Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure CODE’S MONTHLY GNSS P1-P2 DCB SOLUTION, YEAR-MONTH 03-05 05-JUN-03 14:17 -------------------------------------------------------------------------------- DIFFERENTIAL (P1-P2) CODE BIASES FOR SATELLITES AND RECEIVERS: PRN / STATION NAME VALUE (NS) RMS (NS) *** **************** *****.*** *****.*** G01 -1.552 0.004 G02 -2.823 0.006 G03 -1.072 0.005 G04 0.222 0.009 ... ... ... G29 0.576 0.006 G30 1.421 0.005 G31 -0.036 0.008 R03 0.857 0.030 R05 25.907 0.056 R07 -1.370 0.188 ... ... ... R22 -7.880 0.025 R23 -5.789 0.029 R24 0.630 0.045 Figure 22.27: Differential P1-P2 code biases for GNSS satellites (DCB file). GLONASS. Note that a bias value specific to a receiver is addressed with the corresponding station name. The type of code biases is indicated by the string “P1-P2” or “P1-C1 in the header of the file. More information concerning DCBs may be found in Chapter 13 or in [Schaer, 1999]. 22.7.12 Receiver Clock Coefficients Type: ASCII Directory: Campaign-specific directory ORB. Extension: CLK ATTENTION: same extension and directory as the Bernese satellite clock file. Content: Receiver clock corrections (for simulation purposes only). Created by: User-defined. Used by: GPSSIM (”Menu>Service>Generate simulated observation data”). Example: Figure 22.28 and ${X}/DOC/EXAMPLE2.CLK. RECEIVER CLOCKS AS POLYNOMIALS OF DEGREE N-1 POLYNOMIAL COEFFICIENTS IN SEC, SEC/DAY, SEC/DAY**2,... STATION N A0 A1 A2 A3 A4 A5 CHASSERAL 6 -0.003002+0.001234-0.000000+0.010000-0.034556-0.023476 GENEROSO 6 +0.020000-0.010000+0.010000-0.005045-0.000345-0.123456 TITLIS 6 -0.013000+0.020000-0.001234+0.001000-0.006000-0.500000 ZIMMERWALD 6 +0.016017-0.000123+0.000222-0.002000-0.012345+0.000555 Figure 22.28: Receiver clock corrections (for simulation only). Page 512 AIUB
22.8 Station Related Files * ATTITUDE FILE OF CHAMP 0003902 FOR DOY 150-2001 24-JUN-03 17:01 * --------------------------------------------------------------------------------------------- * Data derived from ${K}/JASON/ORB/CHA01150 12.AUX * MJD attitude rotation matrix * Part of MJD first row * --------------------------------------------------------------------------------------------- 52059. 0.00000000000000 0.04616420851114 -0.48525053457856 0.87315564740210 -0.04845498091011 ... 0.00011574073869 0.05591995226978 -0.48442487681705 0.87304381199357 -0.04250661535403 ... 0.00023148148466 0.06569138988084 -0.48360788229990 0.87281616478788 -0.03654388796433 ... 0.00034722222335 0.07547242410888 -0.48279728443165 0.87247389379643 -0.03057827702533 ... 0.00046296296205 0.08520095043148 -0.48199448618883 0.87202185370906 -0.02459677408861 ... ... ... ... ... ... ... Figure 22.29: Satellite attitude file from program LEOAUX. 22.7.13 Satellite Attitude for LEOs Type: ASCII Directory: Campaign-specific directory ORB. Extension: ATT Content: Satellite attitude information. Created by: Program LEOAUX or original CHAMP or JASON attitude files. Used by: CODSPP, MAUPRP, GPSEST, GPSSIM. Example: Figure 22.29. The attitude information provides the transformation from the LEO satellite body fixed coordinate system to inertial (J2000). The reading routine ${LG}/READATT.f90 may read original attitude files from CHAMP and JASON, or these LEO satellite information may be converted into Bernese format using program LEOAUX. The program has to be executed with the command RUNGPS (see Section 18.8). The Bernese file is composed of a header including the integer MJD of the first epoch and of a data section containing the fractional day (column 1) and the attitude rotation matrix elements ordered by row (columns 2–9). Attitude for GPS and GLONASS satellites is hard-wired in the code. 22.8 Station Related Files The station related file types, explained in this section, are listed in Table 22.4. 22.8.1 Session Table Type: ASCII, menu input file format Directory: Campaign-specific directory STA. Extension: SES Content: Time interval covering all observations which should be processed together. Program input panel format. Created by: The file is copied to the campaign during the campaign setup (”Menu>Campaign >Create new campaign”). Edit the file using ”Menu>Campaign>Edit session table”. Used by: All programs. Example: Figure 3.1 and ${X}/SKL/SESSIONS.SES. Bernese GPS Software Version 5.0 Page 513
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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 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 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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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
Page 510 and 511: 22. Data Structure 22.4.4 Antenna P
Page 512 and 513: Page 484 AIUB ANTENNA PHASE CENTER
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 546 and 547: 22. Data Structure 22.8.4 Station P
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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
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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Page 586 and 587: 23. Installation Guide BERN50 : $C
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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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