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A simulation investigation of cockpit display of aircraft traffic during curved, descending, decelerating approachesThe results of a simulation experiment involving the evaluation of cockpit display of aircraft traffic information are presented. The experiment was conducted using taped time dependent, noninteractive traffic in an approach to landing situation and two levels of pilot control models: 3-D automatic and computer augmented control. The tests involved two cases: the simulation aircraft flew approach paths which (1) followed another aircraft in between two other aircraft, and (2) merged between two other aircraft. Speed control via manual throttles was used in all tests (path stretching was not allowed for maintaining separation between aircraft). The approaches were conducted while the simulation aircraft was conducting a curved, descending, decelerating approach to landing. Performance data sets were examined, and subjective opinions regarding workload were gathered. Traffic positioning was varied to further evaluate the test subjects' monitoring performance.
Document ID
19790017881
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Steinmetz, G. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-80098
Report Number: NASA-TM-80098
Accession Number
79N26052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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