Mayer-Gürr, T., Eicker, A., Kurtenbach, E. and Ilk, K.H. (2010) ITG-GRACE: Global Static and Temporal Gravity Field Models from GRACE Data. In: Flechtner, F., Gruber, T., Gntner, A., Mandea, M., Rothacher, M., Schne, T. and Wickert, J., Eds., System Earth via Geodetic-Geophysical Space Techniques, Springer, Berlin, 159-168.
https://doi.org/10.1007/978-3-642-10228-8_13

has been cited by the following article:

• TITLE: Spatio-Temporal Polar-Inclined Space Mission Architecture for a Refined Retrieve of the Earth’s Gravity Field

  AUTHORS: Basem Elsaka

  KEYWORDS: Space Mission Architectures, Orbit Design, Repeat Orbit, Gravity Field Recovery, Full-Scale Simulation

  JOURNAL NAME: World Journal of Engineering and Technology, Vol.7 No.4, November 26, 2019

  ABSTRACT: Future satellite gravity missions (FGMs) have been intensively studied during the last recent years for the era beyond the successful previous GRACE and current GRACE Follow-on satellite missions. Previous studies have investigated the gravity field recovery derived from combined two satellite-pairs (referred here as PI-FGM, a single polar satellite-pair like the GRACE mission combined with another inclined satellite-pair) with different orbital heights of few kilometers and different repeat orbital periods. In this contribution, new innovative idea is introduced by designing the inclined satellite-pair of the FGM at the same orbital height of the polar-type with shifted spatio-temporal (ST-FGM) orbital parameters to avoid any possible collision risk between the two satellite-pairs, polar and inclined, of the FGM architecture. The repeat orbits issue will be taken into consideration through the manuscript and will be set as identical as possible for a fair comparison. The findings through a full-scale simulation analysis show that the new design of shifted spatio-temporal polar-inclined (ST-FGM) mission architecture basically outperforms the two satellite-pairs having different orbital heights (i.e. the PI-FGM mission configuration). Regarding the gravity field recovery, the ST-FGM architecture retrieves the geoid heights with standard deviations of about 17.0 mm providing more isotropic error distribution. An overall improvement by a factor of about 80 and 60 is provided by the ST-FGM and PI-FGM mission architectures, respectively, with respect to the GRACE-like formation and a factor of about 2.4 and 1.8, respectively, with respect to the smoothed gravity solution using the Gaussian filter at radius 400 km. Therefore, the shifted spatio-temporal polar-inclined (ST-FGM) is worthy recommended as stable mission architecture and would be considered as one of the future gravity missions.