Supporting Crewed Lunar Exploration with LiAISON Navigation

This paper examines the benefits of navigating a crewed vehicle between the Earth and the Moon using both ground tracking and satellite-to-satellite tracking. Linked Autonomous Interplanetary Satellite Orbit Navigation (LiAISON) is a new technique that has been shown to dramatically improve the navigation of lunar satellites, libration orbiters, and Earth orbiting satellites using scalar intersatellite observations. In this paper, LiAISON is applied to the problem of navigating a crewed vehicle to the Moon. It has been found that LiAISON observations improve the navigation accuracy enough to reduce the number of active ground tracking stations from six to three.

[1]  George H. Born,et al.  Autonomous Interplanetary Orbit Determination Using Satellite-to-Satellite Tracking , 2007 .

[2]  J. Leonard,et al.  Liaison-Supplemented Navigation for Geosynchronous and Lunar L1 Orbiters , 2012 .

[3]  Rodney L. Anderson,et al.  Navigation Between Geosynchronous and Lunar L1 Orbiters , 2012 .

[4]  A. Konopliv,et al.  Recent Gravity Models as a Result of the Lunar Prospector Mission , 2001 .

[5]  Oliver Montenbruck,et al.  Satellite Orbits: Models, Methods and Applications , 2000 .

[6]  Stephen B. Broschart,et al.  ARTEMIS Mission Design , 2011 .

[7]  J. Junkins,et al.  Optimal Estimation of Dynamic Systems , 2004 .

[8]  D. Richardson,et al.  A uniformly valid solution for motion about the interior libration point of the perturbed elliptic-restricted problem , 1975 .

[9]  M. Cheng,et al.  GGM02 – An improved Earth gravity field model from GRACE , 2005 .

[10]  Robert G. Gottlieb,et al.  Fast gravity, gravity partials, normalized gravity, gravity gradient torque and magnetic field: Derivation, code and data , 1993 .

[11]  George H. Born,et al.  A Lunar L2 Navigation, Communication, and Gravity Mission , 2006 .

[13]  T. Kerr Status of CR-like lower bounds for nonlinear filtering , 1989 .

[14]  K. Hill,et al.  Autonomous Navigation in Libration Point Orbits , 2007 .

[15]  K. Hill AAS 05-399 LINKED , AUTONOMOUS , INTERPLANETARY SATELLITE ORBIT NAVIGATION ( LiAISON ) , 2022 .

[16]  Timothy Crain,et al.  Orion Navigation Sensitivities to Ground Station Infrastructure for Lunar Missions , 2008 .

[17]  W. R. Wollenhaupt,et al.  Apollo Orbit Determination and Navigation , 1970 .

[18]  Jeffrey S. Parker,et al.  Low-energy ballistic lunar transfers , 2007 .

[19]  Daniel Cosgrove,et al.  Stationkeeping of the First Earth-Moon Libration Orbiters: The ARTEMIS Mission , 2011 .

[20]  James H. Taylor The Cramer-Rao estimation error lower bound computation for deterministic nonlinear systems , 1978, 1978 IEEE Conference on Decision and Control including the 17th Symposium on Adaptive Processes.

[21]  Vassilis Angelopoulos,et al.  The ARTEMIS Mission , 2011 .