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A STUDY OF A PILOT'S ABILITY TO CONTROL DURING SIMULATED STABILITY AUGMENTATION SYSTEM FAILURESPilots ability to control during simulated stability augmenter failures
Document ID
19630000307
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Sadoff, M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1962
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TN-D-1552
Report Number: NASA-TN-D-1552
Accession Number
63N10181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
FAILURE
AIRCRAFT INSTRUMENT
FLIGHT SIMULATION
PILOT PERFORMANCE

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