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51#
發(fā)表于 2025-3-30 09:31:30 | 只看該作者
52#
發(fā)表于 2025-3-30 14:33:30 | 只看該作者
Network Approach versus State-space Approach for Strapdown Inertial Kinematic Gravimetryges but displays a serious disadvantage, namely, its very limited capacity to handle space correlations (like the rigorous treatment of cross-over points). This paper examines an alternative through the well known geodetic approach, where the INS differential mechanization equations are interpreted
53#
發(fā)表于 2025-3-30 17:24:41 | 只看該作者
54#
發(fā)表于 2025-3-30 22:03:46 | 只看該作者
Initial results from retracking and reprocessing the ERS-1 geodetic mission altimetry for gravity fi field modeling close to the coast and in Polar Regions is discussed. Close to the coast and in particular in Polar Regions the use of multiple retrackers leads to considerably more and better data than in the normal 1 Hz data delivered by the European Space Agency (ESA)..Extensive comparison with m
55#
發(fā)表于 2025-3-31 04:24:25 | 只看該作者
Space-borne gravimetry: determination of the time variable gravity fielding (SST) and orbital positions from GPS high-low SST) and retrieved gravity field spherical harmonic expansions. In addition, the aliasing of signals predicted by the ECCO model and the effect of low-low SST observation noise and uncertainties in the recovered orbital positions has been analyzed..I
56#
發(fā)表于 2025-3-31 05:10:09 | 只看該作者
57#
發(fā)表于 2025-3-31 10:01:39 | 只看該作者
58#
發(fā)表于 2025-3-31 15:01:48 | 只看該作者
Stochastic model validation of satellite gravity data: A test with CHAMP pseudo-observationsmum Norm Quadratic Unbiased Estimator (MINQUE) as an alternative for the fast Monte Carlo Maximum Likelihood VCE that we have introduced earlier. In this way, spurious data sets could be indicated and downweighted in the least-squares estimation of the unknown parameters. Using only 299 days of CHAM
59#
發(fā)表于 2025-3-31 17:55:36 | 只看該作者
Analysis of , ,-Perturbed Relative Orbits for Satellite Formation Flyingravity gradient tensor. The resulting . are solved analytically..The orbit simulations show that the analytical solution of the modified . are consistent with their numerically integrated counterpart. Differences with respect to the reference . method remain, which means that not all .. effects have
60#
發(fā)表于 2025-4-1 00:34:37 | 只看該作者
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