Bernese GPS Software Version 5.0 - Bernese GNSS Software

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6. Data Preprocessing GAR small pieces of observations (garbage), O-C observations marked due to large observed–computed values during the epoch difference solution (see option “Maximum observed-computed value” in panel “MAUPRP 6: Epoch-Difference Solution”), and CLK observations marked because no satellite clock value was available when preprocessing zero-difference files, or observations marked because of a clock event, see Section 6.5.4. MAUPRP also gives information on the ambiguities set up. Each satellite has one initial ambiguity corresponding to the first epoch. All other ambiguities are called multiple. Only the multiple ambiguities are listed. The ambiguities which were introduced in the most recent run are marked by an asterisk. ------------------------------------------------------------------------ MULTIPLE AMBIGUITIES ------------------------------------------------------------------------ NUMB TYP SATELLITE EPOCH ------------------------------------------------------------------------ 1 *GAP 5 2725 2 *GAP 30 2869 3 *GAP 18 794 4 *GAP 18 2555 5 *GAP 29 2388 The following types of multiple ambiguities are defined: FIL ambiguity which was already set in the observation file header, CYC ambiguity which was introduced due to a cycle slip flag in the observation (see option “If a cycle slip flag in observation file” in panel “MAUPRP 9: Outlier Rejection / Ambiguity Setting”), GAP ambiguity which was introduced due to a gap in the observations, PRP ambiguity which was introduced due to the detection of a cycle slip that could not be corrected (and outlier rejection was not possible), and CLK ambiguity which was introduced due to a clock event, see Section 6.5.4. At the end MAUPRP writes the very important message FILE SAVED which means that all the changes were written into the observation file. If “FILE NOT SAVED” is printed, no changes were made to the original observation file(s) (see option “Save screened observation files” in panel “MAUPRP 3: General Options”). Page 126 AIUB
Example 2 6.5 Preprocessing Phase Observations The second example is based on the very short baseline (only 14 meters) between the two stations in Zimmerwald (ZIMJ−ZIMM) available in the example campaign (see Chapter 20). We used the strategy BOTH in this case. All other options are identical to those in Example 1 with one exception: “Maximum ionospheric change from epoch to epoch” in panel “MAUPRP 8: Cycle Slip Detection/Correction” was set to 30%. The strategy BOTH should not be used for baselines longer than about 10 km. However, this strategy may be superior to the COM- BINED strategy if the baseline is very short and the receiver is of poor quality and provides measurements with a high noise level (not the case in this example). The output from the program is similar to that of Example 1. The only difference is the cycle slip detection flag used: here it is SNG (instead of DUA in Example 1). ------------------------------------------------------------------------ CYCLE SLIPS ACCEPTED IN THIS RUN ------------------------------------------------------------------------ NUMBER OF SLIPS IN L1: 70 NUMBER OF SLIPS IN L2: 124 NUMB TYP N EPOCH SAT FRQ WLF SLIP FRAC RES.L3 IONOS (M) (M) ------------------------------------------------------------------------ 1 CLK * 18 ALL 1 1 51988847. 2 CLK * 18 ALL 2 1 40510790. 3 SNG * 51 18 2 1 -8442034. 0.12 4 SNG * 87 18 2 1 52. 0.08 5 SNG * 87 14 2 1 4106575. 0.06 You may compare the correction for cycle slip 3 (second frequency for satellite 18 at epoch 51) in the second example with the correction for the corresponding cycle slip in the first example. It is the same event that can be attributed to the data of the station Zimmerwald (ZIMM) that was used in both baselines. The small difference in the correction for the clock jump between the two examples does not matter because finally double-differences of the observations without access to the clock parameters are analyzed. Example 3 The third example demonstrates the program output of MAUPRP for screening zerodifference files. Again the station Zimmerwald (ZIMM) is used. A satellite clock file produced by the program CLKEST was introduced. To preprocess zero-difference observation files we have to use the COMBINED mode. The option “Do not accept cycle slip corrections” is marked and the “Maximum ionospheric change from epoch to epoch” is 400% (see panel “MAUPRP 8: Cycle Slip Detection/Correction”). As mentioned in Section 6.5.3 the change of the receiver clock correction is estimated epochwise before the residuals for the cycle slip detection are computed (Eqns. (6.4)). The program output contains a summary of these epoch solutions: Bernese GPS Software Version 5.0 Page 127
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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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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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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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21. Program Structure continued fro
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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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