ESA's gravity field mission GOCE and beyond

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SSI Mission Control System ElementsThe Linear Motion Control in charge of: satellite formation keeping (relativeposition control) drag-free control for each spacecraftThe Angular Motion Control in charge of: spacecraft angular acceleration,angular rate <strong>and</strong> attitude controlBeam Steering Control in charge of: pointing of the laser beam emittedby satellite 1 to the satellite 2IV Hotine-Marussi Symposium, Wuhan 29 May - 2 June 2006
Future Concepts ?GSP - Mass distribution <strong>and</strong> mass transports inthe Earth system (ITT in prep.)Courtesy: C. BartonIV 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 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: Satellite-satellite distance measur

ESA's gravity field mission GOCE and beyond

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