Development And Flight Test Of An Emergency Flight Control System Using Only Engine Thrust On An Md 11 Transport Airplane
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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
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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
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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...
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.
Fault Tolerant Flight Control
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Author : Christopher Edwards
language : en
Publisher: Springer
Release Date : 2010-04-18
Fault Tolerant Flight Control written by Christopher Edwards and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2010-04-18 with Technology & Engineering categories.
Written by leading experts in the field, this book provides the state-of-the-art in terms of fault tolerant control applicable to civil aircraft. The book consists of five parts and includes online material.
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...
Advances In Aerospace Guidance Navigation And Control
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Author : Florian Holzapfel
language : en
Publisher: Springer Science & Business Media
Release Date : 2011-03-15
Advances In Aerospace Guidance Navigation And Control written by Florian Holzapfel and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-03-15 with Technology & Engineering categories.
Over the last few decades, both the aeronautics and space disciplines have greatly influenced advances in controls, sensors, data fusion and navigation. Many of those achievements that made the word “aerospace” synonymous with “high–tech” were enabled by innovations in guidance, navigation and control. Europe has seen a strong trans-national consolidation process in aerospace over the last few decades. Most of the visible products, like commercial aircraft, fighters, helicopters, satellites, launchers or missiles, are not made by a single country – they are the fruits of cooperation. No European country by itself hosts a specialized guidance, navigation and controls community large enough to cover the whole spectrum of disciplines. However, on a European scale, mutual exchange of ideas, concepts and solutions is enriching for all. The 1st CEAS Specialist Conference on Guidance, Navigation and Control is an attempt to bring this community together. This book is a selection of papers presented at the conference. All submitted papers have gone through a formal review process in compliance with good journal practices. The best papers have been recommended by the reviewers to be published in this book.
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.
The Power For Flight
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Author : Jeremy R. Kinney
language : en
Publisher: Government Printing Office
Release Date : 2018-02-15
The Power For Flight written by Jeremy R. Kinney and has been published by Government Printing Office this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-02-15 with Science categories.
The NACA and aircraft propulsion, 1915-1958 -- NASA gets to work, 1958-1975 -- The shift toward commercial aviation, 1966-1975 -- The quest for propulsive efficiency, 1976-1989 -- Propulsion control enters the computer era, 1976-1998 -- Transiting to a new century, 1990-2008 -- Toward the future
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
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 and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Emergencies 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.