Bernese GNSS Software Version 5.2 Tutorial

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7 Additional Examples6 96 0.003 0.003 0.003 0.003 0.004 0.008 0.006 0.0077 96 0.002 0.002 0.002 0.002 0.002 0.005 0.004 0.0048 96 0.002 0.002 0.001 0.001 0.002 0.003 0.003 0.0069 96 0.002 0.002 0.002 0.001 0.003 0.004 0.003 0.00610 96 0.002 0.002 0.002 0.002 0.003 0.006 0.005 0.00511 96 0.002 0.002 0.001 0.001 0.002 0.004 0.003 0.00712 96 0.003 0.003 0.003 0.002 0.003 0.007 0.005 0.00613 96 0.003 0.003 0.003 0.002 0.003 0.013 0.006 0.00614 96 0.003 0.003 0.004 0.003 0.002 0.011 0.006 0.00915 96 0.002 0.002 0.002 0.002 0.002 0.009 0.004 0.00516 96 0.004 0.003 0.004 0.003 0.004 0.007 0.008 0.00817 96 0.002 0.002 0.002 0.002 0.002 0.005 0.004 0.00718 96 0.003 0.002 0.002 0.002 0.003 0.006 0.004 0.00719 96 0.002 0.002 0.002 0.002 0.003 0.005 0.004 0.00520 96 0.002 0.002 0.002 0.001 0.003 0.004 0.003 0.00621 96 0.002 0.002 0.001 0.001 0.003 0.003 0.002 0.00622 96 0.003 0.003 0.003 0.002 0.003 0.005 0.005 0.00623 96 0.003 0.003 0.003 0.002 0.003 0.011 0.005 0.00524 96 0.001 0.001 0.001 0.001 0.002 0.003 0.002 0.00525 96 0.002 0.002 0.002 0.001 0.003 0.004 0.004 0.00726 96 0.004 0.003 0.005 0.003 0.003 0.010 0.006 0.00527 96 0.002 0.002 0.002 0.001 0.003 0.004 0.002 0.00628 96 0.002 0.002 0.002 0.002 0.002 0.004 0.005 0.00729 96 0.003 0.003 0.003 0.003 0.003 0.005 0.006 0.00730 96 0.002 0.002 0.002 0.002 0.002 0.006 0.005 0.00531 96 0.002 0.002 0.002 0.002 0.003 0.005 0.005 0.00932 96 0.002 0.002 0.002 0.001 0.003 0.005 0.003 0.006101 96 0.002 0.002 0.002 0.002 0.002 0.006 0.004 0.007102 96 0.002 0.002 0.002 0.002 0.002 0.006 0.005 0.005103 96 0.002 0.002 0.002 0.001 0.002 0.005 0.005 0.006104 96 0.002 0.001 0.002 0.001 0.002 0.004 0.003 0.004105 96 0.001 0.001 0.001 0.001 0.002 0.002 0.007 0.004107 96 0.002 0.002 0.001 0.001 0.002 0.003 0.006 0.005108 96 0.002 0.002 0.002 0.001 0.002 0.005 0.003 0.004110 96 0.002 0.002 0.001 0.001 0.003 0.007 0.003 0.005111 96 0.001 0.001 0.001 0.001 0.002 0.003 0.010 0.006113 96 0.002 0.002 0.002 0.001 0.002 0.004 0.005 0.005114 96 0.002 0.002 0.002 0.002 0.002 0.005 0.012 0.003115 96 0.002 0.002 0.002 0.001 0.002 0.003 0.008 0.004117 96 0.002 0.002 0.003 0.002 0.002 0.010 0.009 0.003118 96 0.002 0.002 0.002 0.001 0.002 0.005 0.006 0.006119 96 0.003 0.002 0.002 0.002 0.003 0.005 0.006 0.006120 96 0.002 0.002 0.002 0.001 0.003 0.004 0.004 0.006121 96 0.002 0.002 0.002 0.002 0.003 0.006 0.004 0.014122 96 0.002 0.002 0.002 0.002 0.002 0.004 0.006 0.004123 96 0.002 0.002 0.001 0.001 0.002 0.003 0.004 0.004124 96 0.002 0.002 0.001 0.002 0.001 0.003 0.017 0.003-------------------------------------------------------------------------------...The RMS error for the orbit fit for precise IGS orbits should be below 5 mm (for olderorbits it may also achieve 10. . . 15 mm).The file ${P}/INTRO/OUT/IGS10207.LST contains the same results as displayed on page 25but contains also the GLONASS satellite orbits:EXAMPLE: Session 102070: Standard orbit generation 10-JAN-14 18:28TIME FROM DAY : 1 GPS WEEK: 1594TO DAY : 2 GPS WEEK: 1594-------------------------------------------------------------------------------ORBIT REPEATABILITY FROM A 1-DAY FIT THROUGH DAILY ORBIT SOLUTIONS (MM)# ECLIPSING SATELLITES: 5 E / 0 M ( 0 EM)----------------------------- ... ---------------------- ... ---------------------------- ...ECL .. .. .. .. .. .. .. E. E. E. .. .. .. .. .. .. .. ..DOY 1 2 3 4 5 6 ... 12 13 14 15 16 ... 32 101 102 103 104 105 107 ...----------------------------- ... ---------------------- ... ---------------------------- ...207 2 1 4 1 2 3 ... 3 3 3 2 3 ... 2 2 2 2 1 1 2 ...----------------------------- ... ---------------------- ... ---------------------------- ...ALL 2 1 4 1 2 3 ... 3 3 3 2 3 ... 2 2 2 2 1 1 2 ...----------------------------- ... ---------------------- ... ---------------------------- ...If you want to use these orbit files in the processing programs, you simply have to replacethe CODE–related by the IGS–related filenames for the standard orbit and EOPfiles.Page 106AIUB
7.2 Kinematic Positioning7.2 Kinematic Positioning7.2.1 Estimating Kinematic Positions in a Double–Difference SolutionThe example campaign contains no really roving stations. You can, however, define oneof them to be kinematic (e.g., station GANP). Introduce the coordinates from the finalsolution (\$\{P\}/INTRO/STA/FIN10207.CRD) for all other sites.Remove the name of the resulting “Normal equations” file in panel “GPSEST 2.1: Output Files 1”if there is any entry in this input field. Store the kinematic coordinates in an output file(“Kinematic coordinates” in panel “GPSEST 2.2: Output Files 2”).Bernese GNSS Software, Version 5.2 Page 107
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Bernese GNSS Software Version 5.2 Tutorial

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