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Piloted Simulation of Various Synthetic Vision Systems Terrain Portrayal and Guidance Symbology Concepts for Low Altitude En-Route ScenarioIn support of the NASA Aviation Safety Program's Synthetic Vision Systems Project, a series of piloted simulations were conducted to explore and quantify the relationship between candidate Terrain Portrayal Concepts and Guidance Symbology Concepts, specific to General Aviation. The experiment scenario was based on a low altitude en route flight in Instrument Metrological Conditions in the central mountains of Alaska. A total of 18 general aviation pilots, with three levels of pilot experience, evaluated a test matrix of four terrain portrayal concepts and six guidance symbology concepts. Quantitative measures included various pilot/aircraft performance data, flight technical errors and flight control inputs. The qualitative measures included pilot comments and pilot responses to the structured questionnaires such as perceived workload, subjective situation awareness, pilot preferences, and the rare event recognition. There were statistically significant effects found from guidance symbology concepts and terrain portrayal concepts but no significant interactions between them. Lower flight technical errors and increased situation awareness were achieved using Synthetic Vision Systems displays, as compared to the baseline Pitch/Roll Flight Director and Blue Sky Brown Ground combination. Overall, those guidance symbology concepts that have both path based guidance cue and tunnel display performed better than the other guidance concepts.
Document ID
20080017510
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Takallu, M. A.
(Lockheed Martin Corp. Hampton, VA, United States)
Glaab, L. J.
(NASA Langley Research Center Hampton, VA, United States)
Hughes, M. F.
(NASA Langley Research Center Hampton, VA, United States)
Wong, D. T.
(NASA Johnson Space Center Houston, TX, United States)
Bartolone, A. P.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2008
Subject Category
Aeronautics (General)
Report/Patent Number
L-19329
NASA/TP-2008-215127
Report Number: L-19329
Report Number: NASA/TP-2008-215127
Funding Number(s)
WBS: WBS 609866.02.07.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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