Abstract
Monthly gravity field solutions up to d/o 60 are derived by applying the Integrated (one-step) Approach of space geodesy, i.e. by simultaneously processing of the GPS constellation and the twin GRACE satellites. The results are based on latest GRACE RL05 standards (without constraining L3-ambiguities), and consists of 24-h arcs covering the test month April 2008 where the monthly solution was obtained by accumulation of the daily normal equations. The alternative gravity model is compared with the corresponding two-step solution derived by standard two-step GFZ RL05 GRACE processing (including constrained L3-ambiguities). It is shown, that difference degree amplitudes with respect to the static satellite-only model ITG-GRACE2010s for both the Integrated Approach and the two-step solution only differ significantly beyond d/o 17 where the two-step approach still performs slightly better. A great advantage of the Integrated Approach is the largely reduced formal errors indicating higher stochastic significance.
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Acknowledgments
This work was done within project TOBACO-CHAMP/GRACE which was funded within the BMBF R&D-Programme GEOTECHNOLOGIEN with FKZ 03G0728A.
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König , D., Dahle, C. (2014). GRACE Gravity Modeling Using the Integrated Approach. In: Flechtner, F., Sneeuw, N., Schuh, WD. (eds) Observation of the System Earth from Space - CHAMP, GRACE, GOCE and future missions. Advanced Technologies in Earth Sciences. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-32135-1_5
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DOI: https://doi.org/10.1007/978-3-642-32135-1_5
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