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Pilot-model analysis and simulation study of effect of control task desired control responseA pilot model analysis was performed that relates pilot control compensation, pilot aircraft system response, and aircraft response characteristics for longitudinal control. The results show that a higher aircraft short period frequency is required to achieve superior pilot aircraft system response in an altitude control task than is required in an attitude control task. These results were confirmed by a simulation study of target tracking. It was concluded that the pilot model analysis provides a theoretical basis for determining the effect of control task on pilot opinions.
Document ID
19780012200
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Adams, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Gera, J.
(NASA Langley Research Center Hampton, VA, United States)
Jaudon, J. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TP-1140
Report Number: NASA-TP-1140
Accession Number
78N20143
Funding Number(s)
PROJECT: RTOP 512-51-02-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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