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Investigation of Alternative Return Strategies for Orion Trans-earth Injection Design OptionsThe purpose of this study is to investigate alternative return strategies for the Orion trans-Earth injection (TEI) phase. A dynamical systems analysis approach considers the structure of the stable and unstable Sun perturbed Earth-Moon manifolds near the Earth-Moon interface region. A hybrid approach, then, combines the results from this analysis with classical two-body methods in a targeting process that seeks to expand the window of return opportunities in a precision entry scenario. The resulting startup arcs can be used, for instance, to enhance the block set of solutions available onboard during an autonomous targeting process.
Document ID
20100008486
Acquisition Source
Johnson Space Center
Document Type
Other
Authors
Marchand, Belinda G.
(Texas Univ. Austin, TX, United States)
Scarritt, Sara K.
(Texas Univ. Austin, TX, United States)
Howell, Kathleen C.
(Purdue Univ. West Lafayette, IN, United States)
Weeks, Michael W.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
February 14, 2010
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-19904
Report Number: JSC-CN-19904
Meeting Information
Meeting: 20th AAS/AIAA Space Flight Mechanics Meeting
Location: San Diego, CA
Country: United States
Start Date: February 14, 2010
End Date: February 17, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: WBS 644423.02.36.15.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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