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Allowable response delay for large aircraftThe degree of permissible time delay in an airliner flight control system is presently sought by means of a pilot-in-the-loop moving base flight simulator, assuming the characteristics of an advanced L-1011 aircraft variant. Test pilots and engineers from the U.S. Navy, the airliner manufacturer, and NASA Langley were used in a task which encompassed approach and landing after recovery from offsets in localizer and glide slope, during calm, turbulent, and cross-wind conditions. The data obtained in the course of 279 runs included statistics on pilot workload and performance as well as pilot opinion. Preliminary results indicate that requirements for a 0.1-sec maximum delay in aircraft response are excessively conservative for large aircraft, where an offset landing maneuver is the critical design task. Lateral axis delays appear to be more critical than longitudinal ones.
Document ID
19840060666
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meyer, R. T.
(Lockheed-Georgia Co. Marietta, GA, United States)
Tingas, S. A.
(Lockheed-Georgia Co. Marietta, GA, United States)
Grantham, W. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 84-1917
Accession Number
84A43453
Distribution Limits
Public
Copyright
Other

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