DocumentCode :
2290015
Title :
Built-in-test adequacy-evaluation methodology for an air-vehicle system
Author :
Beniquez, Dario R. ; Witteried, David C.
Author_Institution :
USAF, Edwards AFB, CA, USA
fYear :
1995
fDate :
16-19 Jan 1995
Firstpage :
290
Lastpage :
295
Abstract :
Rapid improvement in built-in-test (BIT) system capability is probably one of the most important activities in an air-vehicle system development test and evaluation program. An effective BIT adequacy evaluation methodology can accomplish this. The methodology must provide the development tester BIT parameters that serve as indicators of air-vehicle BIT system performance. Deficiencies that are pinpointed can then be corrected to improve the overall BIT system´s performance. A BIT adequacy evaluation methodology developed and implemented during a recently conducted Air Force development and test program did just that. It provided real-time technical information at a particular period that indicated the status of the BIT system in relation to specified requirements. It also served as a springboard to evaluate the BIT system, and to document the results, which provided the manufacturer with valuable data on the BIT system´s performance. Finally, it gave the manufacturer the opportunity to implement corrective actions within the allocated schedule, and develop the air-vehicle BIT system concurrently
Keywords :
aerospace computing; aircraft; aircraft testing; built-in self test; computerised instrumentation; reliability; Air Force; adequacy evaluation methodology; aircraft reliability; built-in-test; development; performance; real-time; test program; Fault detection; Hardware; Job shop scheduling; Manufacturing; Personnel; Real time systems; Software testing; System performance; System testing; Weapons;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1995. Proceedings., Annual
Conference_Location :
Washington, DC
ISSN :
0149-144X
Print_ISBN :
0-7803-2470-6
Type :
conf
DOI :
10.1109/RAMS.1995.513260
Filename :
513260
Link To Document :
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