2017
DOI: 10.1016/j.geog.2017.03.013
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A GOCE only gravity model GOSG01S and the validation of GOCE related satellite gravity models

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Cited by 19 publications
(19 citation statements)
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“…In this paper, we derive the coseismic gravity and gravity gradient changes by evaluating the differences between a post-earthquake gravity field model and a pre-earthquake one from GOCE data; namely, we first recover gravity field models from the Gravity field and steady state Ocean Circulation Explorer Satellite Gravity Gradient (GOCE SGG) observations before and after the 2011 Tohoku-Oki earthquake. Here, we provide a brief description of the data processing strategies of recovering a gravity field model from GOCE SGG observations (more details can be found in Xu et al [33]).…”
Section: Recovering Gravity Field Model From Goce Sgg Observationsmentioning
confidence: 99%
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“…In this paper, we derive the coseismic gravity and gravity gradient changes by evaluating the differences between a post-earthquake gravity field model and a pre-earthquake one from GOCE data; namely, we first recover gravity field models from the Gravity field and steady state Ocean Circulation Explorer Satellite Gravity Gradient (GOCE SGG) observations before and after the 2011 Tohoku-Oki earthquake. Here, we provide a brief description of the data processing strategies of recovering a gravity field model from GOCE SGG observations (more details can be found in Xu et al [33]).…”
Section: Recovering Gravity Field Model From Goce Sgg Observationsmentioning
confidence: 99%
“…The component V ij of the second-order gravity gradient tensor (GGT) is normally defined in the Local North-Oriented Frame (LNOF) with the x-axis pointing north, the y-axis pointing west and the z-axis up, as follows [33]: C nm S nm (1) where the indices i and j define the gravitational gradient components (xx, yy, zz, xy, . .…”
Section: Recovering Gravity Field Model From Goce Sgg Observationsmentioning
confidence: 99%
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“…In most cases the SST part comes from high-low Global Navigation Satellite System (GNSS) observations between the spacecraft carrying the gradiometer and GNSS spacecraft, and in such cases, the orbits are usually done in Precise Kinematic mode, which means that there are no equations of motion involved and the positions are determined independently at each observation point. [20,35,36,37]. The squareroot variance (or RMS) is plotted as a function of the geopotential degree (the value of 2n in the symbol J 2n of a multipole).…”
Section: Conceptual Shortcomings Of Differencing the Lowest Even Zonamentioning
confidence: 99%
“…The acceleration method is based on Newton's equation of motion, which balances the gravitational vector with satellite accelerations in the inertial reference frame [14,15]. The principle of acceleration approach is simple and has been successfully applied to CHAMP, GRACE, and GOCE SST-hl data analysis [14][15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%