[PDF] Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane - eBooks Review

Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane


Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane
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Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane


Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane
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Author : Frank W. Burcham (Jr.)
language : en
Publisher:
Release Date : 1996

Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane written by Frank W. Burcham (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.




Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane


Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-02

Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-02 with categories.


An emergency flight control system using only engine thrust, called Propulsion-Controlled Aircraft (PCA), has been developed and flight tested on an MD-11 airplane. In this thrust-only control system, pilot flight path and track commands and aircraft feedback parameters are used to control the throttles. The PCA system was installed on the MD-11 airplane using software modifications to existing computers. Flight test results show that the PCA system can be used to fly to an airport and safely land a transport airplane with an inoperative flight control system. In up-and-away operation, the PCA system served as an acceptable autopilot capable of extended flight over a range of speeds and altitudes. The PCA approaches, go-arounds, and three landings without the use of any non-nal flight controls have been demonstrated, including instrument landing system-coupled hands-off landings. The PCA operation was used to recover from an upset condition. In addition, PCA was tested at altitude with all three hydraulic systems turned off. This paper reviews the principles of throttles-only flight control; describes the MD-11 airplane and systems; and discusses PCA system development, operation, flight testing, and pilot comments. Burcham, Frank W., Jr. and Maine, Trindel A. and Burken, John J. and Pappas, Drew Armstrong Flight Research Center RTOP 505-68-10...



Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane


Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane
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Author : Frank W. Burcham (Jr.)
language : en
Publisher:
Release Date : 1997

Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane written by Frank W. Burcham (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with categories.




Using Engine Thrust For Emergency Flight Control Md 11 And B 747 Results


Using Engine Thrust For Emergency Flight Control Md 11 And B 747 Results
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Author : Frank W. Burcham (Jr.)
language : en
Publisher:
Release Date : 1998

Using Engine Thrust For Emergency Flight Control Md 11 And B 747 Results written by Frank W. Burcham (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.




Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane


Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-08

Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-08 with categories.


An emergency flight control system that uses only engine thrust, called the propulsion-controlled aircraft (PCA) system, was developed and flight tested on an MD-11 airplane. The PCA system is a thrust-only control system, which augments pilot flightpath and track commands with aircraft feedback parameters to control engine thrust. The PCA system was implemented on the MD-11 airplane using only software modifications to existing computers. Results of a 25-hr flight test show that the PCA system can be used to fly to an airport and safely land a transport airplane with an inoperative flight control system. In up-and-away operation, the PCA system served as an acceptable autopilot capable of extended flight over a range of speeds, altitudes, and configurations. PCA approaches, go-arounds, and three landings without the use of any normal flight controls were demonstrated, including ILS-coupled hands-off landings. PCA operation was used to recover from an upset condition. The PCA system was also tested at altitude with all three hydraulic systems turned off. This paper reviews the principles of throttles-only flight control, a history of accidents or incidents in which some or all flight controls were lost, the MD-11 airplane and its systems, PCA system development, operation, flight testing, and pilot comments. Burcham, Frank W., Jr. and Burken, John J. and Maine, Trindel A. and Fullerton, C. Gordon Armstrong Flight Research Center...



32nd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit


32nd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit
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Author :
language : en
Publisher:
Release Date : 1996

32nd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Airplanes categories.




Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane


Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane
DOWNLOAD
Author : Frank W. Burcham
language : en
Publisher:
Release Date : 1996

Development And Flight Test Of An Augmented Thrust Only Flight Control System On An Md 11 Transport Airplane written by Frank W. Burcham and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.


An emergency flight control system using only engine thrust, called Propulsion-Controlled Aircraft (PCA), has been developed and flight tested on an MD-11 airplane. In this thrust-only control system, pilot flightpath and track commands and aircraft feedback parameters are used to control the throttles. The PCA system was installed on the MD-11 airplane using software modifications to existing computers. Flight test results show that the PCA system can be used to fly to an airport and safely land a transport airplane with an inoperative flight control system. In up-and-away operation, the PCA system served as an acceptable autopilot capable of extended flight over a range of speeds and altitudes. The PCA approaches, go-arounds, and three landings without the use of any normal flight controls have been demonstrated, including instrument landing system-coupled hands-off landings. The PCA operation was used to recover from an upset condition. In addition, PCA was tested at altitude with all three hydraulic systems turned off. This paper reviews the principles of throttles-only flight control; describes the MD-11 airplane and systems; and discusses PCA system development, operation, flight testing, and pilot comments.



Development And Flight Evaluation Of An Emergency Digital Flight Control System Using Only Engine Thrust On An F 15 Airplane


Development And Flight Evaluation Of An Emergency Digital Flight Control System Using Only Engine Thrust On An F 15 Airplane
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Author : Frank W. Burcham (Jr.)
language : en
Publisher:
Release Date : 1996

Development And Flight Evaluation Of An Emergency Digital Flight Control System Using Only Engine Thrust On An F 15 Airplane written by Frank W. Burcham (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.




33rd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit


33rd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit
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Author :
language : en
Publisher:
Release Date : 1997

33rd Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Airplanes categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1991

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.