A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An overview of the flight program is presented. The roles of the participating parties, the system, and the flight program objectives are described. The test program approach is discussed, and the engine performance benefits are summarized. A description of the follow-on programs is included
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
The digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft ...
The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flig...
The digital electronic engine control (DEEC) is a full-authority digital engine control developed fo...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
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 highly integrated digital electronic control (HIDEC) program will integrate the propulsion and f...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the i...
The airstart performance of the F100 engine equipped with a digital electronic engine control (DEEC)...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
The NASA highly integrated digital electronic control (HIDEC) program is structured to conduct fligh...
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
The digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft ...
The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flig...
The digital electronic engine control (DEEC) is a full-authority digital engine control developed fo...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
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 highly integrated digital electronic control (HIDEC) program will integrate the propulsion and f...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the i...
The airstart performance of the F100 engine equipped with a digital electronic engine control (DEEC)...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
The NASA highly integrated digital electronic control (HIDEC) program is structured to conduct fligh...
Two builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine...
The digital electronic engine control (DEEC) system installed on an F100 engine in an F-15 aircraft ...
The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flig...