This code models the flight dynamics of the space shuttle during reentry into the atmosphere. The model is limited by a heating rate constraint on the leading edge of the shuttle wings, and runs an optimization in dymos to maximize crossrange. The model was built as a testbed for the autoscaling algorithm in development for OpenMDAO and dymos.
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jdgratz10/SpaceShuttleReentry
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Dynamic model of space shuttle reentering atmosphere. To be used as testbed for autoscaling algorithm.
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