A system for controlling and monitoring pieces of equipment of an aircraft, each piece of equipment being able to be switched between two logic activation state values, comprising a man-machine interface, a module for configuration of a functional activation state of a function able to be performed on at least pieces of equipment of a system of the aircraft, the functional activation state being configurable between an active state and an inactive state, the configuration module being adapted for detecting an action of selection of a functional activation state of the function by an operator, and a control and monitoring module configured for determining a logic activation state of each of the pieces of equipment of the system, so that, when each of the pieces of equipment is in the determined logic activation state, the function is in the selected functional activation state.
SYSTEME ET PROCEDE DE COMMANDE ET DE SURVEILLANCE D'EQUIPEMENTS D'UN AERONEF
2018-06-15
Patent
Electronic Resource
French
IPC: | G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
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