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|Title: ||Navigation between geosynchronous and Lunar L1 orbiters|
|Authors: ||Parker, Jeffrey S.|
Anderson, Rodney L.
Born, George H.
Leonard, Jason M.
McGranaghan, Ryan M.
|Keywords: ||LiAISON (Linked Autonomous Interplanetary Satellite Orbit Navigation)|
|Issue Date: ||13-Aug-2012 |
|Publisher: ||Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012.|
|Citation: ||AIAA/AAS Astrodynamics Specialist Conference, Minneapolis, Minnesota, August 13-16, 2012|
|Abstract: ||Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON) is a new technique
that takes advantage of the asymmetrical gravity field present in a three-body system
in order to perform absolute tracking of satellites using only relative satellite-to-satellite observations. Previous studies have demonstrated LiAISON’s practical applications for lunar missions, including a satellite in a halo orbit about either the Earth-Moon L1 or L2 point. This paper studies the viability of applying LiAISON measurements between a
lunar halo orbiter and a satellite in a geosynchronous orbit. Simulations demonstrate that the absolute positions and velocities of both satellites are observable using only relative measurements with an achieved uncertainty on the order of observation noise.|
|Appears in Collections:||JPL TRS 1992+|
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