Bernese GPS Software Version 5.0 - Bernese GNSS Software

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16. Antenna Phase Center Offsets and Variations In order to allow for an efficient switch between different antenna phase center models in a BPE, it is recommended to use a BPE variable V PCV for the file extensions. You may rename the satellite information file in all program panels in BPE option directories from SATELLIT. to SATELLIT.$(PCV) and PHAS IGS.REL to PHAS ccc.$(PCV) (ccc may stand for the identifier for your institution) using program CHNGEN (”Menu>Configure>Change general options”). In the last section of the PCFs you may then define the variable V PCV variable in the following way # VARIABLE DESCRIPTION DEFAULT 8******* 40************************************** 16************** ... V_PCV GNSS PCV MODEL I05 ... # # DO NOT USE V_D, V_J, V_M, V_Y VARIABLES! # using either an ASCII editor or ”Menu>BPE>Edit process control file (PCF)”, panel “BPE Server Variables”. We refer to Section 19.5.4 for more information on BPE variables and their usage. 16.2.6 Antenna Phase Center Model Name for SINEX The model name (”IGS 01” for relative files or ”IGS05 wwww” for absolute files) is expected to be included in the title line of the output Bernese phase center eccentricity file. This is done automatically if the ANTEX converter (PHCCNV, ”Menu>Conversion>ANTEX to Bernese format”, description in Section 16.3) is used to create or update this file. Program ADDNEQ2 reads the title line if an input Bernese “Phase center variations” file is specified in panel “ADDNEQ2 1.1: General Files” and if an output SINEX file shall be written. It extracts the antenna phase center model name from the characters 13-22, if characters 1-10 of the title string are ”MODEL NAME”, 1 2 3 4 5 6 7 8 12345678901234567890123456789012345678901234567890123456789012345678901234567890 MODEL NAME: IGS_01 23-JUN-06 12:45 -------------------------------------------------------------------------------- and includes it in the SINEX section SITE/GPS PHASE CENTER. Be sure to select the same file in program ADDNEQ2 as you used in program GPSEST. The SINEX result file contains the generic entry ----- for the serial number of all antennas in theSITE/ANTENNA block. For a clear conversion from the 20-character input in the header of the RINEX observation files via the 6-digit integer internally used in the Bernese GPS Software to the 5-character string in the SINEX file a further software implementation will be necessary. Page 334 AIUB
16.3 ANTEX Converter PHCCNV 16.3.1 General Description 16.3 ANTEX Converter PHCCNV With the ANTEX converter PHCCNV (”Menu>Conversion>ANTEX to Bernese format”) you are able to: • update the Bernese phase center file in case of new antenna calibration values get available, • prepare a completely new Bernese phase center eccentricity file (relative or absolute) from ANTEX, • convert a relative Bernese phase center eccentricity file (with all included antennas) to an absolute Bernese phase center eccentricity file, • merge new or individually calibrated antenna patterns from (relative or absolute) ANTEX to your existing (relative or absolute) Bernese phase center eccentricity file, • add patterns of antenna radome combinations that are not included in ANTEX to the Bernese phase center eccentricity file according to the antenna list in your station information file, • update old Bernese phase center eccentricity files containing old satellite antenna names and no receiver antenna radome codes. Note that the consideration of radome codes is a must for the ANTEX converter. In addition, the converter requires the SATELLIT.xxx files made available at the anonymous FTP server (see Section 4.12). Be sure to use the correct version (*.I01 = relative or*.I05 = absolute), depending on the desired output phase center eccentricity file type. The program PHCCNV has three input panels. In the first panel “PHCCNV 1: Input” you can select input, result and output files. In addition you may choose options concerning the Bernese input file (see Figure 16.2). General files, in particular the satellite information file, may be selected in the second panel “PHCCNV 1.1: General Files”. The panel “PHCCNV 2: ANTEX Conversion” (see Figure 16.2) is specific to the ANTEX file conversion. It provides options allowing to fill missing phase pattern values up to a specified elevation (or nadir) angle. Depending on the measurement technique pattern values close to the limiting zenith (or nadir) angle may be missing. These values may be filled with zeroes or with the value of the last available zenith (or nadir) angle. In addition, the missing values for ground antennas may be substituted by the values of the AOAD/M T antenna, the reference antenna in case of relative antenna patterns. Further description of the options can be found in the online help or in the examples in Section 16.3.2. Depending on the input files, the program handles relative or absolute antenna models. Furthermore the conversion from the relative to the absolute antenna model is possible. The program checks whether the elevation dependent corrections for the antenna "AOAD/M_T NONE" numbered with 999999 (second entry in antenna number range) are zero or not in order to find out whether the input file refers to the relative or the absolute model. In any case, check the detailed program output carefully in order to verify that the information for all antennas was properly handled and that the output phase center eccentricity file is ready for use. Bernese GPS Software Version 5.0 Page 335
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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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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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Page 338 and 339: 15. Estimation of Satellite Orbits
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Page 384 and 385: 18. The Menu System 18.2 Starting t
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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 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 PID 903 CLK
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20. Processing Examples and IGS 00B
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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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21. Program Structure continued fro
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21. Program Structure ! -----------
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22. Data Structure "Program" Area $
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22. Data Structure Table 22.1: List
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22. Data Structure 22.4.2 Geodetic
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22. Data Structure 22.4.4 Antenna P
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Page 484 AIUB ANTENNA PHASE CENTER
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22. Data Structure 22.4.5 Satellite
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22. Data Structure 22.4.6 Satellite
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22. Data Structure DIFFERENCE OF GP
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22. Data Structure 22.4.9 Subdaily
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22. Data Structure EGM96 EGM96, VER
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22. Data Structure SINEX : OPTION I
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22. Data Structure 22.4.16 Panel Up
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22. Data Structure 22.6.2 Header an
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22. Data Structure 15 Antenna type(
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22. Data Structure SVN-NUMBER= 2 ME
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22. Data Structure -1 2 1 5 TITLE :
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22. Data Structure Used by: ORBGEN
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22. Data Structure 53064.00 53065.0
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22. Data Structure CODE’S MONTHLY
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22. Data Structure Table 22.4: Stat
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22. Data Structure (3) TYPE 003: HA
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22. Data Structure 22.8.4 Station P
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22. Data Structure Remarks: • Eac
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22. Data Structure The following st
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22. Data Structure Table 22.7: List
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22. Data Structure AJAC $$ FES2004
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22. Data Structure Station sigma fi
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22. Data Structure GOPE 11502M002 Z
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22. Data Structure 22.8.18 Receiver
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22. Data Structure CODE RAPID 3-DAY
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22. Data Structure 22.9.3 Meteo and
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22. Data Structure IONOSPHERE MODEL
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22. Data Structure 22.10 Miscellane
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22. Data Structure 22.10.4 Variance
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22. Data Structure 22.10.5 Normal E
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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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Bernese GPS Software Version 5.0 - Bernese GNSS Software

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