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Orbit determination for the GOCE satellite
Authors:PNAM Visser  J van den IJssel  T Van Helleputte  H Bock  A Jäggi  G Beutler  D Švehla  U Hugentobler  M Heinze
Institution:1. Delft Institute of Earth Observation and Space systems (DEOS), Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS, Delft, The Netherlands;2. Astronomical Institute, University of Bern (AIUB), Sidlerstrasse 5, CH-3012, Bern, Switzerland;3. Institute of Astronomical and Physical Geodesy (IAPG), Technische Universität München, Arcisstrasse 21, 80333, Munich, Germany
Abstract:Precise Orbit Determination (POD) for the Gravity field and steady-state Ocean Circulation Explorer (GOCE), the first core explorer mission by the European Space Agency (ESA), forms an integrated part of the so-called High-Level Processing Facility (HPF). Two POD chains have been set up referred to as quick-look Rapid and Precise Science Orbit determination or RSO and PSO, respectively. These chains make use of different software systems and have latencies of 1 day and 2 weeks, respectively, after tracking data availability. The RSO and PSO solutions have to meet a 3-dimensional (3D) position precision requirement of 50 cm and a few cm, respectively. The tracking data will be collected by the new Lagrange GPS receiver and the predicted characteristics of this receiver have been taken into account during the implementation phase of the two chains.
Keywords:GOCE  High-Level Processing Facility (HPF)  Precise Orbit Determination (POD)  Rapid Science Orbits (RSO)  Precise Science Orbits (PSO)
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