Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure SVN-NUMBER= 2 MESSAGE-NR= 1 0.125200000000000000D+04 0.172800000000000000D+06 0.265618431506390683D+08 0.231909182620999993D-01 0.931938345555999970D+00 0.121485586332999995D+01 -0.172696358223000002D+01 0.211032279951000001D+01 0.532093592404999958D-08 -0.801640534402999908D-08 .... 07-JAN-04 06:20 Figure 22.19: Broadcast messages (BRD File). 40 lines of information per message. Directory: Campaign-specific directory ORB. Extension: PRE Content: Precise ephemerides. Created by: STDPRE (”Menu>Orbits/EOP>Convert standard to precise orbits”), RXNPRE (”Menu>RINEX >Import RINEX to Bernese format>Navigation files to SP3”), CCPREORB (”Menu>Orbits/EOP >Cut/concatenate precise orbit files”), PREWEI (”Menu>Orbits/EOP>Set accuracy codes in precise orbits”), and KINPRE. Official exchange format within IGS. Used by: PREWEI, PRETAB (”Menu>Orbits/EOP>Create tabular orbits”), ORBGEN (”Menu >Orbits/EOP>Create standard orbits”), and ORBCMP (”Menu>Orbits/EOP>Compare orbits >Precise orbits”). Example: Figure 4.7 shows a precise orbit file created by CODE for December 12, 2003. Files from external sources may also have the extensions sp3, sp3d, EPH. Apart from SP3c older precise orbit file formats (SP1, SP2, and SP3) may be read and written by the Bernese GPS Software. All the satellite positions in the precise files are given in an Earth-fixed reference frame. SP1 positions of the satellites (obsolete). SP2 positions and velocities of the satellites (obsolete). SP3 positions in km (and optionally velocities in dm/s) and clock information of the satellites in microseconds. SP3c positions in km (and optionally velocities) and clock information of the satellites in microseconds (the new format allows, e.g., for maneuver and prediction flags). The recommended format is SP3c. Detailed informations may be found in [Remondi, 1989] and at ftp://ftp.igs.org/igscb/data/format/sp3c.txt. The satellite-specific formal rms values are given in lines 8–9, specifying the rms in 2 x mm, x = 5−14 (accuracy codes). Satellites with accuracy codes zero or exceeding a user specified limit may be excluded in PRETAB (”Menu>Orbits/EOP>Create tabular orbits”, “PRETAB 2: General Options”). Accuracy codes can also be set or changed by program PREWEI (”Menu>Orbits/EOP >Set accuracy codes in precise orbits”) using a LST file written by ORBGEN. For more details on the satellite clock values (last column, 999999.999999 if not available) and their use see Section 5.5. Page 504 AIUB
TABULAR EPHEMERIS DERIVED FROM PREC. EPH: PR2004. 6 SYSTEM J2000.0 CELESTIAL POLE OFFSET: IAU80 SUBDAILY POLE MODEL: IERS2000 1 6 2004 0.000000000000D+00 0.000000000000D+00 0.000000000000D+00 1 6 2004 0.230000000000D+02 0.450000000000D+02 0.209540641867D-06 0.900000000000D+03 96 -0.390592916107D+00 0.187917856810D-01 0.155273619621D+00 38 SVN 1 ... .. SVN 124 22.7 Orbit Related Files 1 -0.133523047097537D+05 0.671876755934849D+04 0.221249776236694D+05 2 -0.251715229898754D+05 -0.329767345053296D+04 0.886157743828107D+04 3 -0.199030234194768D+05 -0.140239394493945D+05 -0.104360944553931D+05 4 0.248063838069284D+04 0.201877116851523D+05 0.172729998678100D+05 .... 22.7.3 Tabular Orbits Type: ASCII Figure 22.20: Tabular orbit information (TAB file). Directory: Campaign-specific directory ORB. Extension: TAB Content: Tabular satellite positions in the inertial frame B1950.0 or J2000.0. Created by: PRETAB (”Menu>Orbits/EOP>Create tabular orbits”), BRDTAB (”Menu>Orbits/EOP >Broadcast orbits>Create tabular orbits”). Used by: ORBGEN (”Menu>Orbits/EOP>Create standard orbits”). Example: Figure 22.20. The orbit source is specified in the title line from column 44 to 53 (PR2004 in Figure 22.20). This information is transferred to the standard orbit file by program ORBGEN. The following line contains information about the subdaily pole and nutation model used. The next two lines contain start/end time. They are followed by the tabular interval and the (nominal) number of ephemeris points. The next line contains pole information (which is not used by the program system). In the following lines the number of satellites and the satellite numbers (PRN-numbers) are defined. Finally the satellite positions (in system B1950.0 or J2000.0) are given in km. Satellite and epoch belonging to a specific record are reconstructed from the record number which is the first item of each record. Records of satellites for which no positions exist for a certain time interval are not contained in the file to save space. 22.7.4 Standard Orbits Type: Binary Directory: Campaign-specific directory ORB. Extension: STD Content: Standard orbit (Bernese orbit representation using sets of polynomials). Bernese GPS Software Version 5.0 Page 505
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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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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 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 536 and 537: 22. Data Structure Used by: ORBGEN
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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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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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