Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure SINEX : OPTION INPUT FILE 30-MAY-95 18:02 ------------------------------------------------------------------------ (REMARK: YES=1,NO=0 ; 2 EMPTY LINES AFTER EVERY INPUT GROUP) AGENCY: ------- *** --> : XYZ DATA : ------ *** --> : IGS HEADER INFORMATION TO BE INCLUDED: ---------------------------------- +FILE/REFERENCE *INFO TYPE INFO DESCRIPTION My agency/institute OUTPUT One-session solution generated by RNX2SNX BPE CONTACT My e-mail address SOFTWARE Bernese GPS Software Version 5.0 HARDWARE My computer INPUT IGS/IGLOS GNSS tracking data -FILE/REFERENCE +FILE/COMMENT -FILE/COMMENT +INPUT/ACKNOWLEDGMENTS *AGY DESCRIPTION XYZ My agency/institute and its address IGS International GPS Service -INPUT/ACKNOWLEDGMENTS Figure 22.15: General SINEX information file SINEX. You have to adjust and complete this file as soon as you want to create ionosphere map files in IONEX format (see Section 22.9.5). We recommend you to copy the example file $X/GEN/IONEX. to, e. g., $X/GEN/IONEX.USR and to edit the last-mentioned file. This file does not only contain “auxiliary” text information to be included in IONEX files but also important specifications to be defined by the user. Let us briefly highlight all entries: (1) “SATELLITE SYSTEM”, the satellite system used, e. g., GPS, GLONASS, or GNSS. (2) “AGENCY”, the agency creating the IONEX file, e. g., AIUB. (3) “MULTI-LINE DESCRIPTION” is intended for a brief description of the technique used to derive the TEC data provided. A contact address is desirable. (4) “OBSERVABLES USED”, one-line specification of the observable(s) used in the TEC computation. (5) “MULTI-LINE COMMENT”, additional comment lines. (6) “DCB COMMENT”, DCB-related comment line (one line only). (7) “INFORMATION TO BE SAVED”: Here you may specify whether “TEC MAPS” (TEC values), “RMS MAPS” (rms errors), “DIFFERENTIAL CODE BIASES” (DCB estimates for the GPS/GLONASS satellites) are requested to be included in the IONEX file. The entry “DEFAULT EXPONENT” defines in which unit the TEC and rms values are given in the IONEX file. With “-1”, the recommended value, these values are given in units of 0.1 TECU. Page 496 AIUB
22.4 General Files (8) At “REQUESTED SNAPSHOTS”, you may define for which times TEC maps (snapshots) should be computed and written to the IONEX file. Using “12 00 00”, “12 00 00”, “86400”, you would get a single snapshot at 12:00:00 UT. An other setting might be: “01 00 00”, “23 00 00”, “7200”. This would lead to 12 2-hourly snapshots, namely at 01:00:00, 03:00:00, 05:00:00, ..., 23:00:00 UT. (9) At “DATA GRID”, you have to define the geographical area and the spatial resolution of the grid where TEC and rms values are probed. Note that the current setting is suited for global TEC maps, but not for regional maps. (10) Under “ADDITIONAL OPTIONS”, you might define (a) a “minimum TEC value” (TEC values below this threshold are set to this value), (b) a “maximum rms value” (TEC values with larger rms errors are considered as unavailable), and (c) a “scaling factor for rms values” to scale (multiply) the rms errors obtained by the least-squares adjustment. Since negative TEC is physically impossible, a threshold value of 0 TECU would make sense at (a). Nevertheless, we advise the interested user to study the IONEX format specifications [Schaer et al., 1998] and to have a look at CODE’s ionosphere-related web site http://www.aiub. unibe.ch/ionosphere.html [Schaer, 1998]. IONEX CONTROL FILE 14-MAR-02 00:00 ------------------------------------------------------------------------ (REMARK: YES=1,NO=0 ; 2 EMPTY LINES AFTER EVERY INPUT GROUP) SATELLITE SYSTEM: ---------------- ******************** --> : GPS AGENCY: ------ ******************** --> : MULTI-LINE DESCRIPTION (UP TO 30 LINES): --------------------------------------- ************************************************************ --> : OBSERVABLES USED: ---------------- ************************************************************ --> : MULTI-LINE COMMENT (UP TO 30 LINES): ----------------------------------- ************************************************************ --> : TEC/RMS values in 0.1 TECU; 9999, if no value available DCB COMMENT: ----------- ************************************************************ --> : DCB values in ns; zero-mean condition wrt satellite values ... Figure 22.16: General IONEX information file IONEX. Bernese GPS Software Version 5.0 Page 497
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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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Page 494 and 495: 21. Program Structure $C / %C% PGM
Page 496 and 497: 21. Program Structure (program GPSE
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Page 502 and 503: 21. Program Structure ! -----------
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
Page 516 and 517: 22. Data Structure 22.4.6 Satellite
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 526 and 527: 22. Data Structure 22.4.16 Panel Up
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Page 530 and 531: 22. Data Structure 15 Antenna type(
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Page 536 and 537: 22. Data Structure Used by: ORBGEN
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Page 540 and 541: 22. Data Structure CODE’S MONTHLY
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Page 544 and 545: 22. Data Structure (3) TYPE 003: HA
Page 546 and 547: 22. Data Structure 22.8.4 Station P
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Page 552 and 553: 22. Data Structure Table 22.7: List
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
Page 562 and 563: 22. Data Structure CODE RAPID 3-DAY
Page 564 and 565: 22. Data Structure 22.9.3 Meteo and
Page 566 and 567: 22. Data Structure IONOSPHERE MODEL
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22. Data Structure 22.10.7 Observat
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22. Data Structure Created by: Each
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22. Data Structure ----------------
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22. Data Structure 22.10.17 BPE log
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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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