Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. Topics discussed include: system description, F100 engine tests, effects of inlet distortion on static pressure probe, flight tests, digital electronic engine control fault detection and accommodation flight evaluation, flight evaluation of a hydromechanical backup control, augmentor transient capability of an F100 engine, investigation of nozzle instability, real time in flight thrust calculation, and control technology for future aircraft propulsion systems. It is shown that the DEEC system is a powerful and flexible controller for the F100 engine.


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    Title :

    Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane


    Publication date :

    1984-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English