Bernese GPS Software Version 5.0 - Bernese GNSS Software

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22. Data Structure DIFFERENCE OF GPS-TIME MINUS UTC-TIME ------------------------------------- GPS-UTC VALID SINCE (SEC) YYYY MM DD HH MM SS.SS 4. 1985 07 01 00 00 00.00 5. 1988 01 01 00 00 00.00 6. 1990 01 01 00 00 00.00 7. 1991 01 01 00 00 00.00 8. 1992 07 01 00 00 00.00 9. 1993 07 01 00 00 00.00 10. 1994 07 01 00 00 00.00 11. 1996 01 01 00 00 00.00 12. 1997 07 01 00 00 00.00 13. 1999 01 01 00 00 00.00 22.4.7 Leap Seconds Figure 22.9: The leap second file GPSUTC. Type: ASCII Directory: ${X}/GEN (UNIX) or %X%\GEN (Windows) Extension: - Content: Leap seconds. Created by: User-defined. Available from BSW aftp server. Used by: Used by programs POLUPD, QLRINEXO, RXNPRE, RXOBV3, SNX2NQ0. Example: Figure 22.9 and ${X}/GEN/GPSUTC.. The file has to be updated each time a leap second is introduced. Most programs take the leap second information from the pole file. Programs CODSPP, GPSEST, MAUPRP need the file only if an attitude file for JASON is used. 22.4.8 Nutation Model Type: ASCII Directory: ${X}/GEN (UNIX) or %X%\GEN (Windows) Extension: NUT Content: Nutation model coefficients. Created by: User-defined. Used by: All programs writing and using orbit information. Example: Figure 22.10 and ${X}/GEN/IAU2000.NUT. Nutation models IAU80 and IAU2000 are available in Version 5.0 which are conforming with the respective IAU resolutions. The files contain the coefficients for luni-solar and planetary nutation terms as well as for the computation of the nutation arguments. The IAU2000 precession-nutation model replaces the IAU80 nutation model and is recommended by the IERS Conventions 2003 [McCarthy and Petit, 2004]. It is based on a non-rigid Earth and includes 678 lunisolar terms and 687 planetary terms. In order to increase efficiency the nutation matrix is buffered in a table with tabular interval of 1 hour. Values in this interval are interpolated linearly. The nutation model file has to be consequently used for all programs starting with program PRETAB. For standard orbits generated with Version 4.2 the model IAU80 has to be used. Page 490 AIUB
Bernese GPS Software Version 5.0 Page 491 IAU 2000 NUTATION MODEL INCLUDING PLANETARY NUTATION -------------------------------------------------------------------------------- Nutation model name: IAU2000 Precession corrections to IAU 1976 precession model: --------------------------------------------------- Offset in longitude (") : -0.0417750 at J2000.0 Offset in obliquity (") : -0.0068192 Correction in longitude ("/c): -0.29965 Correction in obliquity ("/c): -0.02524 Fundamental arguments: --------------------- ARG A0 A1 A2 A3 A4 R (") ("/c) ("/c**2) ("/c**3) ("/c**4) L 485868.2490360000 715923.2177999020 31.8792000000 0.0516350000 -0.0002447000 1325. L’ 1287104.7930500000 1292581.0480999947 -0.5532000000 0.0001360000 -0.0000114900 99. F 335779.5262320000 295262.8478000164 -12.7512000000 -0.0010370000 0.0000041700 1342. D 1072260.7036900001 1105601.2090001106 -6.3706000000 0.0065930000 -0.0000316900 1236. O 450160.3980360000 -482890.5431000004 7.4722000000 0.0077020000 -0.0000593900 -5. LQ 908103.2597768833 261628.6889778376 0.0000000000 0.0000000000 0.0000000000 415. LV 655127.2830690601 712136.4335481822 0.0000000000 0.0000000000 0.0000000000 162. . . PA 0.0000000000 5029.0969397151 1.1111299474 0.0000000000 0.0000000000 0. MULTIPLIERS OF FUNDAMENTAL ARGUMENTS PERIOD LONGITUDE OBLIQ... (days) LS LS’ LC LC’ OC OC’ ... L L’ F D O LQ LV LE LM LJ LS LU LN PA (mas) (mas/c) (mas) (mas/c) (mas) (mas/c) ... 0 0 0 0 1 0 0 0 0 0 0 0 0 0 -6798.383 -17206.4161 -17.4666 3.3386 0.0029 9205.2331 0.9086 ... 0 0 2 -2 2 0 0 0 0 0 0 0 0 0 182.621 -1317.0906 -0.1675 -1.3696 0.0012 573.0336 -0.3015 ... 0 0 2 0 2 0 0 0 0 0 0 0 0 0 13.661 -227.6413 -0.0234 0.2796 0.0002 97.8459 -0.0485 ... 0 0 0 0 2 0 0 0 0 0 0 0 0 0 -3399.192 207.4554 0.0207 -0.0698 0.0000 -89.7492 0.0470 ... . . . Figure 22.10: Nutation model file IAU2000.NUT 22.4 General Files
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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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Page 494 and 495: 21. Program Structure $C / %C% PGM
Page 496 and 497: 21. Program Structure (program GPSE
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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
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
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Page 522 and 523: 22. Data Structure EGM96 EGM96, VER
Page 524 and 525: 22. Data Structure SINEX : OPTION I
Page 526 and 527: 22. Data Structure 22.4.16 Panel Up
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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 546 and 547: 22. Data Structure 22.8.4 Station P
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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 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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