Report discusses design and testing of redundant control system for F-8 digital fly-by-wire airplane. Outstanding feature of system is fault-tolerant software (REBUS) residing in primary digital computers. Transition to operation on backup software smooth.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fault-Tolerant Software For Flight Control


    Contributors:

    Published in:

    Publication date :

    1988-07-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Fault Tolerant Flight Control

    Meir Pachter / Yih-Shiun Huang | AIAA | 2003


    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

    TELES FERREIRA JOÃO FILIPE / RIBAS GABRIEL OLIVEIRA | European Patent Office | 2024

    Free access