[IGSREPORT-7670] Wk 1083 JPL Analysis Report

David C Jefferson djeff at cobra.jpl.nasa.gov
Tue Oct 24 16:38:07 PDT 2000


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IGS Electronic Report   24 Oct 16:38:13 PDT 2000      Message Number 7670
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Author: D C Jefferson

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JPL ANALYSIS REPORT   GPS-WEEK 1083 (DAYS 282-288, DATES 2000 Oct 08 - Oct 14)
******************************************************************************

Submitted by the JPL IGS/FLINN Analysis Team:

D C Jefferson, Y E Bar-Sever, M B Heflin, F H Webb, J F Zumberge

all at the Jet Propulsion Laboratory, California Institute of Technology, 
Pasadena, CA  91109.

Files listed below are available in Unix compressed format and can be
retrieved using anonymous ftp to sideshow.jpl.nasa.gov (137.78.60.30),
directory pub/jpligsac/1083.  These files (except for *.tro) have also
been sent to the CDDIS.

______________________________________________________________________________
filename             contents
______________________________________________________________________________
jpl10837.sum         This text file.
jpl10837.erp         Earth rotation parameters for GPS week 1083.
jpl10837.snx         Ground station coordinates for GPS week 1083, SINEX format.
jpl1083[0-6].sp3     GPS ephemerides for GPS week 1083, sp3 format.
jpl1083[0-6].tro     Ground station troposphere estimates for GPS week 1083.
jpl1083[0-6].clk     GPS and ground station clocks for GPS week 1083, RINEX.
______________________________________________________________________________

Median Orbit Repeatability (see table below): 8.0 cm

This week, we add three new candidate global stations.  As with other sites,
these sites are given the opportunity to participate in the orbit and clock
solution as the global site distribution varies.  The following nominal
coordinates were assumed:
                                        X (m)           Y (m)           Z (m)
NRIL (Norilsk, Russian Federation)   64537.2902    2253782.9180    5946363.6340
RBAY (Richardsbay, S. Africa)      4739765.9403    2970758.2793   -3054077.8671
YEBE (Yebes, Spain)                4848724.8079    -261632.2914    4123094.1106

Due to potential problems, data from stations mentioned below were not
considered for use in the global solution for the day indicated.  (For
geographical reasons, they may not have been used in any case.)

WARNING: NRC1 (not USNO) used as reference clock days 282 and 288.
WARNING: ALGO (not USNO) used as reference clock days 286 and 287.
WARNING: Data from PRN15 and PRN28 excluded the entire GPS week 1083.
WARNING: Data from PRN13 excluded days 284 and 285.
WARNING: Data from PRN11 excluded days 286 and 287.
WARNING: Data from GUAT, JAB1, KELY, PETP, RIOG, WTZT excluded day 282.
WARNING: Data from EPRT, MEDI, NICO, NTUS, PETP, WTZT excluded day 283.
WARNING: Data from KELY, LBCH, NICO, NTUS, OAT2, PETP, UNSA, WTZT excluded day
         284.
WARNING: Data from DGAR, GUAT, JAB1, LBCH, MALI, PETP, UNSA excluded day 285.
WARNING: Data from GUAT, JAB1, LBCH, PETP, WTZT excluded day 286.
WARNING: Data from DRAG, GUAT, JAB1, MALI, PETP, WTZT excluded day 287.
WARNING: Data from ESTI, GUAT, LBCH, PETP, WTZT excluded day 288.

