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Analysis of pilot control strategyMethods for nonintrusive identification of pilot control strategy and task execution dynamics are presented along with examples based on flight data. The specific analysis technique is Nonintrusive Parameter Identification Procedure (NIPIP), which is described in a companion user's guide (NASA CR-170398). Quantification of pilot control strategy and task execution dynamics is discussed in general terms followed by a more detailed description of how NIPIP can be applied. The examples are based on flight data obtained from the NASA F-8 digital fly by wire airplane. These examples involve various piloting tasks and control axes as well as a demonstration of how the dynamics of the aircraft itself are identified using NIPIP. Application of NIPIP to the AFTI/F-16 flight test program is discussed. Recommendations are made for flight test applications in general and refinement of NIPIP to include interactive computer graphics.
Document ID
19830013941
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Heffley, R. K.
(Systems Technology, Inc. Mountain View, CA, United States)
Hanson, G. D.
(Systems Technology, Inc. Mountain View, CA, United States)
Jewell, W. F.
(Systems Technology, Inc. Mountain View, CA, United States)
Clement, W. F.
(Systems Technology, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
TR-1188-2
NAS 1.26:170399
NASA-CR-170399
Report Number: TR-1188-2
Report Number: NAS 1.26:170399
Report Number: NASA-CR-170399
Accession Number
83N22212
Funding Number(s)
CONTRACT_GRANT: NAS4-2941
PROJECT: RTOP 505-31-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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