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Human dynamic orientation model applied to motion simulationThe Ormsby model of dynamic orientation, in the form of a discrete time computer program was used to predict non-visually induced sensations during an idealized coordinated aircraft turn. To predict simulation fidelity, the Ormsby model was used to assign penalties for incorrect attitude and angular rate perceptions. It was determined that a three rotational degree of freedom simulation should remain faithful to attitude perception even at the expense of incorrect angular rate sensations. Implementing this strategy, a simulation profile for the idealized turn was designed for a Link GAT-1 trainer. A simple optokinetic display was added to improve the fidelity of roll rate sensations.
Document ID
19770012810
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Borah, J. D.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-149862
Report Number: NASA-CR-149862
Accession Number
77N19754
Funding Number(s)
CONTRACT_GRANT: NSR-22-009-701
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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