NASA NTRS ยท 19770012810
Human dynamic orientation model applied to motion simulation
Abstract
The 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.
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Borah, J. D.. 1976-05-01. Human dynamic orientation model applied to motion simulation. https://ntrs.nasa.gov/citations/19770012810
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