Add to ORKGFlight weight digital computers are being used today to carry out many of the propulsion system control functions previously delegated exclusively to hydromechanical controllers. An operational digital computer facility for propulsion control mode studies has been used successfully in several experimental programs. This paper describes the system and some of the results concerned with engine control, inlet control, and inlet engine integrated control. Analytical designs for the digital propulsion control modes include both classical and modern/optimal techniques
The major objective was to define the exact role of an onboard spacecraft computer in the control of...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Research programs have demonstrated that digital electronic controls are more suitable for advanced ...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
Development of digital system for on-line control of airbreathing propulsion system
A digitally implemented integrated inlet/engine control system was developed and tested on a mixed c...
The standard hydromechanical control system of a turbojet engine was replaced with a digital control...
A digital computer control and abort system which is used at NASA-Lewis research center is described...
Digital integrated control systems are studied. Such systems allow minimization of undesirable inter...
Technological developments necessary for the implementation of advanced digital control concepts for...
The results of studies which were undertaken to contribute to the design of digital flight control s...
The development of digital controls for turbojet and turbofan engines is presented by the use of rea...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
The design and evaluation are described of a digital turbojet engine control which is capable of sen...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The major objective was to define the exact role of an onboard spacecraft computer in the control of...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Research programs have demonstrated that digital electronic controls are more suitable for advanced ...
The need for a more sophisticated engine control system is discussed. The improvements in better thr...
Development of digital system for on-line control of airbreathing propulsion system
A digitally implemented integrated inlet/engine control system was developed and tested on a mixed c...
The standard hydromechanical control system of a turbojet engine was replaced with a digital control...
A digital computer control and abort system which is used at NASA-Lewis research center is described...
Digital integrated control systems are studied. Such systems allow minimization of undesirable inter...
Technological developments necessary for the implementation of advanced digital control concepts for...
The results of studies which were undertaken to contribute to the design of digital flight control s...
The development of digital controls for turbojet and turbofan engines is presented by the use of rea...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
The design and evaluation are described of a digital turbojet engine control which is capable of sen...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The major objective was to define the exact role of an onboard spacecraft computer in the control of...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
Research programs have demonstrated that digital electronic controls are more suitable for advanced ...