DocumentCode :
1600654
Title :
Avionics product line software architecture flow policies
Author :
Sharp, David C.
Author_Institution :
Boeing Co., St. Louis, MO, USA
Volume :
2
fYear :
1999
fDate :
6/21/1905 12:00:00 AM
Abstract :
In 1995, an initiative was launched to assess the, potential for reuse of operational flight program software across multiple fighter aircraft platforms, and to define and demonstrate a supporting system architecture based upon open commercial hardware, software, standards and practices. The following year, this validation of the product line approach led to broader application of the techniques to the tactical aircraft mission processing domain. Key aspects of the component based logical architecture developed have been previously described. This paper briefly restates principle results from the previously published work to set the context for discussion. It then describes the flow policies, to be subsequently defined, developed on the project that substantively affect the product line reusability and suitability of the developed application components
Keywords :
aircraft computers; application program interfaces; data flow analysis; military avionics; military computing; open systems; software architecture; software reusability; API; avionics product line software architecture; control flow; data flow; flow policies; life cycle cost; message passing; multiple fighter aircraft platforms; operational flight program software; product line reusability; push-pull; software reuse; supporting system architecture; Aerospace electronics; Aircraft navigation; Application software; Collaborative software; Computer architecture; Control systems; Software architecture; Software performance; Software reusability; Software systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1999. Proceedings. 18th
Conference_Location :
St Louis, MO
Print_ISBN :
0-7803-5749-3
Type :
conf
DOI :
10.1109/DASC.1999.822052
Filename :
822052
Link To Document :
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