Mission design, operation and exploitation of the gravity field and steady-state ocean circulation explorer mission
By R. Floberghagen, M. Fehringer, D. Lamarre, D. Muzi, B. Frommknecht, Christoph Steiger, J. Piñeiro, Andrea da Costa. 2011
258 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Molecular Biology, Oceanography
View Paper: https://www.semanticscholar.org/paper/7e7b1825977bfd3eb9f4047a5e864736f870926b
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In Aerospace Engineering
In Molecular Biology
In Oceanography
- S. Mulet
- J. Brockmann
- E. Höck
- Torsten Mayer-Gürr
- Roland Pail
- Sean Bruinsma
- Sylvain Bonvalot
- Wolf-Dieter Schuh
Citations in the corpus
- GOCE gravitational gradiometry (2011, background): “Each accelerometer is ultra-precise along two orthogonal directions but much less sensitive along its third axis (see also Floberghagen et al. 2011).”
- ESA's satellite‐only gravity field model via the direct approach based on all GOCE data (2014, methodology): “GOCE was equipped with a triaxial gravity gradiometer, GPS receiver, laser retrore fl ector, star sensors, and an ion propulsion engine with variable thrust to reach these goals [ Floberghagen et al ., 2011].”
- EGM_TIM_RL05: An independent geoid with centimeter accuracy purely based on the GOCE mission (2014, background): “Although the entire satellite acts as the sensor [Floberghagen et al., 2011], the core and unique measurement instrument is a three-axes gradiometer, measuring acceleration differences along baselines of 0.5 m in the gradiometer reference frame (GRF) defined by the orthogonal gradiometer arms [EGG-”