DocumentCode :
2397785
Title :
The architectural specification of an avionic subsystem
Author :
Barroca, L.M. ; Fitzgerald, J.S. ; Spencer, L.
Author_Institution :
Dept. of Comput., Open Univ., Milton Keynes, UK
fYear :
1995
fDate :
5-8 Apr 1995
Firstpage :
17
Lastpage :
29
Abstract :
The work of the British Aerospace Dependable Computing Systems Centre includes the development of formal techniques for use in defining and tracing requirements for software systems at the system architecture level. A basic repertoire of techniques proposed so far includes the graphical representation of timing requirements allied to model-oriented specifications of functionality. This paper gives an overview of these techniques and reports on a small study in their application conducted by British Aerospace Defence. The study uses a realistic example of an avionics system: the pilot data entry system for a waypoint database. The example is described with some technical detail. Formally analysing a timing requirement for the rate of data entry yields local timing requirements for the cockpit equipments. Conclusions assess the value of these techniques, as perceived by BAe systems developers and propose further work in providing tool support
Keywords :
aircraft computers; formal specification; real-time systems; safety-critical software; architectural specification; avionic subsystem; formal techniques; functionality; local timing requirements; model-oriented specifications; pilot data entry system; system architecture level; timing requirements; waypoint database; Aerospace electronics; Aerospace industry; Coils; Databases; Military aircraft; Military computing; Production; Real time systems; Software reliability; Timing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial-Strength Formal Specification Techniques, 1995. Proceedings., Workshop on
Conference_Location :
Boca Raton, FL
Print_ISBN :
0-8186-7005-3
Type :
conf
DOI :
10.1109/WIFT.1995.515476
Filename :
515476
Link To Document :
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