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Integrated Thermal Response Modeling System For Hypersonic Entry VehiclesWe 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.
Document ID
20010066108
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Chen, Y.-K. (NASA Ames Research Center Moffett Field, CA United States)
Milos, F. S. (NASA Ames Research Center Moffett Field, CA United States)
Partridge, Harry
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 39th AIAA Space Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 242-90-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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