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Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamicsThis report presents the results of analysis of cockpit lateral control feel-system studies. Variations in feel-system natural frequency, damping, and command sensing reference (force and position) were investigated, in combination with variations in the aircraft response characteristics. The primary data for the report were obtained from a flight investigation conducted with a variable-stability airplane, with additional information taken from other flight experiments and ground-based simulations for both airplanes and helicopters . The study consisted of analysis of handling qualities ratings and extraction of open-loop, pilot-vehicle describing functions from sum-of-sines tracking data, including, for a limited subset of these data, the development of pilot models. The study confirms the findings of other investigators that the effects on pilot opinion of cockpit feel-system dynamics are not equivalent to a comparable level of added time delay, and until a more comprehensive set of criteria are developed, it is recommended that feel-system dynamics be considered a delay-inducing element in the aircraft response. The best correlation with time-delay requirements was found when the feel-system dynamics were included in the delay measurements, regardless of the command reference. This is a radical departure from past approaches.
Document ID
19920019341
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mitchell, David G.
(Systems Technology, Inc. Hawthorne, CA, United States)
Aponso, Bimal L.
(Systems Technology, Inc. Hawthorne, CA, United States)
Klyde, David H.
(Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Publication Information
Publisher: NASA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:4443
NASA-CR-4443
H-1769
Report Number: NAS 1.26:4443
Report Number: NASA-CR-4443
Report Number: H-1769
Accession Number
92N28584
Funding Number(s)
CONTRACT_GRANT: NAS2-12722
CONTRACT_GRANT: ATD-90-STI-6401
PROJECT: RTOP 505-64-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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