General Electric Co designed, fabricated and evaluated bread-board model of failure-correcting, rate-maneuvering flight control proving feasibility of triple-redundant majority logic voting using HYDAPT (hybrid digital-analog pulse time) concept; following techniques developed or used in General Electric programs or contracts are described -- triple redundancy with majority logic voting, hammock networks, dual actuators with model and automatic fault removal and failure-correcting redundant power supplies.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Development of failure-correcting flight control system


    Weitere Titelangaben:

    SAE-NASA -- Aerospace Vehicle Flight Control Conference -- Proc


    Beteiligte:
    Neebe, F.C. (Autor:in)

    Kongress:

    Proceedings of the SAE-NASA Aerospace Vehicle Flight Control Conference ; 1965 Control equipment



    Erscheinungsdatum :

    1965


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Development of Failure-Correcting Flight Control System

    Neebe, F. C. | SAE Technical Papers | 1965


    FLIGHT ROUTE LEARNING DEVICE, CONDITION CORRECTING DEVICE AND FLIGHT ROUTE DETERMINING DEVICE

    IWAKURA TAKASHI / ISHIDA TAKAYUKI | Europäisches Patentamt | 2021

    Freier Zugriff

    Method for semi-automatically correcting flight next-day plan data of flight

    SONG YU / YUAN YONG / LIU TAO et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Flight System Sensor Failure

    Filburn, Thomas | Springer Verlag | 2019


    FLIGHT ROUTE LEARNING DEVICE, CONDITION CORRECTING DEVICE AND FLIGHT ROUTE DECIDING DEVICE

    IWAKURA TAKASHI / ISHIDA TAKAYUKI | Europäisches Patentamt | 2024

    Freier Zugriff