Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure -1 2 1 5 TITLE : Conversion of STD-orbit file into ASCII CREATE: 07-JAN-04 09:44 INTEGR: 1.00000 10 6.00000 12 NUTSUB: IAU80 IERS2000 GRAVIT: JGM-3 12 38 24 10 1 2 3 4 5 6 7 8 9 10 11 13 14 15 16 17 18 20 21 23 24 25 26 27 28 29 30 31103117118121122123124105 22 52 UP2004.006 5.3010000000000000E+04 2.0000000000000000 5.3010000000000000E+04 5.3010041666666664E+04 5.3010083333333336E+04 ... 5.3010958333333336E+04 5.3011000000000000E+04 2.6557971550620001E+07 5.4645659999999997E-03 0.9777242716317193 1.0362597403608640 4.5790799264559272 1.6090326590102526 2.0347582948916021E+04 2.6563029231750000E+07 ... Figure 22.21: Standard orbits (STD/FSO file). Created by: ORBGEN (”Menu>Orbits/EOP>Create standard orbits”). Used by: Some orbit programs (e.g., STDDIF (”Menu>Orbits/EOP>Compare orbits>Standard orbits”)) and the processing programs (”Menu>Processing”). Example: Figure 22.21 (ASCII example). A standard orbit contains all the information to compute position, velocity, and higher time derivatives for each satellite. The orbit is stored in the form of polynomial coefficients (one set of coefficients for typically 1 hour). One standard orbit file may contain several arcs per satellite. For additional information we refer to Chapter 5. The format is binary. To transform it to ASCII and back to binary (e.g., to allow a transfer to a different computer platform) use the programs STDFMT and FMTSTD (”Menu>Conversion>Orbit files>Binary to ASCII” and ”Menu>Conversion>Orbit files>ASCII to binary”) (default extension for the ASCII files: FSO). Nutation and subdaily pole model names are saved in the file in order to allow for consistency checks. Old files are accepted. Because they do not contain an entry for these models, we assume IAU80 and RAY 96 respectively. 22.7.5 Radiation Pressure Coefficient File Type: Binary Directory: Campaign-specific directory ORB. Extension: RPR Content: Radiation pressure coefficients and partial derivatives of the satellite positions with respect to the radiation pressure coefficients. The partial derivatives of the satellite positions with respect to the Keplerian elements referring to the beginning of the arc are contained in this file, too. Page 506 AIUB
Created by: ORBGEN (”Menu>Orbits/EOP>Create standard orbits”). 22.7 Orbit Related Files Used by: Program GPSEST (”Menu>Processing>Parameter estimation”) for orbit improvements, program ADDNEQ2 (”Menu>Processing>Normal equation stacking”) for long arc computation. Example: Not given. The structure of this file is similar to the standard orbit file (e.g., more than one arc per satellite possible). Only if you want to improve orbits it is necessary to generate an RPR file with the program ORBGEN. In all other cases the STD files are sufficient for the orbit representation. For additional information see Chapter 15. The format is binary. To transform it to ASCII and back to binary (e.g., to allow a transfer to a different computer platform) use the programs STDFMT and FMTSTD (”Menu>Conversion>Orbit files>Binary to ASCII” and ”Menu>Conversion>Orbit files >ASCII to binary”) (default extension for the ASCII files: FRP). 22.7.6 Osculating Orbital Elements Type: ASCII Directory: Campaign-specific directory ORB. Extension: ELE Content: A priori and estimated orbit parameters with formal uncertainties. Created by: GPSEST (”Menu>Processing>Parameter estimation”) and ADDNEQ2 (”Menu>Processing >Normal equation stacking”). CODE RAPID 3-DAY SOLUTION, DAY 006, YEAR 2004 ARC-NUMBER = 1 SATELLITE = 1 TOSC= 53010.000000000000 --------------------------------------------------------------------------- A = 26557971.51761 26557971.55062 +- 0.002 ORBSYS 2 E = 0.0054645656 0.0054645660 +- 0.000000000 ORBSYS 2 I = 56.019474336 56.019474292 +- 0.000000003 ORBSYS 2 NODE = 59.373309370 59.373309602 +- 0.000000013 ORBSYS 2 PERIGEE = 262.361971162 262.361953839 +- 0.000000848 ORBSYS 2 ARG. OF LAT (START) = 92.190780531 92.190780460 +- 0.000000006 ORBSYS 2 D0 =-0.424268714D-09-0.593293900D-09 +- 0.71850D-11 T950101B Y0 = 0.456279704D-10 0.170825507D-09 +- 0.37105D-11 T950101B X0 =-0.217697936D-09-0.262645556D-09 +- 0.66317D-11 T950101B DC =-0.229929047D-13-0.501698511D-12 +- 0.14187D-11 T950101B YC = 0.311597808D-13 0.673652668D-12 +- 0.14217D-11 T950101B XC =-0.395132643D-09 0.394500404D-10 +- 0.35065D-10 T950101B DS = 0.298656292D-13 0.405107221D-12 +- 0.14201D-11 T950101B YS =-0.119236106D-13-0.505329711D-12 +- 0.14219D-11 T950101B XS =-0.428869929D-09-0.111999774D-09 +- 0.39832D-10 T950101B ARC-NUMBER = 1 SATELLITE = 2 TOSC= 53010.000000000000 ... *** STOCHASTIC ORBIT PARAMETERS *** --------------------------------------------------------------------------- ARC-NUMBER = 1 SATELLITE = 1 TOSC= 53010.000000000000 --------------------------------------------------------------------------- 1 3 13 53010.50000 0.000000000D+00-0.158574027D-05 0.59113D-06 2 3 13 53010.50000 0.000000000D+00 0.349829131D-05 0.10947D-06 3 3 13 53010.50000 0.000000000D+00 0.208901082D-08 0.14219D-07 ARC-NUMBER = 1 SATELLITE = 3 TOSC= 53010.000000000000 ... Figure 22.22: File of a priori and estimated orbit parameters (ELE file). Bernese GPS Software Version 5.0 Page 507
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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 20.4.1.7 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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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 560 and 561: 22. Data Structure 22.8.18 Receiver
Page 562 and 563: 22. Data Structure CODE RAPID 3-DAY
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Page 566 and 567: 22. Data Structure IONOSPHERE MODEL
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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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