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Title
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Human Pilot Dynamics in Compensatory Systems: Theory, Models, and Experiments with Controlled Element and Forcing Function Variations
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Date
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1965
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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AFFDL TR 65-15
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Creator
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McRuer, Duane
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Graham, Dunstan
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Krendel, Ezra
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Reisener, William, Jr.
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Corporate Author
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Systems Technology, Inc.; The Franklin Institute
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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216
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NTRL Accession Number
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AD470337
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Identifier
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AD0470337
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Access Rights
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Notice(s)
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Distribution Classification
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1
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Contract
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AF 33(616)-7501
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DoD Project
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8219
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DoD Task
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821905
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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None
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Abstract
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The description of human pilot dynamic characteristics in mathematical terms compatible with flight control engineering practice is an essential prerequisite to the analytical treatment of manual vehicular control systems. The enormously adaptive nature of the human pilot makes such a description exceedingly difficult to obtain, although a quasi-linear model with parameters which vary with the system task variables had been successfully applied to many flight situations. The primary purposes of the experimental series reported are the validation of the existing quasi-linear pilot model, and the extension of this model in accuracy and detail.
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Report Availability
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Full text available
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Date Issued
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1965-07
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Provenance
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AFRL/VACA
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Type
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report
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Format
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1 online resource
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Is Referenced By
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Iuliia S. Zaitceva, Nikolay V. Kuznetsov and Boris R. Andrievsky "Application of the Nonlinear Correction Method for Attitude Control and Landing Oscillations Prevention" in Cyber-Physical Systems and Control II, 2nd International Conference on CyberPhysical Systems and Control, St. Petersburg, Russia (2021)
AFFDLTR65-015.pdf