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Simulating the Liaison Navigation Concept in a Geo + Earth-Moon Halo ConstellationLinked Autonomous Interplanetary Satellite Orbit Navigation, or LiAISON, is a novel satellite navigation technique where relative radiometric measurements between two or more spacecraft in a constellation are processed to obtain the absolute state of all spacecraft. The method leverages the asymmetry of the gravity field that the constellation exists in. This paper takes a step forward in developing a high fidelity navigation simulation for the LiAISON concept in an Earth-Moon constellation. In particular, we aim to process two-way Doppler measurements between a satellite in GEO orbit and another in a halo orbit about the Earth-Moon L1 point.
Document ID
20150004593
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Fujimoto, K.
(Colorado Univ. Boulder, CO, United States)
Leonard, J. M.
(Colorado Univ. Boulder, CO, United States)
McGranaghan, R. M.
(Colorado Univ. Boulder, CO, United States)
Parker, J. S.
(Colorado Univ. Boulder, CO, United States)
Anderson, R. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Born, G. H.
(Colorado Univ. Boulder, CO, United States)
Date Acquired
April 8, 2015
Publication Date
October 29, 2012
Subject Category
Lunar And Planetary Science And Exploration
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: International Symposium on Space Flight Dynamics
Location: Pasadena, CA
Country: United States
Start Date: October 29, 2012
End Date: November 2, 2012
Sponsors: Jet Propulsion Lab., California Inst. of Tech.
Distribution Limits
Public
Copyright
Other
Keywords
Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON)
satellite-to-satellite tracking
orbit determination
autonomous nagivation

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