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.


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    Title :

    Development of failure-correcting flight control system


    Additional title:

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


    Contributors:
    Neebe, F.C. (author)

    Conference:

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



    Publication date :

    1965


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Development of Failure-Correcting Flight Control System

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


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