In the following table, UT1R-UTC are the integrated values based on estimated
LODR values in the adjacent column.  See IGS Report No. 1498 (jpl07827.sum)
for details:

JPL ERP TABLE                               GPS week 1083 (2000 Oct 08 - Oct 14)
version 2           
     MJD   XPole   Ypole  UT1R-UTC   LODR Xsg Ysg UTsg LOsg Nr Nf Nt   Xrt   Yrt
         10**-6" 10**-6"      .1us .1us/d 10**-6" .1us .1us/d          10**-6"/d
51825.50  -18398  250867   1503000   8039  36  45  138  138 42  0 25 -1689   300
51826.50  -19822  251574   1494995   7971  35  43  139  139 42  0 25 -1672   963
51827.50  -21173  252615   1486719   8581  36  44  138  138 42  0 24 -1507  1412
51828.50  -22394  254073   1477770   9318  37  45  140  140 42  0 24 -1115  1964
51829.50  -23522  255783   1468314   9593  37  45  147  147 42  0 24 -1469  1730
51830.50  -25312  257387   1458673   9689  37  44  156  156 42  0 24 -2326  1564
51831.50  -27268  258822   1448640  10378  36  43  140  140 42  0 25 -2222   925
END ERP TABLE

The following table indicates the "3-dimensional orbit repeatability", as 
defined in IGS Mail Message 37, for GPS week 1083:
["3d rss" = sqrt(xrms**2 + yrms**2 + zrms**2)]

JPL ORBIT REPEATABILITY TABLE               GPS week 1083 (2000 Oct 08 - Oct 14)
      00 10  8   00 10  9   00 10 10   00 10 11   00 10 12   00 10 13   00 10 14
prn   3d rss (cm)
  1      12         30         13         10          9         17         22   
  2       6          5          6         10         14         17         12   
  3       6          5          8          8          8          4          6   
  4       7          7          6          8         11          4          7   
  5       3          6          6          5          8          5          6   
  6      12         14          6          5          6         10          9   
  7       6          9          5          6         12          8          5   
  8       5          6          5          8         10         20         10   
  9       5          5          5          4          4          8          5   
 10       4          5          5          8         30         25          7   
 11      17         15         25         30                               12   
 13       8         18                                3          7         11   
 17       6          5          8          4          5          9          7   
 19      13          9          6         13          7          9          6   
 20      14          8         12         14         14         14         11   
 21       6          4          9          9          7          7          9   
 22       5          9         13         14          7          6          8   
 23       5          4          7          4          7         11         11   
 24       6          8          8          7         11          8          6   
 25       8          8          9         14          8          5          8   
 26       4          6          5          5         10          5          6   
 27       6         14          7         10          7         15          8   
 29       6          5         11         11          6         10         11   
 30       6          8          5          7          6          6          6   
 31      11          5          9          9          8          9          7   
_______________________
END ORBIT REPEATABILITY TABLE

The following table statistically summarizes this week's "engineering data", as
described in IGS Report No. 1528:

