Method of recovering a flight critical computer after a...

G - Physics – 06 – F

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G06F 11/00 (2006.01) G06F 11/16 (2006.01) G06F 11/20 (2006.01)

Patent

CA 2440887

A method and apparatus for recovering a real-time computer system by running (steps 33-34) multiple versions of an operational program including multiple data partitions are described wherein each of the multiple data partitions is associated with one version of the operational program and wherein one of the versions of the operational program is a "controller" program and the other versions are "identity observer" programs. When the controller memory partition is damaged (step 35) the damaged memory is overwritten (step 37) with fault-free data.

L'invention concerne un procédé et un appareil permettant de récupérer un système informatique en temps réel par exécution (étapes 33-34) de plusieurs versions d'un programme opérationnel comprenant plusieurs partitions de données, chaque partition de données étant associée à une version du programme opérationnel et une des versions du système opérationnel étant un programme d'"unité de commande" et les autres versions étant des programmes d'"observateur d'identité". Quand la partition de mémoire de l'unité de commande est endommagée (étape 35), la mémoire endommagée est écrasée (étape 37) au moyen de données exemptes d'erreur.

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