2014
DOI: 10.1016/j.asr.2013.11.031
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Gravity field models from kinematic orbits of CHAMP, GRACE and GOCE satellites

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Cited by 30 publications
(23 citation statements)
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“…We estimated the drag coefficient of each satellite by means of the long-term change in the orbital elements in order to consider realistic values. Further details of our approach can be found in Bezděk (2010); Bezděk et al (2014Bezděk et al ( , 2016Bezděk et al ( , 2017.…”
Section: Non-gravitational Accelerationsmentioning
confidence: 99%
“…We estimated the drag coefficient of each satellite by means of the long-term change in the orbital elements in order to consider realistic values. Further details of our approach can be found in Bezděk (2010); Bezděk et al (2014Bezděk et al ( , 2016Bezděk et al ( , 2017.…”
Section: Non-gravitational Accelerationsmentioning
confidence: 99%
“…Alternative data sets used in this study are models based on GRACE and Swarm satellite orbits, developed by ASU CAS [7,9], accessed from http://www.asu.cas.cz/~{}bezdek/vyzkum/geopotencial/ index.php.…”
Section: Gravity Field Models Obtained From Kinematic Orbits Of the Lmentioning
confidence: 99%
“…Surprisingly, these good results were not found for the Swarm ABC ITSG solutions. The reason for these differences may be the fact that both institutes used different approaches during computation of their gravity field models, namely the acceleration approach [7] for CAS solution and the short-arc approach [54] for ITSG solutions. The series computed from Jason 2, MetOp-A, and MetOp-B data revealed much higher STDs of χ 1 and χ 2 than reference data and other missions.…”
Section: Time Series and Trendsmentioning
confidence: 99%
“…In case of combination of the first and second derivatives (the last row in Table 2), we can see the solution keeps the sensitivity of the former. Holmes and Featherstone (2002) using the acceleration approach (Bezděk et al 2012).…”
Section: Effect Of the Normal For Other Functionalsmentioning
confidence: 99%