The digital electronic engine control (DEEC) is a full-authority digital engine control developed for the F100-PW-100 turbofan engine which was flight tested on an F-15 aircraft. The DEEC hardware and software throughout the F-15 flight envelope was evaluated. Real-time data reduction and data display systems were implemented. New test techniques and stronger coordination between the propulsion test engineer and pilot were developed which produced efficient use of test time, reduced pilot work load, and greatly improved quality data. The engine pressure ratio (EPR) control mode is demonstrated. It is found that the nonaugmented throttle transients and engine performance are satisfactory
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
A brief description of the NASA F-15 research aircraft propulsion system is given. The F-15 is power...
The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the i...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
The third phase of a flight evaluation of a digital electronic engine control system in an F-15 has ...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft ...
The airstart performance of the F100 engine equipped with a digital electronic engine control (DEEC)...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
An F100 augmented turbofan engine equipped with digital electronic engine control (DEEC) system was ...
The highly integrated digital electronic control (HIDEC) program will integrate the propulsion and f...
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
A brief description of the NASA F-15 research aircraft propulsion system is given. The F-15 is power...
The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the i...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
The third phase of a flight evaluation of a digital electronic engine control system in an F-15 has ...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft ...
The airstart performance of the F100 engine equipped with a digital electronic engine control (DEEC)...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
An F100 augmented turbofan engine equipped with digital electronic engine control (DEEC) system was ...
The highly integrated digital electronic control (HIDEC) program will integrate the propulsion and f...
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
A brief description of the NASA F-15 research aircraft propulsion system is given. The F-15 is power...
The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the i...