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Combining Simulation Tools for End-to-End Trajectory OptimizationTrajectory simulations with advanced optimization algorithms are invaluable tools in the process of designing spacecraft. Due to the need for complex models, simulations are often highly tailored to the needs of the particular program or mission. NASA's Orion and SLS programs are no exception. While independent analyses are valuable to assess individual spacecraft capabilities, a complete end-to-end trajectory from launch to splashdown maximizes potential performance and ensures a continuous solution. In order to obtain end-to-end capability, Orion's in-space tool (Copernicus) was made to interface directly with the SLS's ascent tool (POST2) and a new tool to optimize the full problem by operating both simulations simultaneously was born.
Document ID
20150016036
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Whitley, Ryan
(NASA Johnson Space Center Houston, TX, United States)
Gutkowski, Jeffrey
(NASA Johnson Space Center Houston, TX, United States)
Craig, Scott
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Dawn, Tim
(NASA Johnson Space Center Houston, TX, United States)
Williams, Jacobs
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Stein, William B.
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Litton, Daniel
(NASA Langley Research Center Hampton, VA, United States)
Lugo, Rafael
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Qu, Min
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
August 14, 2015
Publication Date
August 9, 2015
Subject Category
Astrodynamics
Report/Patent Number
AAS 15-662
JSC-CN-33978
Report Number: AAS 15-662
Report Number: JSC-CN-33978
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist
Location: Vail, CO
Country: United States
Start Date: August 9, 2015
End Date: August 13, 2015
Sponsors: American Astronomical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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