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Simulating the liaison navigation concept in a geo + Earth-Moon halo constellation

Show simple item record Fujimoto, K. Leonard, J. M. McGranaghan, R. M. Parker, J. S. Anderson, R. L. Born, G. H. 2013-04-23T15:20:43Z 2013-04-23T15:20:43Z 2012-10-29
dc.identifier.citation 23rd International Symposium on Space Flight Dynamics, Pasadena, California, October 29 - November 2, 2012 en_US
dc.identifier.clearanceno 12-5146
dc.description.abstract Linked 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. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012. en_US
dc.subject Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON) en_US
dc.subject satellite-to-satellite tracking en_US
dc.subject orbit determination en_US
dc.subject autonomous nagivation en_US
dc.title Simulating the liaison navigation concept in a geo + Earth-Moon halo constellation en_US
dc.type Preprint en_US
dc.subject.NASATaxonomy Space Communications, Spacecraft Communications, Command and Tracking en_US

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