Aircraft fly-by-wire systems and related vehicle electrical systems are provided. A vehicle electrical system includes a bus arrangement having a plurality of buses, a first control module coupled to a first subset of the buses, a second control module coupled to a second subset of the buses, and a third control module coupled to a third subset of the buses. The first subset includes a first bus, a second bus, a third bus, and a fourth bus, the second subset includes the third bus, the fourth bus, a fifth bus, and a sixth bus, and the third subset includes the first bus, the second bus, the fifth bus and the sixth bus.


    Access

    Download


    Export, share and cite



    Title :

    Redundant fly-by-wire systems with fault resiliency


    Contributors:

    Publication date :

    2022-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Redundant fly-by-wire systems with fault resiliency

    WILKENS DEAN | European Patent Office | 2021

    Free access

    REDUNDANT FLY-BY-WIRE SYSTEMS WITH FAULT RESILIENCY

    KEIR MICHAEL | European Patent Office | 2022

    Free access

    REDUNDANT FLY-BY-WIRE SYSTEMS WITH FAULT RESILIENCY

    KEIR MICHAEL | European Patent Office | 2021

    Free access

    REDUNDANT FLY-BY-WIRE SYSTEMS WITH FAULT RESILIENCY

    WILKENS DEAN | European Patent Office | 2020

    Free access

    Threats to Resiliency of Redundant Systems Due to Destructive SEE

    Raymond L Ladbury / Michael Bay / Jeffrey J Zinchuk | NTRS | 2020