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Baseline Orbit Generation for Near Rectilinear Halo OrbitsA Near Rectilinear Halo Orbit (NRHO) with an eclipse-favorable phase serves as the current baseline orbit for the Gateway mission. The baseline provides a catalog of orbit maintenance targets and serves as a reference path for other types of trajectory analysis. In this investigation, an automated multiple-shooting differential corrections strategy is developed to generate many-revolution, long-duration, ballistic baseline orbits in a higher-fidelity ephemeris force model at the eclipse-avoidant phases and at other alternative phases. Additional geometric considerations for eclipse avoidance in the NRHO are presented and utilized within a long-lead orbit maintenance-based phase shift strategy.
Document ID
20230010734
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Emily M. Zimovan-Spreen
(Johnson Space Center Houston, Texas, United States)
Stephen T. Scheuerle
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Brian P. Mccarthy
(Jacobs (United States) Dallas, Texas, United States)
Diane C. Davis
(Johnson Space Center Dallas, Texas, United States)
Kathleen C. Howell
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Date Acquired
July 24, 2023
Subject Category
Astronomy
Geosciences (General)
Report/Patent Number
AAS 23-268
Meeting Information
Meeting: AAS/AAIA Astrodynamics Specialist Conference
Location: Big Sky, MT
Country: US
Start Date: August 13, 2023
End Date: August 17, 2023
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: #NNJ13HA01C
CONTRACT_GRANT: #80NSSC18M0122
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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