Bernese GPS Software Version 5.0 - Bernese GNSS Software

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10. Station Coordinates and Velocities fore, epoch-wise pre-elimination and resubstitution of epoch parameters (description see Section 7.5.6) is preferable for most applications. It is enabled when the option “Pre-Elimination” in panel “GPSEST 5.1” is set to EVERY EPOCH for kinematic coordinates. The way formal errors of kinematic coordinates and normalized residuals are computed in the case of epoch-wise pre-elimination and resubstitution depends on the setting for option “Var-covar wrt epoch parameters” in panel “GPSEST 3.2: General Options 2”. If the option is set to SIMPLIFIED formal errors are computed based on the epoch solution only, with the non-epoch parameters introduced without error. With the option set to CORRECT the formal error is computed correctly but the processing time and memory consumption may become very large. For option SIMPLIFIED it is then preferable to scale normalized residuals with the a priori variance (NORM APRIORI instead of NORMALIZED in option “Type of computed residuals” in panel “GPSEST 3.1: General Options 1”). We refer to Section 7.5.6 for more information. 10.4.3 Program Output and Result File The results of the kinematic coordinate estimation are included in the GPSEST program output. An example is given in the left hand panel of Figure 10.6. The first line gives the a priori coordinates for the station (degrees, minutes, and seconds of arc for latitude and longitude, meters for height) as it is given in the input static coordinate file. For each epoch one line is printed containing the following information: EPO : Epoch number. EPOCH (MJD): Epoch of the kinematic position in modified Julian date. #OBS: Number of observations that contributed to the epoch parameter (observations from different baselines are counted separately). STA : First four characters of the station name. CORRECTION AND RMS IN METER: Estimated correction and formal error in north, east, and up components in meters. The corrections refer to the a priori coordinates used. ESTIMATED POSITION WRT. FIXED COORD.: Estimated trajectory in north, east, and up components in meters. The columns contain the difference between the position estimated for the particular epoch and the constant coordinate from the coordinate input file. The output for different kinematic stations is separated by a blank line. A minimum number of observations contributing to the kinematic position of an epoch can be defined in panel “GPSEST 6.5: Kinematic Coordinates”. If less observations are available the corresponding value is labeled with the flag S instead of flag K in the kinematic result file and is marked in the program output by an asterisk in the column containing the number of observations. The program output section looks slightly different for LEOs (see the right hand example in Figure 10.6). In that case only the estimated corrections in the X,Y,Z-components in the Earth-fixed system are printed together with their formal error. Page 228 AIUB
Bernese GPS Software Version 5.0 Page 229 Figure 10.6: GPSEST program output for the estimation of kinematic coordinates (left: terrestrial station, right: LEO). KINEMATIC COORDINATES: ${P}/EXAMPLE/STA/K1_03138.KIN --------------------- EPO: EPOCHS SINCE 2003-05-18 10:00:00 (SAMPLING 300 SEC) CORRECTION AND RMS IN METER ESTIMATED POSITION WRT. FIXED COORD. EPO EPOCH(MJD) #OBS STA LATITUDE LONGITUDE HEIGHT NORTH(M) EAST(M) UP(M) ----------------------------------------------------------------------------------------------------------------------------------- PTBB 14234M001 52 17 46.280644 10 27 35.085144 130.2259 1 52777.416667 7 PTBB -0.0400 +- 0.053 0.0912 +- 0.043 0.0025 +- 0.093 -0.0400 0.0912 0.0025 2 52777.420139 7 PTBB -0.0434 +- 0.052 0.0871 +- 0.044 -0.0236 +- 0.090 -0.0434 0.0871 -0.0236 3 52777.423611 7 PTBB -0.0615 +- 0.051 0.0866 +- 0.045 -0.0157 +- 0.088 -0.0615 0.0866 -0.0157 4 52777.427083 5 * PTBB -0.0374 +- 0.050 0.0857 +- 0.046 -0.0335 +- 0.081 -0.0374 0.0857 -0.0335 5 52777.430556 6 PTBB -0.0334 +- 0.050 0.0960 +- 0.049 -0.0349 +- 0.078 -0.0334 0.0960 -0.0349 6 52777.434028 6 PTBB -0.0282 +- 0.049 0.0938 +- 0.050 -0.0040 +- 0.073 -0.0282 0.0938 -0.0040 ... KINEMATIC COORDINATES: ${K}/GRACE/STA/ZK104141.KIN --------------------- EPO: EPOCHS SINCE 2004-05-19 21:00:00 (SAMPLING 30 SEC) CORRECTION AND RMS IN METER ESTIMATED POSITION WRT. FIXED COORD. EPO EPOCH(MJD) #OBS STA LATITUDE LONGITUDE HEIGHT NORTH(M) EAST(M) UP(M) ----------------------------------------------------------------------------------------------------------------------------------- 1 53144.875000 8 GRCA L09 -0.046 +- 0.006 0.047 +- 0.006 0.078 +- 0.027 LEO Earth-fixed XYZ 2 53144.875347 8 GRCA L09 -0.046 +- 0.006 0.046 +- 0.006 0.094 +- 0.027 LEO Earth-fixed XYZ 3 53144.875694 8 GRCA L09 -0.048 +- 0.006 0.046 +- 0.006 0.084 +- 0.027 LEO Earth-fixed XYZ 4 53144.876042 8 GRCA L09 -0.042 +- 0.006 0.053 +- 0.006 0.005 +- 0.027 LEO Earth-fixed XYZ 5 53144.876389 8 GRCA L09 -0.048 +- 0.006 0.047 +- 0.006 0.048 +- 0.027 LEO Earth-fixed XYZ 6 53144.876736 8 GRCA L09 -0.048 +- 0.006 0.044 +- 0.006 0.024 +- 0.027 LEO Earth-fixed XYZ ... 10.4 Estimating Kinematic Coordinates
