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Survey of Quantitative Research Metrics to Assess Pilot Performance in Upset RecoveryAccidents attributable to in-flight loss of control are the primary cause for fatal commercial jet accidents worldwide. The National Aeronautics and Space Administration (NASA) conducted a literature review to determine and identify the quantitative standards for assessing upset recovery performance. This review contains current recovery procedures for both military and commercial aviation and includes the metrics researchers use to assess aircraft recovery performance. Metrics include time to first input, recognition time and recovery time and whether that input was correct or incorrect. Other metrics included are: the state of the autopilot and autothrottle, control wheel/sidestick movement resulting in pitch and roll, and inputs to the throttle and rudder. In addition, airplane state measures, such as roll reversals, altitude loss/gain, maximum vertical speed, maximum/minimum air speed, maximum bank angle and maximum g loading are reviewed as well.
Document ID
20160006310
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Le Vie, Lisa R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 17, 2016
Publication Date
April 1, 2016
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/TM-2016-219191
L-20572
NF1676L-21763
Funding Number(s)
WBS: WBS 284848.02.50.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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