NASA NTRS · 19800010786
Closed loop models for analyzing engineering requirements for simulators
Abstract
A closed loop analytic model, incorporating a model for the human pilot, (namely, the optimal control model) that would allow certain simulation design tradeoffs to be evaluated quantitatively was developed. This model was applied to a realistic flight control problem. The resulting model is used to analyze both overall simulation effects and the effects of individual elements. The results show that, as compared to an ideal continuous simulation, the discrete simulation can result in significant performance and/or workload penalties.
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Baron, S., Muralidharan, R., Kleinman, D.. 1980-02-01. Closed loop models for analyzing engineering requirements for simulators. https://ntrs.nasa.gov/citations/19800010786
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