Gravity, Geoid and Height Systems: Proceedings of the IAG by Urs Marti

By Urs Marti

This quantity encompasses a collection of papers awarded on the IAG foreign symposium "Gravity, Geoid and top structures 2012" (GGHS2012), which used to be geared up through IAG fee 2 “Gravity box” with the help of the overseas Gravity box provider (IGFS) and GGOS subject matter 1 “Unified worldwide peak System”. The booklet summarizes the newest effects on gravimetry and gravity networks, worldwide gravity box modeling and functions, destiny gravity box missions. It offers a close compilation on advances in distinct neighborhood and nearby high-resolution geoid modeling, the institution and unification of vertical reference platforms, contributions to gravity box and mass shipping modeling in addition to articles at the gravity box of planetary bodies.

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Extra resources for Gravity, Geoid and Height Systems: Proceedings of the IAG Symposium GGHS2012, October 9-12, 2012, Venice, Italy

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If the data (1) are given at equidistant points along the parallels, (2) are uncorrelated, and (3) have the same accuracy, then the resulting normal equation matrices are order-wise block-diagonal (Colombo 1981). M. Brockmann et al. and memory requirements for their assembly, storage and solution of the equation system are also comparably small. It is well known, however, that these simplifying assumptions are not true for real altimetry and terrestrial gravity measurements. Terrestrial and altimetry data are either not available with global coverage, or their availability is restricted (Pavlis et al.

GOCE Long-Wavelength Gravity Field Recovery from 1s-Sampled Kinematic Orbits Using the Acceleration Approach −8 −8 10 10 max L max degree−RMS (m > 5) −10 degree−RMS ITG−GRACE2010s L = 90 ITG−GRACE2010s EDF(1s) EDF(30s) EDF(1s), orders m > 5 EDF(30s), orders m > 5 10 −12 10 = 110 Lmax = 120 −9 10 EDF(30s), empirical covariances −10 10 −11 −14 10 23 0 20 40 60 80 degree 10 0 20 40 60 80 degree Fig. 1 Model errors: degree RMS obtained by application of EDF(1s) and EDF(30s) to a simulated noise-free GOCE-orbit; the dashed lines are obtained from exclusion of orders m Ä 5 in order to account for the polar gap Fig.

In combined solutions, we find its impact to be insignificant and below noise level. 2 Evaluation of the Striping Error In order to investigate the extent of the striping pattern in temporal gravity field estimates, a global root mean square error (RMSE) method is introduced. The basis for the RMSE is an hypothesized pure striping error which can be obtained by the subtraction of a smoothed GRACE solution (Gaussian smoothing (cf. Wahr and Molenaar 1998) with R D 500 km) of the same period. With this operation all stationary and time-variable gravity signals are eliminated in the respective month and only the (striping) error remains.

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