DocumentCode
2706412
Title
The T/D avionics integration methodology
Author
Harbi, R. ; Beiser, D.
fYear
1990
fDate
8-10 May 1990
Firstpage
270
Lastpage
272
Abstract
The methodology of system integration that was applied in the development of the avionics system of the T/D aircraft is described. This methodology is part of the entire-life-cycle methodology. The integration methodology uses the executable system description that evolves during the system development both for test preparation and test execution. The method is equivalent to rapid prototyping
Keywords
aerospace computing; aircraft instrumentation; T/D aircraft; T/D avionics integration methodology; entire-life-cycle methodology; rapid prototyping; system development; system integration; test execution; test preparation; Aerospace electronics; Aircraft; Airports; Computer displays; Control systems; Distributed computing; Iterative methods; Laboratories; Prototypes; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
CompEuro '90. Proceedings of the 1990 IEEE International Conference on Computer Systems and Software Engineering
Conference_Location
Tel-Aviv
Print_ISBN
0-8186-2041-2
Type
conf
DOI
10.1109/CMPEUR.1990.113634
Filename
113634
Link To Document