JPL ENGINEERING DATA SUMMARY TABLE          GPS week 1083 (2000 Oct 08 - Oct 14)
 receiver/transmitter (dot means point positioned, * means fiducial site)
 |     days analyzed
 |     |      rms clock noise (ns)
 |     |      |           average clock solution (us)
 |     |      |           |           rms pseudorange (cm)
 |     |      |           |           |   (dot means pcode not analyzed)
 |     |      |           |           |           rms phase (mm)
 |     |      |           |           |           |           average arc (hr)
 |     |      |           |           |           |           |
 |___  |__    |_______    |_______    |___        |___        |__
ALGO*  7.0    .784e-01    1.64        32.2        3.77        3.32    
ALIC   1.0    124.       -.129e-01    48.0        5.00        3.72    
AOML   1.0    20.7       -.163e-02    57.0        6.00        3.10    
AREQ*  3.0    37.8        15.2        26.3        4.39        2.31    
ARTU   5.0    20.7       -.873e-01    36.2        4.00        2.55    
ASC1   6.5    126.       -.121e-01    77.1        5.15        2.38    
AUCK*  6.0    18.4       -.390e-02    59.9        4.53        2.79    
BAHR*  7.0    .504        763.        34.9        4.87        3.51    
BARB   1.8    31.1       -.114        26.1        6.51        3.04    
BJFS   2.0    2.06        691.        18.5        4.00        3.18    
CAS1*  2.0    11.5       -.402e-02    27.4        4.00        1.35    
CIC1   5.9    104.       -.156e-01    59.1        4.18        2.92    
COCO   7.0    14.5       -.230e-02    27.1        5.73        3.73    
CRO1   1.0    .250       -.357e-01      .         4.00        .989    
DAEJ   4.0    1.65        563.        62.5        5.27        2.26    
DARW   2.0    .174e+05   -.871        39.4        7.52        3.41    
DAV1*  7.0    17.1       -.355e-02    79.1        3.86        1.22    
DGAR   3.9    67.8       -.147e-01    34.7        6.30        2.94    
EISL   5.7    56.1       -.150e-01    80.8        4.85        2.77    
FAIR*  6.7    1.35       -1.57        32.7        3.77        .830    
FORT*  5.6    36.0        .471        85.6        5.35        1.51    
GALA   3.9    33.2       -.125        24.7        4.00        3.08    
GOUG   3.0    .289e+06    502.        62.0        4.37        2.75    
GUAM*  7.0    44.2       -.159        49.6        7.17        3.21    
HOB2*  3.0    .112       -36.0        46.0        5.69        3.20    
HRAO   5.0    .289e+06    506.        77.6        4.63        3.82    
IISC   3.3    49.6       -.319e-01    90.2        5.53        2.03    
IRKT*  7.0    .489       -.197        68.7        4.00        2.52    
JAB1   3.0    34.2       -.138        63.7        6.73        3.32    
JPLM   1.0    .697e+04    7.01        63.0        4.00        2.95    
KELY   1.0    14.9       -.796e-03    73.0        5.00        1.22    
KERG*  6.0    .289e+06    506.        51.9        6.18        2.31    
KIT3*  1.9    30.5       -.693e-02    43.0        5.00        3.59    
KOKB*  7.0    .761       -2.28        42.4        5.46        1.15    
KOUR*  4.0    33.4       -.129        49.3        6.26        2.48    
KUNM   2.9    97.9       -.583e-01    93.0        5.00        2.74    
KWJ1*  5.9    .169e+06    2.77        60.8        5.35        .968    
LHAS*  3.9    12.7       -.229e-02    32.7        4.28        3.66    
MAC1*  6.7    16.6       -.108        33.1        3.91        1.76    
MAG0   6.9    22.6       -.903e-01    42.2        4.31        2.76    
MALI*   .8    .168e+04    2.55          .         7.00        1.99    
MANA   1.0    .288e+06    504.        87.0        7.00        2.21    
MAS1*  4.0    127.        .127        28.8        4.52        3.28    
MAW1   1.0    21.8       -.503e-02    35.0        4.00        1.76    
MCM4*  5.5    .512e+04    11.5        61.0        4.51        .968    
NKLG   6.0    .281e+06    508.        71.6        7.32        1.74    
NRC1   2.1    .           .           42.2        4.52        3.43    
NRIL   1.0    16.2       -.803e-01    37.0        4.00        1.55    
NYA1   1.0    258.        .437        32.0        4.00        1.02    
NYAL*  6.0    .174       -.477        53.6        4.47        1.35    
OHIG*  6.6    22.4       -.275e-02    78.4        4.00        2.04    
ONSA*  7.0    11.7       -.491e-01    45.5        4.16        2.59    
PERT*  1.0    282.       -.170e-01    66.0        4.00        2.62    
REYK   5.0    9.21       -.597e-02    56.4        6.00        1.65    
SANT*  6.3    633.       -.270        35.5        4.00        1.16    
SELE   3.9    56.6       -.701e-02    77.7        3.00        3.02    
SFER   3.0    .559        837.        68.0        4.00        2.51    
STJO   5.0    3.70        .667        32.4        4.85        3.67    
SUTH   2.0    47.8       -.463e-02    83.5        4.00        2.74    
SYOG    .8    .253e+06    551.        43.0        7.00        .917    
TEGU   2.0    .289e+06    503.        94.4        6.55        1.77    
THTI   6.0    .289e+06    503.        76.6        5.85        2.07    
TIDB*  7.0    .226        522.        27.9        5.74        3.86    
TRAB   1.0    16.3        .286e-01    45.0        5.00        3.11    
TSKB*   .8    1.42        1.50        65.0        4.00        2.79    
USNO   3.0    .           .           44.7        5.00        3.73    
WHIT   1.0    13.5       -1.59        29.0        4.00        2.82    
WTZR*  7.0    .191       -1.25        53.7        4.73        2.82    
YAR1*  5.2    820.       -.692        62.6        3.77        1.88    
YELL*  6.8    .144        .537        45.2        4.15        1.44    
ZECK   1.0    31.6       -.169e-01    73.0        3.00        2.66    
PRN01  7.0    2.83        148.        53.2        5.00        2.05    
PRN02  6.9    3.04       -282.        52.9        5.00        2.15    
PRN03  7.0    2.11        47.7        53.9        5.00        2.07    
PRN04  7.0    1.31        486.        57.2        5.00        2.14    
PRN05  7.0    2.81        269.        53.3        5.00        2.17    
PRN06  7.0    6.85       -.546e-01    53.4        5.15        2.37    
PRN07  7.0    1.75        197.        58.5        5.00        2.26    
PRN08  7.0    3.34        575.        52.9        5.00        2.10    
PRN09  7.0    2.28       -12.0        54.2        5.00        2.17    
PRN10  7.0    2.31        57.9        54.6        5.16        2.22    
PRN11  5.0    .434        .194        52.5        5.22        1.99    
PRN13  5.0    .599       -331.        60.5        4.82        2.04    
PRN17  7.0    4.01       -278.        58.5        5.15        2.25    
PRN19  7.0    4.20        316.        52.7        5.00        1.85    
PRN20  7.0    .531       -51.7        59.1        5.00        2.04    
PRN21  7.0    4.74        17.1        55.1        5.15        2.20    
PRN22  6.9    1.19        345.        56.0        5.00        2.05    
PRN23  7.0    5.40        .894        55.1        5.16        2.42    
PRN24  7.0    2.61        7.71        55.1        5.00        2.19    
PRN25  7.0    1.98        8.83        54.1        5.15        1.87    
PRN26  7.0    .733        562.        52.4        5.15        2.24    
PRN27  7.0    4.79        33.5        50.3        4.86        1.93    
PRN29  7.0    .778        144.        55.8        5.00        2.22    
PRN30  7.0    1.78       -41.5        52.4        5.00        2.11    
PRN31  7.0    2.67        14.3        57.3        5.00        2.06    
_______________________
END ENGINEERING DATA SUMMARY TABLE

