ESA's gravity field mission GOCE and beyond

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GPS inter-satellite baseline test: GRACEHigh-pass filtered GRACE inter-satellite rangingFrom KBRFrom GPSEmpirical rangeerrors(GPS vs. KBR)σσσalongcrossradial===2.12.02.7mmmmmmExpected rangerateaccuracy:σ ≈10 −2mm/sIV Hotine-Marussi Symposium, Wuhan 29 May - 2 June 2006
SH-Error CharacteristicsAlong-track simulations vs. real data (GRACE)(1)Inclination functionsCovariance Matrix(2)error propagationEnergy integralEIGEN-GRACE02s (GFZ)full simulationIV Hotine-Marussi Symposium, Wuhan 29 May - 2 June 2006
Page 1 and 2: ESA’s gravity field missionGOCE a
Page 3 and 4: ESA’s Living Planet ProgrammeLivi
Page 5 and 6: • ESA’s Living Planet Programme
Page 7 and 8: Mission Requirements• To determin
Page 9 and 10: High-Level Processing FacilityAIUB:
Page 11 and 12: Main Technical Challenges Highest s
Page 13 and 14: Gradiometer Structural ModelIV Hoti
Page 15 and 16: Consequence of Launch DelayLaunch i
Page 17 and 18: Meetings and Studies• 3 rd Intern
Page 19 and 20: • ESA’s Living Planet Programme
Page 21 and 22: Swarm Satellite & ConstellationAcce
Page 23: Swarm and GravityUse of GPS-Baselin
Page 27 and 28: SH-Error Characteristicsfrom Gradie
Page 29 and 30: Simulation results: 1 MonthDegree R
Page 31 and 32: Remarks• Gravity field recovery w
Page 33 and 34: Studies Recently Performed• Gravi
Page 35 and 36: Measurement and control elements of
Page 37 and 38: Satellite-satellite distance measur
Page 39: Future Concepts ?GSP - Mass distrib

ESA's gravity field mission GOCE and beyond

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