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Emergency Flight Control Using Only Engine Thrust and Lateral Center-of-Gravity Offset: A First LookNormally, the damage that results in a total loss of the primary flight controls of a jet transport airplane, including all engines on one side, would be catastrophic. In response, NASA Dryden has conceived an emergency flight control system that uses only the thrust of a wing-mounted engine along with a lateral center-of-gravity (CGY) offset from fuel transfer. Initial analysis and simulation studies indicate that such a system works, and recent high-fidelity simulation tests on the MD-11 and B-747 suggest that the system provides enough control for a survivable landing. This paper discusses principles of flight control using only a wing engine thrust and CGY offset, along with the amount of CGY offset capability of some transport airplanes. The paper also presents simulation results of the throttle-only control capability and closed-loop control of ground track using computer-controlled thrust.
Document ID
19970022980
Acquisition Source
Armstrong Flight Research Center
Document Type
Reprint (Version printed in journal)
Authors
Burcham, Frank W., Jr.
(NASA Dryden Flight Research Center Edwards, CA United States)
Burken, John
(NASA Dryden Flight Research Center Edwards, CA United States)
Maine, Trindel A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Bull, John
(Caelum Research Corp. Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
H-2176
NAS 1.15:4798
NASA-TM-4798
AIAA Paper 97-3189
Report Number: H-2176
Report Number: NAS 1.15:4798
Report Number: NASA-TM-4798
Report Number: AIAA Paper 97-3189
Meeting Information
Meeting: Propulsion
Location: Seattle, WA
Country: United States
Start Date: July 6, 1997
End Date: July 9, 1997
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers
Accession Number
97N23391
Funding Number(s)
PROJECT: RTOP 522-15-34-00-39-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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