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Effect of lead-aircraft ground-speed on self-spacing performance using a cockpit display of traffic informationA simulator investigation was conducted to determine the effect of the lead-aircraft ground-speed quantization level on self-spacing performance using a Cockpit Display of Traffic Information (CDTI). The study utilized a simulator employing cathode-ray tubes for the primary flight and navigation displays and highly augmented flight control modes. The pilot's task was to follow, and self-space on, a lead aircraft which was performing an idle-thrust profile descent to an instrument landing system (ILS) approach and landing. The spacing requirement was specified in terms of both a minimum distance and a time interval. The results indicate that the ground-speed quantization level, lead-aircraft scenario, and pilot technique had a significant effect on self-spacing performance. However, the ground-speed quantization level only had a significant effect on the performance when the lead aircraft flew a fast final approach.
Document ID
19830027757
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Kelly, J. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Instrumentation
Report/Patent Number
NAS 1.60:2194
L-15402
NASA-TP-2194
Report Number: NAS 1.60:2194
Report Number: L-15402
Report Number: NASA-TP-2194
Accession Number
83N36028
Funding Number(s)
PROJECT: RTOP 505-35-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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