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Phase Control and Eclipse Avoidance in Near Rectilinear Halo OrbitsThe baseline trajectory proposed for the Gateway is a southern Earth-Moon L2 Near Rectilinear Halo Orbit (NRHO). Designed to avoid eclipses, the NRHO exhibits a resonance with the lunar synodic period. The current investigation details the eclipse behavior in the baseline NRHO. Then, phase control is added to the orbit maintenance algorithm to regulate perilune passage time and maintain the eclipse-free characteristics of the Gateway reference orbit. A targeting strategy is designed to periodically target back to the long-horizon virtual reference if the orbit diverges over time in the presence of additional perturbations.

Document ID
20200000733
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Davis, Diane C.
(Jacobs Engineering Group Houston, TX, United States)
Khoury, Fouad S.
(Purdue Univ. West Lafayette, IN, United States)
Howell, Kathleen C.
(Purdue Univ. West Lafayette, IN, United States)
Sweeney, Daniel J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
February 4, 2020
Publication Date
January 30, 2020
Subject Category
Astrodynamics
Report/Patent Number
JSC-E-DAA-TN77422
Report Number: JSC-E-DAA-TN77422
Meeting Information
Meeting: AAS Guidance, Navigation and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: January 30, 2020
End Date: February 5, 2020
Sponsors: American Astronautical Society (AAS)
Funding Number(s)
CONTRACT_GRANT: NNJ13HA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
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