Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure 53064.00 53065.00 0.0164 0.0074 0.0082 0.0009 0.0009 0.0014 53065.00 53066.00 0.0203 0.0051 0.0180 0.0009 0.0009 0.0014 53066.00 53067.00 0.0101 0.0032 0.0065 0.0009 0.0009 0.0013 53067.00 53068.00 0.0148 0.0110 0.0089 0.0009 0.0009 0.0013 53068.00 53069.00 0.0172 0.0152 0.0057 0.0010 0.0010 0.0014 53069.00 53070.00 0.0143 0.0077 0.0136 0.0009 0.0009 0.0013 53070.00 53071.00 0.0127 0.0112 0.0063 0.0009 0.0009 0.0012 53071.00 53072.00 0.0128 0.0151 0.0096 0.0009 0.0009 0.0012 22.7.9 Geocenter Coordinates Figure 22.25: Geocenter coordinates (GCC file). Type: ASCII Directory: Campaign-specific directory ORB. Extension: GCC Content: Geocenter coordinates. Created by: ADDNEQ2 (”Menu>Processing>Normal equation stacking”). Used by: ADDNEQ2. Example: Figure 22.25 and ${X}/DOC/EXAMPLE.GCC. The file contains estimated geocenter coordinates in x, y, z (columns 3-5) together with formal errors (columns 6-8) in meters for time intervals (MJD, columns 1-2) as estimated by ADDNEQ2 (see Section 15.4.4). In general it makes only sense to estimate geocenter coordinates when improving orbits in a global solution and applying a no-net rotation and no-net translation constraint. The results then give the coordinates of the geocenter as sensed by the satellite orbits with respect to the origin of the terrestrial reference frame in which the fiducial stations are defined. 22.7.10 Satellite Clock Coefficients Type: ASCII Directory: Campaign-specific directory ORB. Extension: CLK Content: Satellite clock parameters (extracted from broadcast messages, precise orbit files, or Clock RINEX files). Created by: SATCLK (”Menu>Orbits/EOP>Broadcast orbits>Extract satellite clocks”) for extraction from broadcast file, CCRNXC (”Menu>RINEX>RINEX utilities>Combine/manipulate clock data”) for extraction from Clock RINEX, PRETAB (”Menu>Orbits/EOP>Create tabular orbits”) for extraction from precise ephemerides, GPSEST (”Menu>Processing >Parameter estimation”), and CLKEST from estimation, CODSPP (”Menu>Processing >Code-based clock synchronization”) for correcting GLONASS satellite clock offsets to GPS time. Used by: CODSPP (”Menu>Processing>Code-based clock synchronization”), MAUPRP (”Menu >Processing>Phase preprocessing”), GPSEST (”Menu>Processing>Parameter estimation”), and CLKEST. Example: Figure 22.26 and ${X}/DOC/EXAMPLE1.CLK. Page 510 AIUB
Remarks: 22.7 Orbit Related Files SATELLITE CLOCKS FROM BROADCAST FILE 07-JAN-04 06:21 -------------------------------------------------------------------------------- SAT WEEK TOC #PAR A0 (SEC) A1 (SEC/SEC) A2 (SEC/SEC**2) 2 1252 172800. 3 -0.251892023D-03 -0.670752343D-11 0.000000000D+00 2 1252 180000. 3 -0.251940452D-03 -0.670752343D-11 0.000000000D+00 ... 2 1252 252000. 3 -0.252443366D-03 -0.682121026D-11 0.000000000D+00 5 1252 172800. 3 0.122361816D-04 0.147792889D-11 0.000000000D+00 ... 124 1252 241200. 2 0.152935050D-04 -0.326291729D-11 Figure 22.26: Satellite clock (CLK) file. • In CODSPP a satellite clock file has to be specified if standard orbits are used as orbit information (no clock information stored in standard orbits). • In MAUPRP and GPSEST this file is used to take into account the satellite clock corrections in the time interval between the measurements of the two receivers of a baseline. It is of importance only if different receiver types are combined that measure at significantly different epochs (> 20 millisec). • Precise high rate clocks are required if MAUPRP is used in the zero-difference mode. • It is also possible to store the clocks of several sessions in one file. • If the number of polynomial coefficients is one (#PAR=1) the clock reading routine does not interpolate for epochs with missing clock values. • Clock RINEX files may contain also receiver clock corrections. This file type is stored in the OUT directory of the campaign (see Section 22.10.1). See Section 5.5 for more information. 22.7.11 Differential Code Biases for Satellites and Receivers Type: ASCII Directory: Campaign-specific directory ORB. Extension: DCB Content: Differential P1-P2 and P1-C1 code bias (DCB) values for GPS/GLONASS satellites and receivers. Created by: GPSEST (”Menu>Processing>Parameter estimation”) and ADDNEQ2 (”Menu>Processing >Normal equation stacking”). Used by: CODSPP (”Menu>Processing>Code-based clock synchronization”), GPSEST, ADDNEQ2, GPSSIM (”Menu>Service>Generate simulated observation data”). Example: Figure 22.27 and ${X}/DOC/EXAMPLE.DCB. GPS-related DCB values are indicated by a leading “G”, GLONASS-related values by a leading “R”. If such an indicator is missing (e. g., in old CODE P1-P2 DCB files), the DCB information is assumed to be GPS-related. In case of GPS/GLONASS-combined receivers, two receiver-specific bias values are provided, one related to GPS and one related to Bernese GPS Software Version 5.0 Page 511
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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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6. Data Preprocessing Page 138 AIUB
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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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9. Combination of Solutions 9.2 Seq
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9. Combination of Solutions Substit
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9. Combination of Solutions We may
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9. Combination of Solutions files a
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9. Combination of Solutions x x 1 t
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9. Combination of Solutions Both re
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9. Combination of Solutions 9.4 The
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9. Combination of Solutions 9.4.2 G
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9. Combination of Solutions Excepti
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9. Combination of Solutions As alre
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9. Combination of Solutions Table 9
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9. Combination of Solutions The poi
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9. Combination of Solutions (2) Tra
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9. Combination of Solutions Step 1:
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10. Station Coordinates and Velocit
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Page 220 AIUB Station coordinates a
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11. Troposphere Modeling and Estima
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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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Page 494 and 495: 21. Program Structure $C / %C% PGM
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Page 504 and 505: 22. Data Structure "Program" Area $
Page 506 and 507: 22. Data Structure Table 22.1: List
Page 508 and 509: 22. Data Structure 22.4.2 Geodetic
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Page 514 and 515: 22. Data Structure 22.4.5 Satellite
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Page 518 and 519: 22. Data Structure DIFFERENCE OF GP
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Page 522 and 523: 22. Data Structure EGM96 EGM96, VER
Page 524 and 525: 22. Data Structure SINEX : OPTION I
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Page 536 and 537: 22. Data Structure Used by: ORBGEN
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Page 554 and 555: 22. Data Structure AJAC $$ FES2004
Page 556 and 557: 22. Data Structure Station sigma fi
Page 558 and 559: 22. Data Structure GOPE 11502M002 Z
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Page 566 and 567: 22. Data Structure IONOSPHERE MODEL
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Page 580 and 581: 22. Data Structure 22.10.17 BPE log
Page 582 and 583: 23. Installation Guide 23.1.2 Conte
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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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