A flight control system (10) for an aircraft comprises a flight control computer system (12), which is connected via an electronic or optoelectronic bus system (22) with a plurality of bus nodes (14, 16, 18, 20), which each are configured to at least one of controlling an associated aircraft device based on command messages received from the flight control computer system via the bus system and sending information messages to the flight control computer system via the bus system. According to one aspect of the disclosure, the electronic or optoelectronic bus system is a redundant electronic or optoelectronic bus system (22) comprising plural independent bus sub-systems (22a, 22b), wherein each bus node is configured to communicate with the flight control computer system (12) via two different bus sub-systems (22a, 22b) of the plural independent bus sub-systems, wherein each bus node further is configured to communicate with the flight control computer system on basis of an associated predetermined bus communication protocol via a first bus sub-system (22a) of the respective two different bus sub-systems and on basis of an associated predetermined bus communication protocol via a second bus sub-system (22b) of the respective two different bus sub-systems.


    Access

    Download


    Export, share and cite



    Title :

    FAULT TOLERANT AIRCRAFT FLIGHT CONTROL SYSTEM


    Additional title:

    FEHLERTOLERANTES FLUGZEUGFLUGSTEUERUNGSSYSTEM
    SYSTÈME DE COMMANDE DE VOL D'AÉRONEF TOLÉRANT AUX PANNES



    Publication date :

    2024-04-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr



    FAULT TOLERANT AIRCRAFT FLIGHT CONTROL SYSTEM

    TELES FERREIRA JOÃO FILIPE / RIBAS GABRIEL OLIVEIRA | European Patent Office | 2022

    Free access

    Fault-tolerant aircraft flight control system and aircraft preferably having such aircraft flight control system

    TELES FERREIRA JORGE FILIPE / RIBAS GIDEON O | European Patent Office | 2022

    Free access

    FAULT TOLERANT AIRCRAFT FLIGHT CONTROL SYSTEM AND AIRCRAFT PREFERABLY HAVING SUCH AN AIRCRAFT FLIGHT CONTROL SYSTEM

    TELES FERREIRA JOÃO FILIPE / RIBAS GABRIEL OLIVEIRA | European Patent Office | 2022

    Free access

    Fault Tolerant Flight Control

    Meir Pachter / Yih-Shiun Huang | AIAA | 2003


    Electric aircraft modeling and fault-tolerant flight control method for aircraft body damage

    ZHANG LEI / XIONG XUHAI / ZHOU WENYA et al. | European Patent Office | 2023

    Free access