ELECTRONIC COMPUTER FOR CARRYING OUT AT LEAST ONE CRITICAL FUNCTION, ASSOCIATED ELECTRONIC DEVICE, METHOD AND COMPUTER PROGRAM

ELECTRONIC COMPUTER FOR CARRYING OUT AT LEAST ONE CRITICAL FUNCTION, ASSOCIATED ELECTRONIC DEVICE, METHOD AND COMPUTER PROGRAM

A programmable electronic computer embedded in an avionics environment on board an aircraft for implementing at least one critical function and associated electronic device, method and computer program are disclosed. In one aspect, the electronic computer includes at least one control module configu...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: RECULEAU, Jean-Christophe, FUMEY, Marc, CLEMENT, Frederick, CADOTTE, Patrick, BOSSON, Joël
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
CALCULATING
COMPUTING
CONTROL OR REGULATING SYSTEMS IN GENERAL
CONTROLLING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
FUNCTIONAL ELEMENTS OF SUCH SYSTEMS
MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS
PHYSICS
REGULATING
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Beschreibung
Zusammenfassung:A programmable electronic computer embedded in an avionics environment on board an aircraft for implementing at least one critical function and associated electronic device, method and computer program are disclosed. In one aspect, the electronic computer includes at least one control module configured to implement a respective critical function and configured to deliver at least one output data item associated with the critical function, and at least one monitoring module of a control module of another electronic computer. Each monitoring module configured to implement the same respective critical function as the one implemented by the monitored control module.