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Comparison of simulator fidelity model predictions with in-simulator evaluation dataA full factorial in simulator experiment of a single axis, multiloop, compensatory pitch tracking task is described. The experiment was conducted to provide data to validate extensions to an analytic, closed loop model of a real time digital simulation facility. The results of the experiment encompassing various simulation fidelity factors, such as visual delay, digital integration algorithms, computer iteration rates, control loading bandwidths and proprioceptive cues, and g-seat kinesthetic cues, are compared with predictions obtained from the analytic model incorporating an optimal control model of the human pilot. The in-simulator results demonstrate more sensitivity to the g-seat and to the control loader conditions than were predicted by the model. However, the model predictions are generally upheld, although the predicted magnitudes of the states and of the error terms are sometimes off considerably. Of particular concern is the large sensitivity difference for one control loader condition, as well as the model/in-simulator mismatch in the magnitude of the plant states when the other states match.
Document ID
19830010444
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Parrish, R. V.
(NASA Langley Research Center Hampton, VA, United States)
Mckissick, B. T.
(NASA Langley Research Center Hampton, VA, United States)
Ashworth, B. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.60:2106
NASA-TP-2106
L-15519
Report Number: NAS 1.60:2106
Report Number: NASA-TP-2106
Report Number: L-15519
Accession Number
83N18715
Funding Number(s)
PROJECT: RTOP 505-35-33-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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