Orbit determination of the Lunar Reconnaissance Orbiter: Status after Seven Years

Erwan Mazarico; Gregory A Neumann; Michael K Barker; Sander Goossens; David E Smith; Maria T Zuber

doi:10.1016/j.pss.2017.10.004

Orbit determination of the Lunar Reconnaissance Orbiter: Status after Seven Years

Planet Space Sci. 2018 Nov 1:162:2-19. doi: 10.1016/j.pss.2017.10.004. Epub 2017 Oct 12.

Authors

Erwan Mazarico¹, Gregory A Neumann¹, Michael K Barker^{2

1}, Sander Goossens^{3

1}, David E Smith⁴, Maria T Zuber⁴

Affiliations

¹ NASA Goddard Space Flight Center, 8800 Greenbelt Road, Greenbelt, Maryland, USA.
² Sigma Space Corporation, 4600 Forbes Boulevard, Lanham, Maryland, USA.
³ University of Maryland Baltimore County, Center for Research and Exploration in Space Science & Technology, 1000 Hilltop Circle, Baltimore, Maryland, USA.
⁴ Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, Massachusetts, USA.

Abstract

The Lunar Reconnaissance Orbiter (LRO) has been orbiting the Moon since 2009, obtaining unique and foundational datasets important to understanding the evolution of the Moon and the Solar System. The high-resolution data acquired by LRO benefit from precise orbit determination (OD), limiting the need for geolocation and co-registration tasks. The initial position knowledge requirement (50 meters) was met with radio tracking from ground stations, after combination with LOLA altimetric crossovers. LRO-specific gravity field solutions were determined and allowed radio-only OD to perform at the level of 20 meters, although secular inclination changes required frequent updates. The high-accuracy gravity fields from GRAIL, with <10 km spatial resolution, further improved the radio-only orbit reconstruction quality (<10 meters). However, orbit reconstruction is in part limited by the 0.3-0.5 mm/s measurement noise level in S-band tracking. One-way tracking through Laser Ranging can supplement the tracking available for OD with 28-Hz ranges with 20-cm single-shot precision, but is available only on the nearside (the lunar hemisphere facing the Earth due to tidal locking). Here, we report on the status of the OD effort since the beginning of the mission, a period spanning more than seven years. We describe modeling improvements and the use of new measurements. In particular, the LOLA altimetric data give accurate, uniform, and independent information about LRO's orbit, with a different sensitivity and geometry which includes coverage over the lunar farside and is not tied to ground-based assets. With SLDEM2015 (a combination of the LOLA topographic profiles and the Kaguya Terrain Camera stereo images), another use of altimetry is possible for OD. We extend the 'direct altimetry' technique developed for the ICESat mission to perform OD and adjust spacecraft position to minimize discrepancies between LOLA tracks and SLDEM2015. Comparisons with the radio-only orbits are used to evaluate this new tracking type, of interest for the OD of future lunar orbiters carrying a laser altimeter. LROC NAC images also provide independent accuracy estimation, through the repeated views taken of anthropogenic features for instance.

Keywords: Laser Altimetry; Lunar Reconnaissance Orbiter; Moon; Orbit Determination; Radio Tracking.