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Evaluation of Fused Synthetic and Enhanced Vision Display Concepts for Low-Visibility Approach and LandingNASA is developing revolutionary crew-vehicle interface technologies that strive to proactively overcome aircraft safety barriers that would otherwise constrain the full realization of the next generation air transportation system. A piloted simulation experiment was conducted to evaluate the complementary use of Synthetic and Enhanced Vision technologies. Specific focus was placed on new techniques for integration and/or fusion of Enhanced and Synthetic Vision and its impact within a two-crew flight deck during low-visibility approach and landing operations. Overall, the experimental data showed that significant improvements in situation awareness, without concomitant increases in workload and display clutter, could be provided by the integration and/or fusion of synthetic and enhanced vision technologies for the pilot-flying and the pilot-not-flying. Improvements in lateral path control performance were realized when the Head-Up Display concepts included a tunnel, independent of the imagery (enhanced vision or fusion of enhanced and synthetic vision) presented with it. During non-normal operations, the ability of the crew to handle substantial navigational errors and runway incursions were neither improved nor adversely impacted by the display concepts. The addition of Enhanced Vision may not, of itself, provide an improvement in runway incursion detection without being specifically tailored for this application.
Document ID
20090019723
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Bailey, Randall E.
(NASA Langley Research Center Hampton, VA, United States)
Kramer, Lynda J.
(NASA Langley Research Center Hampton, VA, United States)
Prinzel, Lawrence J., III
(NASA Langley Research Center Hampton, VA, United States)
Wilz, Susan J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
April 1, 2009
Subject Category
Air Transportation And Safety
Report/Patent Number
LF99-7406
L-19504
NASA/TP-2009-215707
Funding Number(s)
WBS: WBS 609866.02.07.07.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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