DocumentCode
280939
Title
Application of parallel processing in fault tolerant gas turbine engine control
Author
Thompson, H.A.
Author_Institution
Dowty Controls, Loudwater, UK
fYear
1990
fDate
33217
Firstpage
42370
Lastpage
42374
Abstract
Describes a demonstrator project investigating the use of parallel processing in fault-tolerant gas turbine engine control undertaken by Dowty Controls. The vehicle for this work is the Inmos transputer. As a multiple processor architecture is to be used there is inherent redundancy within the system and the aim of this work is to try and exploit this redundancy to introduce fault tolerance into the system while efficiently utilising the processing power available. A system simulator is under development which uses multiprocessor arrays. This simulator allows engine and controller simulations to be operated in closed-loop and allows different fault tolerant strategies and dynamic reconfiguration to be investigated. A user interface is used to alter system parameters during operation and for inducing failures in the system. Among the concepts being investigated are load balancing, dynamic scheduling, fault detection and recovery strategies
Keywords
computerised control; fault tolerant computing; gas turbines; parallel processing; transputers; Dowty Controls; Inmos transputer; aero-engines; dynamic scheduling; fault detection; fault tolerance; gas turbine engine control; load balancing; multiple processor architecture; parallel processing; recovery strategies; simulator; system simulator; user interface;
fLanguage
English
Publisher
iet
Conference_Titel
System Architectures for Failure Management, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
191418
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