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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 flightpath 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 flightpath 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 flightpath 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 pilots resulted in considerable scatter in the data. Many pilots readily adapted to a good piloting technique while some has difficulty. The research demonstrates a new and viable approach to providing an independent means of redundancy or increasing the redundancy capability of transport aircraft flightpath control.
Document ID
19910059539
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 Flight Research Center Edwards, CA, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 91-2223
Accession Number
91A44162
Distribution Limits
Public
Copyright
Other

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