-0643-0
Type :
conf
DOI :
10.1109/AUTEST.1992.270095
Filename :
270095
Link To Document :
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