GRACE-A and GRACE-B together

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Baseline Validation with KBR Reduced-Dynamic Orbit Kinematic Orbit Float ambiguities RMS= 15.1 mm RMS= 11.7 mm Time in hours Time in hours RMS= 3.0 mm Time in hours pseudo-stochastic pulses Fixed ambiguities FGS Workshop 2004, Höllenstein/Wettzell, October 27 - 29, 2004 RMS= 6.1 mm Time in hours
Validation with KBR Reduced-Dynamic Orbit Kinematic Orbit Zero-differences RMS= 12.6 mm RMS= 15.0 mm Time in hours Time in hours Kinematic/Reduced-Dynamic Orbit Double-differences fixed ambiguities FGS Workshop 2004, Höllenstein/Wettzell, October 27 - 29, 2004 Reduced-Dynamic Baseline Validation with KBR Day of year Day of year
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 and 18: POD Strategies for LEO Formation Fl
Page 19: Zero-difference orbits (like two CH
Page 23 and 24: Combined GPS/KBR Baseline Impact of

GRACE-A and GRACE-B together

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