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A Global Solution for the Gravity Field, Rotation, Landmarks, and Ephemeris of Eros
Authors:Alexander S. KonoplivJames K. Miller  William M. OwenDonald K. Yeomans  Jon D. GiorginiRomain Garmier  Jean-Pierre Barriot
Affiliation:
  • a MS 301-125J, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, 91109, f1alex.konopliv@jpl.nasa.govf1
  • b MS 301-125J, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, 91109
  • c Observatoire Midi-Pyrénées, 14 Ave. E. Belin, Toulouse, 31400, France
  • Abstract:As part of the NEAR Radio Science investigation, a global solution that includes both spherical and ellipsoidal harmonic gravity fields of Eros, Eros pole and rotation rate, Eros ephemeris, and landmark positions from the optical data was generated. This solution uses the entire one-year in orbit collection of X-band radiometric tracking (Doppler and range) from the Deep Space Network and landmark tracking observations generated from the NEAR spacecraft images of Eros. When compared to a constant density shape model, the gravity field shows a nearly homogeneous Eros. The Eros landmark solutions are in good agreement with the Eros shape model, and they reduce the center-of-mass and center-of-figure offset in the z direction to 13 m. Most of the NEAR spacecraft orbits are determined in all directions to an accuracy of several meters. The solution for the ephemeris of Eros constrains the mass of Vesta to 18.2±0.4 km3/s2 and reduces the uncertainty in the Earth-Moon mass ratio.
    Keywords:asteroids   Eros
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