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Simulator study of conventional general aviation instrument displays in path-following tasks with emphasis on pilot-induced oscillationsA study of the use of conventional general aviation instruments by general aviation pilots in a six degree of freedom, fixed base simulator was conducted. The tasks performed were tracking a VOR radial and making an ILS approach to landing. A special feature of the tests was that the sensitivity of the displacement indicating instruments (the RMI, CDI, and HSI) was kept constant at values corresponding to 5 n. mi. and 1.25 n. mi. from the station. Both statistical and pilot model analyses of the data were made. The results show that performance in path following improved with increases in display sensitivity up to the highest sensitivity tested. At this maximum test sensitivity, which corresponds to the sensitivity existing at 1.25 n. mi. for the ILS glide slope transmitter, tracking accuracy was no better than it was at 5 n. mi. from the station and the pilot aircraft system exhibited a marked reduction in damping. In some cases, a pilot induced, long period unstable oscillation occurred.
Document ID
19810006482
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Adams, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Instrumentation
Report/Patent Number
L-13785
NASA-TP-1776
Report Number: L-13785
Report Number: NASA-TP-1776
Accession Number
81N14997
Funding Number(s)
PROJECT: RTOP 505-41-73-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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