An aircraft flight control system comprises a set of primary computers, each configured to compute a flight order dependent on at least one aircraft flight parameter and intended for an aircraft control surface actuator remote controller. Each computer participates in command mode within a first virtual command/monitor pair and in monitor mode within a second virtual command/monitor pair. Each computer determines a consolidated flight parameter value as a function of a flight parameter value acquired by this computer and of flight parameter values received from the other computers, using a consolidation algorithm commonly used by all primary computers to each determine a consolidated flight parameter value, and compute the intended flight order for the remote controller as a function of the consolidated flight parameter value, according to a unique computation whose result is used by the computer both when acting in command mode and when acting in monitor mode.


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    Titel :

    Aircraft flight control system


    Beteiligte:
    BROT PATRICE (Autor:in)

    Erscheinungsdatum :

    09.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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