2007
DOI: 10.1016/j.asr.2007.04.040
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The LAGEOS satellites orbital residuals determination and the way to extract gravitational and non-gravitational unmodeled perturbing effects

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Cited by 18 publications
(21 citation statements)
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“…Summarizing, Iorio et al [28,138,139], having at disposal several Earth's gravity models released by different institutions worldwide, took the differences ∆J = J A − J B = 2 4 6 20 between the estimated multipoles for several pairs (A B) of models as representative of the real uncertainties of the even zonals. See also [140]. The models considered in [28,138,139] were EIGEN-GRACE02S [125], GGM02S [136], GGM03S [141], EIGEN-CG03C [134], ITG-Grace02s [142], ITGGrace03s [143], ITG-Grace2010s [144], AIUB-GRACE01S [145], AIUB-GRACE02S [146], JEM01-RL03B from JPL (NASA, USA), EGM2008 [147].…”
Section: It Would Roughly Correspond To ≈ 2 − 3 MM In Determining Thementioning
confidence: 99%
“…Summarizing, Iorio et al [28,138,139], having at disposal several Earth's gravity models released by different institutions worldwide, took the differences ∆J = J A − J B = 2 4 6 20 between the estimated multipoles for several pairs (A B) of models as representative of the real uncertainties of the even zonals. See also [140]. The models considered in [28,138,139] were EIGEN-GRACE02S [125], GGM02S [136], GGM03S [141], EIGEN-CG03C [134], ITG-Grace02s [142], ITGGrace03s [143], ITG-Grace2010s [144], AIUB-GRACE01S [145], AIUB-GRACE02S [146], JEM01-RL03B from JPL (NASA, USA), EGM2008 [147].…”
Section: It Would Roughly Correspond To ≈ 2 − 3 MM In Determining Thementioning
confidence: 99%
“…The scatter is still quite large 9 See Fig. 5 of Lucchesi (2007) for a comparison of the estimated C 40 in different models. 10 I thank M. Watkins (JPL) for having provided me with the even zonals and their sigmas of the JEM01-RL03B model.…”
Section: The Systematic Error Of Gravitational Origin In the Lageos-lmentioning
confidence: 96%
“…[42] to extract the gravitomagentic signal from the LAGEOS and LAGEOS II data is described in detail in Refs. [54,63]. The Lense-Thirring force is not included in the dynamical force models used to fit the satellites' data.…”
Section: A New Approach To Extract the Lense-thirring Signature From mentioning
confidence: 99%