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The Primary Flight Display and Its Pathway Guidance: Workload, Performance, and Situation AwarenessIn two experiments carried out in a high fidelity general aviation flight simulator, 42 instrument rated pilots flew a pathway-in-the-sky (tunnel) display through a series of multi-leg curved stepdown approaches through mountainous terrain. Both experiments examined how properties of the tunnel influenced flight path tracking performance, traffic awareness, terrain awareness and workload (assessed both by subjective and secondary task performance measures). Experiment 1, flown in simulated VMC, compared high and low intensity tunnels, with a less cluttered follow-me-airplane (FMA). The results revealed that both tunnels supported better flight path tracking than the FMA, because of the availability of more preview information. Increasing tunnel intensity, while reducing subjective workload, had no benefit on tracking, and degraded traffic detection performance. In Experiment 2, flown mostly in IMC, the low intensity tunnel was flown with a large (10 inch x 8 inch) and small (8 inch x 6.5 inch) display, representing a geometric field of view (GFOV) of either 30 degrees or 60 degrees. Most measures of flight path tracking performance favored the smaller display, and particularly the 60 degree GFOV, which presented a smaller appearing tunnel, and a wider range of terrain depiction. The larger GFOV also supported better terrain awareness, and yielded a lower secondary task assessment of workload. In both experiments, the final landing approach was terminated by a runway obstruction, and the tunnel guided pilots on a missed approach. In nearly all cases, pilots failed to notice an air hazard that lay in the missed approach path, but was only depicted in the outside view.
Document ID
20040000685
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Wickens, Christopher D.
(Illinois Univ. at Urbana-Champaign Savoy, IL, United States)
Alexander, Amy L.
(Illinois Univ. at Urbana-Champaign Savoy, IL, United States)
Hardy, Thomas J.
(Illinois Univ. at Urbana-Champaign Savoy, IL, United States)
Date Acquired
August 21, 2013
Publication Date
February 1, 2003
Subject Category
Avionics And Aircraft Instrumentation
Report/Patent Number
AHFD-03-2/NASA-03-1
Funding Number(s)
CONTRACT_GRANT: NAG1-02071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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