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

Fujimoto, K.; Leonard, J. M.; McGranaghan, R. M.; Parker, J. S.; Anderson, R. L.; Born, G. H.

dc.contributor.author	Fujimoto, K.
dc.contributor.author	Leonard, J. M.
dc.contributor.author	McGranaghan, R. M.
dc.contributor.author	Parker, J. S.
dc.contributor.author	Anderson, R. L.
dc.contributor.author	Born, G. H.
dc.date.accessioned	2013-04-23T15:20:43Z
dc.date.available	2013-04-23T15:20:43Z
dc.date.issued	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.identifier.uri	http://hdl.handle.net/2014/43020
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