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Constellations of elliptical inclined lunar orbits providing polar and global coveragePrior results have developed a methodology for selecting a long-lived constellation of 3 satellites that provide persistent, stable coverage to either the North or South Pole with no requirement for stationkeeping under the influence of only gravitational perturbations. In the present study, the sensitivity of this coverage in the presence of non-gravitational forces is determined, and a design strategy is formulated that minimizes any potential sensitivity to these accelerations.
Document ID
20060042653
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Ely, Todd A.
Lieb, Erica
Date Acquired
August 23, 2013
Publication Date
August 7, 2005
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Lake Tahoe, CA
Country: United States
Start Date: August 7, 2005
End Date: August 11, 2005
Distribution Limits
Public
Copyright
Other
Keywords
lunar constellation design
orbit control
astrodynamics

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