Title :
The T/D avionics integration methodology
Author :
Harbi, R. ; Beiser, D.
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;
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
DOI :
10.1109/CMPEUR.1990.113634