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Bernese GPS Software Version 5.0 Ed
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Bernese GPS Software Version 5.0 As
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Contents 2.3.6.1 Ionosphere-Free Li
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Contents 6.3.3 Kinematic Stations .
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Contents 9.4.4 Pre-Elimination Opti
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Contents 13.2 How to Correct P1-P2
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Contents 18.3.2 Command Bar . . . .
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Contents 20.4 Description of the Pr
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Contents 22.8.2 Station Abbreviatio
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Contents Page XVI AIUB
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List of Figures 5.1 Flow diagram of
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List of Figures 13.3 P1-C1 code bia
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List of Figures 22.20 Tabular orbit
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List of Tables 12.2 Influences of t
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1. Introduction and Overview • bu
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1. Introduction and Overview Table
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1. Introduction and Overview • Th
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1. Introduction and Overview The Be
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1. Introduction and Overview for Ca
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2. Fundamentals 2.1.1 GPS System De
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2. Fundamentals Table 2.2: Componen
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2. Fundamentals Clock correction [n
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2. Fundamentals Figure 2.5: GLONASS
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2. Fundamentals Table 2.6: GLONASS
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2. Fundamentals In contrast to the
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2. Fundamentals 2.2 GNSS Satellite
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2. Fundamentals 2.2.2.1 The Kepleri
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2. Fundamentals Table 2.9: Perturbi
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2. Fundamentals R.A. of Ascending N
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2. Fundamentals where aROCK is the
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2. Fundamentals By taking the deriv
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2. Fundamentals δi error of satell
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2. Fundamentals Ionospheric refract
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2. Fundamentals 2.3.6.1 Ionosphere-
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2. Fundamentals Table 2.10: Linear
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3. Campaign Setup variable to the f
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3. Campaign Setup Figure 3.1: Examp
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3. Campaign Setup In this section w
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3. Campaign Setup 3.5 Processing Ov
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4. Import and Export of External Fi
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5. Preparation of Earth Orientation
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6. Data Preprocessing Preprocessing
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6. Data Preprocessing (a) AS turned
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6. Data Preprocessing 6.2.4 Code Sm
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6. Data Preprocessing is set to 2.
