DocumentCode
2395897
Title
The advanced avionics subsystem technology demonstration program
Author
Monaghan, Tim ; Kanawati, Ghani ; Abraham, Jacob ; Olson, Daniel ; Iyer, Ravi
Author_Institution
Naval Air Warfare Center, Warminster, PA, USA
fYear
1994
fDate
30 Oct-3 Nov 1994
Firstpage
389
Lastpage
401
Abstract
The Navy´s Advanced Avionics Subsystem Technology (AAST) Fault Tolerant program is clarifying the Navy´s fault tolerant avionics specifications methods and acceptance tests. The goal of the program will be clarify the Specification and Statement of Work language needed in future procurements and to demonstrate fault tolerant validation tools on an avionics design. A set of tool features will then be developed that spans the needs of fault tolerant computer system design from early concept studies to full scale production and operational support, both hardware and software. The paper will give an overview of the AAST Fault Tolerant Demonstration and focus on two tools that are being used in the demonstration: FERRARI-a software fault injector that will be used to validate the fault tolerance of the Common Integrated Processor (CIP), the F-22 Mission Processor and GRIND, a concept evaluation tool that will be used to evaluate the overall CIP architecture
Keywords
aircraft computers; computer architecture; fault tolerant computing; military computing; AAST Fault Tolerant Demonstration; CIP architecture; F-22 Mission Processor; FERRARI; GRIND; Navy; acceptance tests; advanced avionics subsystem technology; avionics design; avionics specifications; fault tolerant compute; fault tolerant program; fault tolerant validation tools; procurements; software fault injector; Aerospace electronics; Aircraft; Application software; Fault tolerance; Fault tolerant systems; Hardware; Jacobian matrices; Procurement; Research initiatives; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1994. 13th DASC., AIAA/IEEE
Conference_Location
Phoenix, AZ
Print_ISBN
0-7803-2425-0
Type
conf
DOI
10.1109/DASC.1994.369451
Filename
369451
Link To Document