ESA's gravity field mission GOCE and beyond

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Simulation results: 1 MonthDegree RMSKaula10 -1CHAMP10 -2][m10 -3cross10 0 s h-de gre ealongSwarmradialA-B and A-C10 -4cross + alongGRACE10 -5KBR10 -610 20 30 40 50 60 70IV Hotine-Marussi Symposium, Wuhan 29 May - 2 June 2006
Remarks• Gravity field recovery with Swarm is possible• Continuation of decade of gravity field mappingpossible (but, with reduced accuracy)• Radial component most sensitive at end of mission(but, bad visibility)• Simulation must include full GPS-simulation(visibility)• Realistic error estimates for GPS?• Different analysis methods possible (not necessarilyenergy integral)IV 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 and 24: Swarm and GravityUse of GPS-Baselin
Page 25 and 26: SH-Error CharacteristicsAlong-track
Page 27 and 28: SH-Error Characteristicsfrom Gradie
Page 29: Simulation results: 1 MonthDegree R
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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