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6. Data Preprocessing 6.3.2 Preproc
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6. Data Preprocessing RMS of kin. s
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6. Data Preprocessing The ambiguiti
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6. Data Preprocessing no loss of si
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6. Data Preprocessing This epoch-di
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6. Data Preprocessing result in lar
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6. Data Preprocessing (e.g., from C
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6. Data Preprocessing The second pa
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6. Data Preprocessing GAR small pie
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6. Data Preprocessing -------------
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6. Data Preprocessing automated pro
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6. Data Preprocessing 6.6.2 Generat
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6. Data Preprocessing 6.6.3 Detect
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6. Data Preprocessing (6) If the to
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7. Parameter Estimation p u × 1 ve
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7. Parameter Estimation The two bas
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7. Parameter Estimation contains a
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7. Parameter Estimation The binary
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7. Parameter Estimation 7.5.2 Piece
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7. Parameter Estimation The equatio
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7. Parameter Estimation 7.5.4.4 Fix
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7. Parameter Estimation where Q 11
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7. Parameter Estimation consequence
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7. Parameter Estimation are address
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7. Parameter Estimation ... ! Pre-p
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7. Parameter Estimation The RINEX m
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7. Parameter Estimation In a succes
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7. Parameter Estimation Page 166 AI
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8. Initial Phase Ambiguities and Am
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12. Ionosphere Modeling and Estimat
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13. Differential Code Biases Promin
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13. Differential Code Biases Figure
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13. Differential Code Biases Figure
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13. Differential Code Biases ======
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13. Differential Code Biases Page 2
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14. Clock Estimation τ (BRUS-PTBB)
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14. Clock Estimation Here the limit
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14. Clock Estimation to zero. All c
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14. Clock Estimation #OBS : Number
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14. Clock Estimation 14.3 Clock RIN
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14. Clock Estimation cessed if CCRN
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14. Clock Estimation RINEX files th
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14. Clock Estimation the clock valu
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14. Clock Estimation SINGLE POINT P
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14. Clock Estimation Page 308 AIUB
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15. Estimation of Satellite Orbits
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16. Antenna Phase Center Offsets an
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17. Data Simulation Tool GPSSIM 17.
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17. Data Simulation Tool GPSSIM The
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17. Data Simulation Tool GPSSIM The
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17. Data Simulation Tool GPSSIM Res
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18. The Menu System 18.2 Starting t
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18. The Menu System 18.3.1 Menu Bar
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18. The Menu System 18.3.5 Panel Co
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18. The Menu System the menu the ne
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18. The Menu System Table 18.1: Pre
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18. The Menu System 18.5.3 System E
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18. The Menu System 18.7 Change Opt
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18. The Menu System 18.9 Technical
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18. The Menu System ... ! Environme
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18. The Menu System The keyword ENV
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18. The Menu System ! List of Remai
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18. The Menu System The MENUAUX-mec
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18. The Menu System Keyword values
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19. Bernese Processing Engine (BPE)
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20. Processing Examples inspect the
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20. Processing Examples 20.3.1 How
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20. Processing Examples • (option
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20. Processing Examples PID 111 PRE
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20. Processing Examples 20.4.1.4 Co
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20. Processing Examples 20.4.1.5 Ta
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20. Processing Examples 20.4.1.7 Cr
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20. Processing Examples 20.4.2.1 Co
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20. Processing Examples appears in
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20. Processing Examples PID 313 MPR
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20. Processing Examples Further rea
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20. Processing Examples # # Create
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20. Processing Examples PID 101 GPS
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20. Processing Examples The RINEX n
