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
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