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 |