GOCE orbit analysis: Long-wavelength gravity field determination using the acceleration approach

被引:14
|
作者
Baur, O. [1 ]
Reubelt, T. [2 ]
Weigelt, M. [2 ]
Roth, M. [2 ]
Sneeuw, N. [2 ]
机构
[1] Austrian Acad Sci, Space Res Inst, A-8042 Graz, Austria
[2] Univ Stuttgart, Inst Geodesy, D-70174 Stuttgart, Germany
关键词
Kinematic positions; GOCE; GPS; Numerical differentiation; Empirical covariance function; Gravity field; POLAR GAP; SATELLITE; RECOVERY; CHAMP; SERIES;
D O I
10.1016/j.asr.2012.04.022
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The restricted sensitivity of the Gravity field and steady-state Ocean Circulation Explorer (GOCE) gradiometer instrument requires satellite gravity gradiometry to be supplemented by orbit analysis in order to resolve long-wavelength features of the geopotential. For the hitherto published releases of the GOCE time-wise (TIM) and GOCE space-wise gravity field series-two of the official ESA products-the energy conservation method has been adopted to exploit GPS-based satellite-to-satellite tracking information. On the other hand, gravity field recovery from data collected by the CHAllenging Mini-satellite Payload (CHAMP) satellite showed the energy conservation principle to be a sub-optimal choice. For this reason, we propose to estimate the low-frequency part of the gravity field by the point-wise solution of Newton's equation of motion, also known as the acceleration approach. This approach balances the gravitational vector with satellite accelerations, and hence is characterized by (second-order) numerical differentiation of the kinematic orbit. In order to apply the method to GOCE, we present tailored processing strategies with regard to low-pass filtering, variance-covariance information handling, and robust parameter estimation. By comparison of our GIWF solutions (initials GI for "Geodatisches Institut" and IWF for "Institut fur WeltraumForschung") and the GOCE-TIM estimates with a state-of-the-art gravity field solution derived from GRACE (Gravity Recovery And Climate Experiment), we conclude that the acceleration approach is better suited for GOCE-only gravity field determination as opposed to the energy conservation method. (c) 2012 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:385 / 396
页数:12
相关论文
共 50 条
  • [1] GOCE Long-Wavelength Gravity Field Recovery from 1s-Sampled Kinematic Orbits Using the Acceleration Approach
    Reubelt, T.
    Baur, O.
    Weigelt, M.
    Roth, M.
    Sneeuw, N.
    [J]. GRAVITY, GEOID AND HEIGHT SYSTEMS, 2014, 141 : 21 - 26
  • [2] Exploring gravity field determination from orbit perturbations of the European Gravity Mission GOCE
    P. N. A. M. Visser
    J. van den IJssel
    R. Koop
    R. Klees
    [J]. Journal of Geodesy, 2001, 75 : 89 - 98
  • [3] Exploring gravity field determination from orbit perturbations of the European Gravity Mission GOCE
    Visser, PNAM
    van den IJssel, J
    Koop, R
    Klees, R
    [J]. JOURNAL OF GEODESY, 2001, 75 (2-3) : 89 - 98
  • [4] Precise orbit determination and the earth gravity field recovery by acceleration approach for Swarm
    Zhang B.
    [J]. Cehui Xuebao/Acta Geodaetica et Cartographica Sinica, 2019, 48 (08): : 1068
  • [5] Gravity field determination with GOCE and GRACE
    [J]. Adv Space Res, 4 (771-776):
  • [6] The continental tectosphere and Earth's long-wavelength gravity field
    Shapiro, SS
    Hager, BH
    Jordan, TH
    [J]. LITHOS, 1999, 48 (1-4) : 135 - 152
  • [7] Application of Gravity Gradients in the Process of GOCE Orbit Determination
    Bobojc, Andrzej
    [J]. ACTA GEOPHYSICA, 2016, 64 (02): : 521 - 540
  • [8] Application of Gravity Gradients in the Process of GOCE Orbit Determination
    Andrzej Bobojć
    [J]. Acta Geophysica, 2016, 64 : 521 - 540
  • [9] Gravity field determination with GOCE and GRACE
    Visser, PNAM
    [J]. SATELLITE DYNAMICS, ORBIT ANALYSIS AND COMBINATION OF SPACE TECHNIQUES, 1999, 23 (04): : 771 - 776
  • [10] Long-wavelength lunar gravity field recovery from simulated orbit and inter-satellite tracking data
    Yan, Jianguo
    Baur, Oliver
    Fei, Li
    Ping Jinsong
    [J]. ADVANCES IN SPACE RESEARCH, 2013, 52 (11) : 1919 - 1928