As described in IGS Mail Message 37, the following table compares the JPL
precise ephemerides with those from the broadcast ephemeris:

JPL COMPARISON OF BROADCAST NAVIGATION MESSAGE WITH PRECISE EPHEMERIDES
      00 10  8   00 10  9   00 10 10   00 10 11   00 10 12   00 10 13   00 10 14
prn   3d rss (cm)
  1     574        826        545        512        456        244        264   
  2     363        642        710        532        426        348        507   
  3     343        445        333        392        306        361        523   
  4     331        450        434        446        457        266        278   
  5     621        514        654        411        535        566        342   
  6     443        482        567        511        536        524        497   
  7     449        328        313        489        329        560        346   
  8     459        358        430        530        299        337        325   
  9     320        520        415        452        394        484        462   
 10     415        425        381        405        492        391        463   
 11     494        605        590        519                              199   
 13     514        424                              507        552        363   
 17     550        229        169        328        377        281        293   
 19    1108        656        446        615        354        332        383   
 20     427        537        681        601        492        493        621   
 21     281        387        447        471        401        330        471   
 22     326        344        284        433        263        454        465   
 23     569       1205        955        863        446        913        430   
 24     873        522        576        583        477        460        454   
 25     405        413        470        547        438        394        369   
 26     548        242        238        360        340        510        481   
 27     553        413        372        221        385        364        301   
 29     424        473        582        561        227        257        204   
 30     323        288        233        282        229        260        168   
 31     491        318        395        361        294        366        378   
_______________________
END COMPARISON OF BROADCAST NAVIGATION MESSAGE WITH PRECISE EPHEMERIDES

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