An analog onboard monitoring system was installed on a YF-12 airplane as the first phase of a program to monitor the engine inlet and portions of the airplane's electrical and fuel management subsystems in flight. The system provided data which were considered to form a suitable base for diagnostic test logic and decision criteria for the rest of the program. The data were also adequate for the purpose of maintaining the engine inlet and identifying malfunctions within it. The investigation showed that the requirements of an onboard monitoring system should be considered during the original design of the system to be monitored.


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    Title :

    Flight study of a vehicle operational status and monitoring system


    Contributors:
    Love, J. E. (author) / Fox, W. J. (author) / Wicklund, E. J. (author)

    Publication date :

    1964-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Flight study of a vehicle operational status and monitoring system

    Love, James E. / Fox, William J. / Wicklund, Edward J. | TIBKAT | 1974


    Flight Study of a Vehicle Operational Status and Monitoring System

    J. E. Love / W. J. Fox / E. J. Wicklund | NTIS | 1964


    Flight Phase Status Monitor Study. Phase 2. Operational Simulation

    G. P. Boucek / B. L. Berson / L. G. Summers et al. | NTIS | 1985


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    AXELSON GUSTAF / JOHANSSON JONATHAN | European Patent Office | 2021

    Free access

    PEDAL SYSTEM FOR ROAD AND FLIGHT OPERATIONAL USE VEHICLE

    JOHANSSON JONATHAN / AXELSON GUSTAF | European Patent Office | 2022

    Free access