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Navigation Design and Analysis for the Orion Earth-Moon MissionThis paper details the design of the cislunar optical navigation system being proposed for the Orion Earth-Moon (EM) missions. In particular, it presents the mathematics of the navigation filter. The unmodeled accelerations and their characterization are detailed. It also presents the analysis that has been performed to understand the performance of the proposed system, with particular attention paid to entry flight path angle constraints and the delta-V performance.
Document ID
20140005962
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
DSouza, Christopher (NASA Johnson Space Center Houston, TX, United States)
Zanetti, Renato (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
May 20, 2014
Publication Date
January 26, 2014
Subject Category
Astrodynamics
Report/Patent Number
JSC-CN-30283
AAS 14-263
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Conference
Location: Santa Fe, NM
Country: United States
Start Date: January 26, 2014
End Date: January 30, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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