English

LATOR Covariance Analysis

General Relativity and Quantum Cosmology 2009-11-11 v4

Abstract

We present results from a covariance study for the proposed Laser Astrometric Test of Relativity (LATOR) mission. This mission would send two laser-transmitter spacecraft behind the Sun and measure the relative gravitational light bending of their signals using a hundred-meter-baseline optical interferometer to be constructed on the International Space Station. We assume that each spacecraft is equipped with a <1.9×1013ms2Hz1/2 < 1.9 \times 10^{-13} \mathrm{m} \mathrm{s}^2 \mathrm{Hz}^{-1/2} drag-free system and assume approximately one year of data. We conclude that the observations allow a simultaneous determination of the orbit parameters of the spacecraft and of the Parametrized Post-Newtonian (PPN) parameter γ\gamma with an uncertainty of 2.4×1092.4 \times 10^{-9}. We also find a 6×1096 \times 10^{-9} determination of the solar quadrupole moment, J2J_2, as well as the first measurement of the second-order post-PPN parameter δ\delta to an accuracy of about 10310^{-3}.

Keywords

Cite

@article{arxiv.gr-qc/0505064,
  title  = {LATOR Covariance Analysis},
  author = {Joseph E. Plowman and Ronald W. Hellings},
  journal= {arXiv preprint arXiv:gr-qc/0505064},
  year   = {2009}
}

Comments

9 pages, 3 figures. first revision: minor changes to results. Second revision: additional discussion of orbit modelling and LATOR drag-free system requirement feasibility. Added references to tables I and V (which list PPN parameter uncertainties), removed word from sentence in Section III. 3rd revision: removed 2 incorrect text fragments (referring to impact parameter as distance of closest approach) and reference to upcoming publication of ref. 2, removed spurious gamma from eq. 1 - Last error is still in cqg published version