Abstract
This paper presents a tutorial analysis of a hybrid computer model of a missile reentering the atmosphere. An important aspect is that an example of how to go about analyzing the suitability of a hybrid computer configuration for a particular large-scale simulation is presented from an overall systems point of view. Equations describing a missile (six-degrees of freedom) reentering the atmosphere are given as is a hybrid computer configuration for solving them. This configuration is then analyzed to establish its suitability for simulation.
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