The design and evaluation are described of a digital turbojet engine control which is capable of sensing catastrophic failures in either the engine rotor speed or the compressor discharge static-pressure signal and is capable of switching control modes to maintain near normal operation. The control program was developed for and tested on a turbojet engine located in a sea-level test stand. The control program is also capable of acquiring all the data that are necessary for the fail-operational control to function
The objective of the Advanced Detection, Isolation, and Accommodation (ADIA) Program is to improve t...
The objective of the advanced detection, isolation, and accommodation (ADIA) program is to improve t...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
A self-learning, sensor fail-operational, control system for the TF30-P-3 afterburning turbofan engi...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...
The standard hydromechanical control system of a turbojet engine was replaced with a digital control...
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
An algorithm was developed which detects, isolates, and accommodates sensor failures using analytica...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
A hypothetical turbofan engine simplified simulation with a multivariable control and sensor failure...
Analytical redundant sensor failure detection, isolation and accommodation techniques for gas turbin...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...
A digital computer control and abort system which is used at NASA-Lewis research center is described...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
The objective of the Advanced Detection, Isolation, and Accommodation (ADIA) Program is to improve t...
The objective of the advanced detection, isolation, and accommodation (ADIA) program is to improve t...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...
A self-learning, sensor fail-operational, control system for the TF30-P-3 afterburning turbofan engi...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...
The standard hydromechanical control system of a turbojet engine was replaced with a digital control...
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
An algorithm was developed which detects, isolates, and accommodates sensor failures using analytica...
A digital electronic engine control (DEEC) was developed for use on the F100-PW-100 turbofan engine....
The capabilities and performance of various fault detection and accommodation (FDA) schemes in exist...
A hypothetical turbofan engine simplified simulation with a multivariable control and sensor failure...
Analytical redundant sensor failure detection, isolation and accommodation techniques for gas turbin...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...
A digital computer control and abort system which is used at NASA-Lewis research center is described...
Flight evaluation in an F-15 aircraft by digital electronic engine control (DEEC) was investigated. ...
The objective of the Advanced Detection, Isolation, and Accommodation (ADIA) Program is to improve t...
The objective of the advanced detection, isolation, and accommodation (ADIA) program is to improve t...
Substantial benefits of a full authority digital electronic engine control on an air breathing engin...