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Design considerations of manipulator and feel system characteristics in roll trackingA fixed-base simulation was performed to identify and quantify interactions between the pilot's hand/arm neuromuscular subsystem and such control system features of typical modern fighter aircraft roll rate command mechanizations as: (1) force versus displacement sensing side-stick type manipulator, (2) feel force/displacement gradient, (3) feel system versus command prefilter dynamic lag, and (4) flight control system effective time delay. The experiment encompassed some 48 manipulator/filter/aircraft configurations. Displacement side-stick experiment results are given and compared with the previous force sidestick experiment results. Attention is focused on control bandwidth, excitement (peaking) of the neuromuscular mode, feel force/displacement gradient effects, time delay effects, etc. Section 5 is devoted to experiments with a center-stick in which force versus displacement sensing, feel system lag, and command prefilter lag influences on tracking performance and pilot preference are investigated.
Document ID
19890017489
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnston, Donald E.
(Systems Technology, Inc. Hawthorne, CA, United States)
Aponso, Bimal L.
(Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1988
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-4111
NAS 1.26:4111
H-1438
Report Number: NASA-CR-4111
Report Number: NAS 1.26:4111
Report Number: H-1438
Accession Number
89N26860
Funding Number(s)
CONTRACT_GRANT: NAS2-12221
PROJECT: RTOP 505-67-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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