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NASA NTRS · 20010066108

Integrated Thermal Response Modeling System For Hypersonic Entry Vehicles

Abstract

We describe all extension of the Markov decision process model in which a continuous time dimension is included ill the state space. This allows for the representation and exact solution of a wide range of problems in which transitions or rewards vary over time. We examine problems based on route planning with public transportation and telescope observation scheduling.

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BibTeXRIS

Chen, Y.-K., Milos, F. S., Partridge, Harry. 2000-01-01. Integrated Thermal Response Modeling System For Hypersonic Entry Vehicles. https://ntrs.nasa.gov/citations/20010066108

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