DocumentCode :
2592560
Title :
A flexible fault tolerant processor for launch vehicle avionics systems
Author :
Taylor, R.C. ; Van Hoff, P. ; Walter, C.
Author_Institution :
Allied-Signal Aerosp. Co., Teterboro, NJ, USA
fYear :
1990
fDate :
15-18 Oct 1990
Firstpage :
147
Lastpage :
152
Abstract :
The multicomputer architecture for fault tolerance (MAFT), a highly flexible approach to achieving fault-tolerant data processing in launch vehicle avionics systems, is described. It offers a multi-lane building block method for designing real-time control systems which are capable of extremely reliable computations and which provide tolerance to a broad class of faults. MAFT is readily adaptable to computer processing applications in both expendable and reusable launch vehicles which carry critical or extremely high-cost payloads. MAFT is well suited for mission-critical processing functions, and can be implemented in a variety of data management system architectures, such as centralized, federated, or distributed configurations. MAFT provides a flexible, highly modular, easily maintained system, having low program life cycle costs
Keywords :
aerospace computer control; aerospace instrumentation; computer architecture; fault tolerant computing; multiprocessing systems; redundancy; distributed configuration; fault-tolerant data processing; federated configuration; flexible fault tolerant processor; launch vehicle avionics; life cycle costs; mission-critical processing functions; multi-lane building block; multicomputer architecture; real-time control systems; Aerospace electronics; Computer applications; Computer architecture; Control systems; Data processing; Design methodology; Fault tolerance; Fault tolerant systems; Real time systems; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location :
Virginia Beach, VA
Type :
conf
DOI :
10.1109/DASC.1990.111277
Filename :
111277
Link To Document :
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