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Investigation of Control Inceptor Dynamics and Effect on Human Subject PerformanceThe control inceptor used in a vehicle simulation is an important part of adequately representing the dynamics of the vehicle. The inceptor characteristics are typically based on a second order spring mass damper system with damping, force gradient, breakout force, and natural frequency parameters. Changing these parameters can have a great effect on pilot control of the vehicle. A quasi transfer of training experiment was performed employing a high fidelity and a low fidelity control inceptor. A disturbance compensatory task was employed which involved a simple horizon line disturbed in roll by a sum of sinusoids presented in an out-the-window display. Vehicle dynamics were modeled as 1/s and 1/s2. The task was to maintain level flight. Twenty subjects were divided between the high and the low fidelity training groups. Each group was trained to a performance asymptote, and then transferred to the high fidelity simulation. RMS tracking error, a PSD analysis, and a workload analysis were performed to quantify the transfer of training effect. Quantitative results of the experiments show that there is no significant difference between the high and low fidelity training groups for 1/s plant dynamics. For 1/s2 plant dynamics there is a greater difference in tracking performance and PSD; and the subjects are less correlated with the input disturbance function
Document ID
20140001008
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Stanco, Anthony A.
(State Univ. of New York Binghamton, NY, United States)
Cardullo, Frank M.
(State Univ. of New York Binghamton, NY, United States)
Houck, Jacob A.
(NASA Langley Research Center Hampton, VA, United States)
Grube, Richard C.
(NASA Langley Research Center Hampton, VA, United States)
Kelly, Lon C.
(Unisys Corp. Hampton, VA, United States)
Date Acquired
March 4, 2014
Publication Date
July 1, 2013
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NF1576L-16936
NASA/TM-2013-218026
L-20288
Funding Number(s)
WBS: WBS 160961.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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