Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure Used by: ORBGEN (”Menu>Orbits/EOP>Create standard orbits”) in the UPDATE mode and STDPRE (”Menu>Orbits/EOP>Convert standard to precise orbits”) to derive approximated rms values of the orbit quality for each satellite. Example: Figure 22.22: In the example file each arc is characterized by 18 orbital elements (6 Keplerian elements, 9 radiation pressure coefficient parameters, and 3 pseudo-stochastic parameters at the middle of the arc). ${X}/DOC/EXAMPLE.ELE is also available. Information concerning the orbit parameterization is given in Chapter 15. The first column contains the a priori orbital parameters, column 2 and 3 the improved values and their rms. An asterisk “*” indicates that a parameter was not estimated, ORBSYS 2 in the last column defines the orbital system (ORBSYS 1: B1950.0, ORBSYS 2: J2000.0), and the string T950101B characterizes, if present, the a priori model for radiation pressure and the orbit model used (orbit model flag “B”). Pseudo-stochastic orbit parameters are listed at the end of the file. 22.7.7 Pole File in IGS/IERS Format Type: ASCII Directory: Campaign-specific directory ORB. Extension: IEP Content: Pole coordinates, UT1-UTC, and nutation offsets together with statistical information. Created by: Parameter estimation program GPSEST (”Menu>Processing>Parameter estimation”) or ADDNEQ2 (”Menu>Processing>Normal equation stacking”) or by other IGS analysis centers. Used by: Extraction programs POLUPD (”Menu>Orbits/EOP>Handle EOP files>Convert IERS to Bernese format”), POLXTR (”Menu>Orbits/EOP>Handle EOP files>Concatenate IERS pole files”), submission format of Earth rotation parameters for IERS and IGS. Example: Figure 22.23 shows Earth rotation estimates in theIEP format stemming from a 3-days arc. The right-most columns listing the correlations and nutation estimates are not reproduced. ${X}/DOC/EXAMPLE.IEP is also available. This file is only used to send pole, UT1-UTC, and nutation information from global Earth rotation parameter estimations to the IERS Bureau. ERP information is provided in this format by the IGS. Note that starting on GPS week 0966 a new version of the format (version 2) was implemented for all official IGS products in order to get an increased resolution for the polar motion coordinates, their rates, UT/LOD, and their respective sigmas (see IGSMAIL #1943). The reading routines in the Bernese GPS Software read the old and the new format (together with about 13 different pole fileformats). Files from external sources have the extension ERP. In order to avoid confusion with Bernese ERP files rename external files to names with extension IEP. Page 508 AIUB
22.7 Orbit Related Files VERSION 2 CODE RAPID 3-DAY SOLUTION, DAY 306, YEAR 2003 03-NOV-03 08:41 ------------------------------------------------------------------------------------------------ NUTATION MODEL : IAU80 SUBDAILY POLE MODEL: IERS2000 MJD X-P Y-P UT1UTC LOD S-X S-Y S-UT S-LD NR NF NT X-RT Y-RT .. E-6" E-6" E-7S E-7S/D E-6" E-6" E-7S E-7S/D E-6"/D .. 52943.00 210899 225409 -3706590 -1087 33 34 1 12 123 0 24 -1606 -1893 .. 52943.50 210096 224463 -3706047 -441 32 32 6 25 123 0 24 -1606 -1893 .. 52944.00 209293 223516 -3705826 34 32 33 11 46 123 0 24 -2082 -1585 .. 52944.50 208252 222724 -3705843 906 32 32 12 51 123 0 24 -2082 -1585 .. 52945.00 207211 221932 -3706296 2011 32 33 15 66 123 0 24 -2269 -2095 .. Figure 22.23: Pole file (IEP) in IGS/IERS format. 22.7.8 Earth Rotation Parameters or Pole Coordinates in Bernese Format Type: ASCII Directory: Campaign-specific directory ORB. Extension: ERP Content: Pole coordinates, UT1-UTC, UTC-GPS, nutation offsets. Created by: Download from our anonymous account C04 yyyy.ERP in Bernese ERP format or download C04 pole, rapid pole, or IGS pole from different places (see Section 4.12) and use POLUPD (”Menu>Orbits/EOP>Handle EOP files>Convert IERS to Bernese format”) to transform to Bernese ERP format (currently 13 different pole file formats are supported). The pole file may also be created as a result of a parameter estimation using programs GPSEST (”Menu>Processing>Parameter estimation”) or ADDNEQ2 (”Menu>Processing>Normal equation stacking”). Used by: All orbit programs and all processing programs. Example: Figure 22.24 and ${X}/DOC/EXAMPLE.ERP. ERP files are input files for most of the programs but they may also be created as output files from parameter estimation using GPSEST or ADDNEQ2. In Version 5.0 Nutation models IAU80 and IAU2000 and subdaily Earth rotation model IERS2000 and RAY 96 are available. Always use the same pole file together with one and the same orbit file (standard orbit or tabular). The pole file is accessed by the subroutine ${LG}/GETPOL.f. It is not important that the pole positions are given at equidistant time intervals. ${LG}/GETPOL.f checks, however, for each request that the spacing between the two data points used for interpolation is smaller than 10 days. The table values are linearly interpolated and a warning is given if a leap second occurred in the interpolation interval. IERS C04 POLE 07-JAN-04 18:36 ------------------------------------------------------------------------------------------------ NUTATION MODEL : IAU80 SUBDAILY POLE MODEL: IERS2000 DATE TIME X-POLE Y-POLE UT1-UTC GPS-UTC RMS XP RMS YP RMS DT DE-CPO DP-C.. YYYY MM DD HH MM (") (") (S) (S) REM (") (") (S) (") (").. .. 2004 1 1 0 0 0.03134 0.15381 -0.389583 13. C04 0.00000 0.00000 0.000000 0.00000 0.00.. 2004 1 2 0 0 0.02881 0.15364 -0.390051 13. C04 0.00000 0.00000 0.000000 0.00000 0.00.. 2004 1 3 0 0 0.02665 0.15381 -0.390382 13. C04 0.00000 0.00000 0.000000 0.00000 0.00.. 2004 1 4 0 0 0.02421 0.15425 -0.390536 13. C04 0.00000 0.00000 0.000000 0.00000 0.00.. 2004 1 5 0 0 0.02171 0.15487 -0.390534 13. C04 0.00000 0.00000 0.000000 0.00000 0.00.. Figure 22.24: Pole file (ERP) in Bernese Format. Bernese GPS Software Version 5.0 Page 509
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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 20.4.1.5 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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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 522 and 523: 22. Data Structure EGM96 EGM96, VER
Page 524 and 525: 22. Data Structure SINEX : OPTION I
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Page 556 and 557: 22. Data Structure Station sigma fi
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Page 560 and 561: 22. Data Structure 22.8.18 Receiver
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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
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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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