DocumentCode :
3125260
Title :
Developing safety cases for integrated flight systems
Author :
Blackwell, Nigel ; Leinster-Evans, Stewart ; Dawkins, Steven K.
Author_Institution :
BAe plc, Preston, UK
Volume :
5
fYear :
1999
fDate :
1999
Firstpage :
225
Abstract :
The successful application of integrated systems into the safety critical domain requires careful management and a realistic approach to planning the introduction of such systems. One such approach is through work on technology demonstration programs. British Aerospace and the UK Ministry of Defence have embarked on such a project, considering the integration of several flight critical applications across a common architecture from various view points including a safety perspective. This presented two main challenges: First, how can we define the safety properties of an architecture which must support safety critical systems whilst providing a more flexible structure which increases availability and reduces physical weight and maintenance? Second, how do we structure and reason about the safety properties of this architecture in a way that can drive design and safety analysis? This paper describes how these two challenges were addressed as part of the technology demonstration project at British Aerospace
Keywords :
aerospace computing; aircraft control; aircraft instrumentation; computer architecture; military computing; safety systems; safety-critical software; British Aerospace; UK Ministry of Defence; architecture; availability; flight critical applications; integrated flight systems; maintenance; physical weight; safety analysis; safety critical domain; safety critical systems; Aerospace control; Aerospace electronics; Aerospace industry; Aerospace safety; Air safety; Aircraft propulsion; Computer aided software engineering; Flexible structures; Military aircraft; Military computing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location :
Snowmass at Aspen, CO
Print_ISBN :
0-7803-5425-7
Type :
conf
DOI :
10.1109/AERO.1999.790204
Filename :
790204
Link To Document :
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