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Integration of Dynamic Models in Range OperationsThis work addresses the various model interactions in real-time to make an efficient internet based decision making tool for Shuttle launch. The decision making tool depends on the launch commit criteria coupled with physical models. Dynamic interaction between a wide variety of simulation applications and techniques, embedded algorithms, and data visualizations are needed to exploit the full potential of modeling and simulation. This paper also discusses in depth details of web based 3-D graphics and applications to range safety. The advantages of this dynamic model integration are secure accessibility and distribution of real time information to other NASA centers.
Document ID
20050009947
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Bardina, Jorge
(NASA Ames Research Center Moffett Field, CA, United States)
Thirumalainambi, Rajkumar
(Science Applications International Corp. Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
SAE-2004-013083
Report Number: SAE-2004-013083
Meeting Information
Meeting: World Aviation Congress 2004
Location: Reno, NV
Country: United States
Start Date: January 1, 2004
Sponsors: Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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