Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure Remarks: • Each coordinate file has to contain in line 3 the name of a geodetic datum specified in the datum file (see Section 22.4.2). Geodetic datum does not mean that the coordinates below are referring to this datum. The geodetic datum is only used to compute ellipsoidal coordinates in the processing programs if necessary. Whenever possible the geocentric coordinates should refer to the ITRF (i.e., to the same reference frame as the precise orbits used). The format of the rectangular coordinates in the geocentric system is: FORMAT(I3,2X,A16,3F15.4,4X,A1) • The coordinate epoch is written by all programs except RXOBV3. It is used in the programs HELMR1 (see Section 10.6.2) and COOVEL (”Menu>Service>Coordinate tools>Extrapolate coordinates”) (propagation of coordinates to a different epoch with help of a velocity file). • Data records start in line 7. The end of the input file is indicated by a blank line. Lines below the blank line are ignored. • The station numbers have to be unique for stations processed simultaneously. • Programs which compute station coordinates always update an input coordinate file leaving coordinates unchanged for stations which were not processed. • Different programs mark the estimated coordinates with different flags. The flags of coordinates which were unchanged by a program are set to blank. The flags are used by program CRDMERGE in order to establish a priority order when merging coordinate files (see Section 10.6.5) and by programs HELMR1 and COMPAR which compares only coordinates with flags. GPSEST and ADDNEQ2 allow to select stations (e.g., for datum defintion) based on their flag. The defined flags are: R Coordinates extracted from RINEX files, from program RXOBV3. C Coordinates from a code single point positioning, from program CODSPP. U Coordinates from an epoch-difference solution in the zero-difference phase screening, from program MAUPRP. T Coordinates from a triple-difference solution in the baseline screening, from program MAUPRP. P Coordinates estimated with or without constraints in the main parameter estimation step, from program GPSEST. M Mean coordinates from several solutions, from program COMPAR. A Coordinates estimated without constraints in the normal equation combination step, from program ADDNEQ2. W Coordinates estimated with constraints in the normal equation combination step, from program ADDNEQ2. N Estimated coordinates for a station used to define a free network condition in the normal equation combination step, from program ADDNEQ2. I ITRF coordinates. E Eccentric site coordinates, when using a station eccentricity file. F Coordinates of the station were fixed in the solution, from programs MAUPRP and GPSEST. others Not estimated, not used, or unknown. Page 520 AIUB
22.8.6 Station Eccentricities Type: ASCII Directory: Campaign-specific directory STA. Extension: ECC Content: Station eccentricities. 22.8 Station Related Files Created by: User-defined, assistance using ”Menu>Campaign>Edit station files>Eccentricities”. Used by: All processing programs. Example: Figure 22.34 and ${X}/DOC/EXAMPLE.ECC. With an eccentricity file it is possible to have receivers at eccentric points with a known position relative to the center station. Introducing the eccentricity elements as given, only the coordinates of the center station will be estimated in GPSEST, CODSPP, and MAUPRP. In some cases it is easier to estimate the eccentric coordinates (where the GNSS receiver/antenna is located) and to handle the eccentricity problem outside of the Bernese programs (especially if the eccentric values are not precisely known). In that case no eccentricity file is needed. The eccentricity file may also be used to estimate one set of coordinates for two receivers by introducing the known vector between the two sites into an eccentricity file. The file contains: • Eccentric station number. The numbers of centers and eccenters has to be unique for stations processed simultaneously. • Eccentric station name. • Name of center station belonging to the eccentric station. • Eccentricities (DN, DE, DH) in the local geodetic datum specified in the third line of the file if you set SYSTEM to “L” (L:LOCAL) or the (DX, DY, DZ) eccentricities in the geocentric system (G:GEOCENTRIC). The datum must be equal to the datum in the coordinate file used. The eccentricities are added to the coordinates of the center station to obtain the eccentric station coordinates. The end of the list is indicated by a blank line. Example for an eccentricity file -------------------------------------------------------------------------------- LOCAL GEODETIC DATUM: IGS00 SYSTEM : L (G: GEOCENTRIC, L: LOCAL) CENTER --> STATION NUM STATION NAME CENTER NAME DN (M) DE (M) DH (M) 1 AUCK 50209S001 AUCK 50209M001 -0.0030 -0.0050 1.3490 2 FAIR 40408S001 FAIR 40408M001 0.0070 0.0040 0.5320 Figure 22.34: Station eccentricity (ECC) file. Bernese GPS Software Version 5.0 Page 521
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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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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 20.4.1.7 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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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 512 and 513: Page 484 AIUB ANTENNA PHASE CENTER
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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 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
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Page 586 and 587: 23. Installation Guide BERN50 : $C
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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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Bernese GPS Software Version 5.0 - Bernese GNSS Software

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