Orbit determination of the Lunar Reconnaissance Orbiter

By E. Mazarico, D. Rowlands, G. Neumann, David E. Smith, M. Torrence, F. LeMoine, Maria T. Zuber. Journal of Geodesy, 2012

183 citations recorded by the source corpus.

Subfields: Astronomy and Astrophysics

View Paper: https://www.semanticscholar.org/paper/97057203098c9e840f85db3c31235baaae2e36cf

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Astronomy and Astrophysics

1. Maria T. Zuber
2. Mark A. Wieczorek
3. G. Neumann
4. James W. Head III
5. David E. Smith
6. F. LeMoine
7. E. Mazarico
8. Mark S. Robinson

Citations in the corpus

• High‒degree gravity models from GRAIL primary mission data (2013, background): “We note that while the DSN furnishes calibration polynomials for correction of ionosphere delay on a per-spacecraft basis, the more general approach that we have implemented has also allowed us to correct the S-band tracking data to the Lunar Reconnaissance Orbiter (LRO), improving in particular the”
• Summary of the results from the lunar orbiter laser altimeter after seven years in lunar orbit (2017, methodology): “Mazarico et al. (2012) described the orbit determination methodology that enabled the fulfillment of the geodetic requirements.”