Add to ORKGThe standard hydromechanical control system of a turbojet engine was replaced with a digital control system that implemented the same control laws. A detailed discussion of the digital control system in use with the engine is presented. The engine was operated in a sea-level test stand. The effects of control update interval are defined, and a method for extending this interval by using digital compensation is discussed
Correlation has been established between transient engine and control data obtained experimentally a...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
Development of digital system for on-line control of airbreathing propulsion system
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
The design and evaluation are described of a digital turbojet engine control which is capable of sen...
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 self-learning, sensor fail-operational, control system for the TF30-P-3 afterburning turbofan engi...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The standard hydromechanical control modes for TF30-P-3 engine were implemented on a digital process...
The digital electronic engine control (DEEC) is a full-authority digital engine control developed fo...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The control of an airbreathing turbojet engine by an onboard digital computer is studied. The approa...
Correlation has been established between transient engine and control data obtained experimentally a...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
Development of digital system for on-line control of airbreathing propulsion system
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
The design and evaluation are described of a digital turbojet engine control which is capable of sen...
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 self-learning, sensor fail-operational, control system for the TF30-P-3 afterburning turbofan engi...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The standard hydromechanical control modes for TF30-P-3 engine were implemented on a digital process...
The digital electronic engine control (DEEC) is a full-authority digital engine control developed fo...
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
The control of an airbreathing turbojet engine by an onboard digital computer is studied. The approa...
Correlation has been established between transient engine and control data obtained experimentally a...
Full authority digital electronic engine controls (DEECs) were studied, developed, and ground tested...
Development of digital system for on-line control of airbreathing propulsion system