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20. Processing Examples # # Preproc
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20. Processing Examples the loop, d
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20. Processing Examples PID 903 CLK
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20. Processing Examples and IGS 00B
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20. Processing Examples • Save th
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20. Processing Examples PID 321 GPS
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20. Processing Examples PID 301 CLK
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21. Program Structure $C / %C% PGM
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21. Program Structure (program GPSE
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21. Program Structure continued fro
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21. Program Structure continued fro
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21. Program Structure ! -----------
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22. Data Structure "Program" Area $
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22. Data Structure Table 22.1: List
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22. Data Structure 22.4.2 Geodetic
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22. Data Structure 22.4.4 Antenna P
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Page 484 AIUB ANTENNA PHASE CENTER
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22. Data Structure 22.4.5 Satellite
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22. Data Structure 22.4.6 Satellite
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22. Data Structure DIFFERENCE OF GP
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22. Data Structure 22.4.9 Subdaily
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22. Data Structure EGM96 EGM96, VER
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22. Data Structure SINEX : OPTION I
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22. Data Structure 22.4.16 Panel Up
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22. Data Structure 22.6.2 Header an
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22. Data Structure 15 Antenna type(
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22. Data Structure SVN-NUMBER= 2 ME
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22. Data Structure -1 2 1 5 TITLE :
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22. Data Structure Used by: ORBGEN
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22. Data Structure 53064.00 53065.0
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22. Data Structure CODE’S MONTHLY
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22. Data Structure Table 22.4: Stat
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22. Data Structure (3) TYPE 003: HA
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22. Data Structure 22.8.4 Station P
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22. Data Structure Remarks: • Eac
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22. Data Structure The following st
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22. Data Structure Table 22.7: List
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22. Data Structure AJAC $$ FES2004
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22. Data Structure Station sigma fi
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22. Data Structure GOPE 11502M002 Z
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22. Data Structure 22.8.18 Receiver
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22. Data Structure CODE RAPID 3-DAY
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22. Data Structure 22.9.3 Meteo and
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22. Data Structure IONOSPHERE MODEL
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22. Data Structure 22.10 Miscellane
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22. Data Structure 22.10.4 Variance
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22. Data Structure 22.10.5 Normal E
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22. Data Structure 22.10.7 Observat
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22. Data Structure Created by: Each
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22. Data Structure ----------------
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22. Data Structure 22.10.17 BPE log
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23. Installation Guide 23.1.2 Conte
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23. Installation Guide 23.1.3.2 Ins
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23. Installation Guide BERN50 : $C
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23. Installation Guide If you have
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23. Installation Guide To make the
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23. Installation Guide List of Inst
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23. Installation Guide 23.2.4 Confi
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23. Installation Guide Configure me
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23. Installation Guide ${P}/EXAMPLE
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23. Installation Guide To recompile
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23. Installation Guide Page 574 AIU
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24. The Step from Version 4.2 to Ve
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BIBLIOGRAPHY Bock, H. (2004), Effic
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BIBLIOGRAPHY Janes, H. W., R. B. La
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BIBLIOGRAPHY Schaer, S. (1998), COD
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BIBLIOGRAPHY Page 588 AIUB
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INDEX OF PROGRAMS NEQ2ASC, 207, 541
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Index of Program Panels CODSPP 2: I
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Index of Program Panels MKCLUS 3: R
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INDEX OF KEYWORDS Antenna verificat
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INDEX OF KEYWORDS Cluster definitio
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INDEX OF KEYWORDS variance-covarian
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INDEX OF KEYWORDS orbit products, 1
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INDEX OF KEYWORDS Multi-session sol
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INDEX OF KEYWORDS Orbital elements
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INDEX OF KEYWORDS Receiver antenna
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INDEX OF KEYWORDS orbit modeling, 9
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INDEX OF KEYWORDS WGS-84, 19, 88, 2
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