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A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath controlThe use of throttle control laws to provide adequate flying qualities for flight path control in the event of a total loss of conventional flight control surface use was evaluated. The results are based on a simulation evaluation by transport research pilots of a B-720 transport with visual display. Throttle augmentation control laws can provide flight path control capable of landing a transport-type aircraft with up to moderate levels of turbulence. The throttle augmentation mode dramatically improves the pilots' ability to control flight path for the approach and landing flight condition using only throttle modulation. For light turbulence, the average Cooper-Harper pilot rating improved from unacceptable to acceptable (a pilot rating improvement of 4.5) in going from manual to augmented control. The low frequency response characteristics of the engines require a considerably different piloting technique. The various techniques used by the pilot resulted in considerable scatter in data. Many pilots readily adapted to a good piloting technique while some had difficulty. A new viable approach is shown to provide independent means of redundancy of transport aircraft flight path control.
Document ID
19910019880
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gilyard, Glenn B.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Conley, Joseph L.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Le, Jeanette
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Burcham, Frank W., Jr.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-4324
NAS 1.15:4324
H-1741
Report Number: NASA-TM-4324
Report Number: NAS 1.15:4324
Report Number: H-1741
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE 27th Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 26, 1991
Accession Number
91N29194
Funding Number(s)
PROJECT: RTOP 505-64-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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