GRACE-A and GRACE-B together

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Ambiguity resolution with GRACE baseline Total number of ambiguities, mean= 416 FGS Workshop 2004, Höllenstein/Wettzell, October 27 - 29, 2004 Resolved narrow-lane ambiguities using kinematic bootstrapping, mean= 93.6% Day of year Day of year Resolved wide-lane ambiguities (Melbourne-Wübbena), mean= 98.4% Day of year Resolved narrow-lane ambiguities using dynamic bootstrapping, mean= 92.8% Day of year
Zero-difference orbits (like two CHAMP satellites) GRACE Formation Flying Zero-differences versus combined zero&double-difference reduced-dyn. orbits, validation with KBR FGS Workshop 2004, Höllenstein/Wettzell, October 27 - 29, 2004 Float ambiguities (GRACE-A and GRACE-B together) RMS=15.7 mm RMS=11.6 mm Time in hours RMS=2.8 mm Time in hours Time in hours Fixed ambiguities (GRACE-A and GRACE-B together)
Page 1 and 2: Kinematic and Dynamic Orbit Determi
Page 3 and 4: FGS Workshop 2004, Höllenstein/Wet
Page 7 and 8: GPS Phase Clocks FGS Workshop 2004,
Page 9 and 10: Kinematic Positioning and Gravity F
Page 11 and 12: Daily RMS difference between kinema
Page 17: POD Strategies for LEO Formation Fl
Page 21 and 22: Validation with KBR Reduced-Dynamic
Page 23 and 24: Combined GPS/KBR Baseline Impact of

GRACE-A and GRACE-B together

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