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Research on utilization of part task spatial orientation information in the dynamic simulatorError and control efficiency analysis of pilots exposed to simulated pitch, roll, yaw, and altitude variations
Document ID
19660002906
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Abbott, B. A. (Bell Helicopter Co. Fort Worth, TX, United States)
Elam, C. B. (Bell Helicopter Co. Fort Worth, TX, United States)
Date Acquired
August 3, 2013
Publication Date
December 6, 1965
Subject Category
Biotechnology
Report/Patent Number
NASA-CR-68219
Report Number: NASA-CR-68219
Accession Number
66N12195
Funding Number(s)
CONTRACT_GRANT: NASW-439
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PILOT PERFORMANCE
CONTROL SIMULATOR
ERROR FUNCTION
STATISTICAL ANALYSIS

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