[IGSREPORT-0780] GFZ Analysis Report (week 734)

Gerd Gerd
Thu Feb 10 23:45:49 PST 1994


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IGS Electronic Report    Thu Feb 10 23:45:49 PST 1994      Message Number 0780
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Author: Gerd Gendt and Galina Dick
Subject: GFZ Analysis Report (week 734)

Subject: GFZ Analysis Report (732)


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GFZ ANALYSIS REPORT   GPS-WEEK 0734 (DAYS 030-036, DATES 30-01-94 TO 05-02-94)
******************************************************************************

Submitted by: G. Gendt, Ch. Reigber, G. Dick, Th. Nischan, W. Mai 
              GeoForschungsZentrum Potsdam (GFZ)
             
              Telegrafenberg A17, D-14473 Potsdam, Germany
              e-mail:gend at gfz-potsdam.de
              fax: (0331) 288 1111
              tel: (0331) 288 1114 

PRODUCT SUMMARY

FILES SENT TO IGN: 
______________________________________________________________________________
gfz07347.sum           this text file
gfz07347.erp           Earth rotation parameters 
gfz0734[0-6].sp3       Daily orbit ephemerides , SP3 format
______________________________________________________________________________


ERP RESULT

Attention: UT is given for midnight
           UT differences plus dLODR(ms) gives the adjusted LODR
           
 
  MJD        XP       YP  UT1R-IAT for 0h SIGX   SIGY  SIGLOD NS FIX NV  dLODR 
           arcsec   arcsec     sec      arcsec  arcsec   ms                ms
49382.500  0.08339  0.47319 -27.867200  0.00004 0.00003 0.004 28 19 26  -0.0243
49383.500  0.08571  0.47184 -27.869500  0.00004 0.00004 0.004 29 20 26  -0.0526
49384.500  0.08879  0.47117 -27.871800  0.00004 0.00004 0.004 29 20 26   0.1378
49385.500  0.09171  0.47023 -27.873900  0.00004 0.00004 0.005 29 20 26   0.0757
49386.500  0.09495  0.46996 -27.876000  0.00004 0.00004 0.005 29 20 26   0.0164
49387.500  0.09724  0.46956 -27.878100  0.00004 0.00004 0.005 29 20 26  -0.0055
49388.500  0.09912  0.46866 -27.880200  0.00004 0.00004 0.005 28 19 26  -0.0366
-------------------------------------------------------------------------------


  MJD          LODR    +/-
             (ms/day)

49382.5000    2.2757  0.004
49383.5000    2.2474  0.004
49384.5000    2.2378  0.004
49385.5000    2.1757  0.005
49386.5000    2.1164  0.005
49387.5000    2.0945  0.005
49388.5000    2.0634  0.005     
-----------------------------


ORBITS REPEATABILITY (cm):
(mean component error rms =sqrt((xrms**2 + yrms**2 + zrms**2)/3) )


            DAY 1  (32 h)              DAY 2  (32 h)
   |------------------------|--------|                            
 
                            |------------------------|--------|

   Six-hour overlap:        |xxxxxx|


   (only rms < 120 are used for MEAN)

Note: E - indicates that the satellite is in eclipse

---------------------------------------------------
                 RMS for DAY
PRN  030    031    032    033    034    035    036
-------------------------------------------------------
 1    15      8     18     17     10     43     26  
 2    56 E   48 E   38 E   28 E   42 E   30 E   29 E
 3    21     15     37     19     21     23     37  
 4    23     26     22     25     28     34     20  
 5    73 E  117 E   51 E   61 E   77 E   56 E   77 E
 7    19     19     14     15     18     17     20  
 9    17     23     29     23     17     16     17  
12     4     18     10     20     30      9     11  
13    11     16     15     16     19     19     16  
14    20     25     35     53     19     56     15  
15    22     24     18     30     25     23     36  
16    46     73     45      -      -     29     37  
17    25     49     51     29     40     52     49  
18    12     10     25     16     15     35     23  
19     9     26     32     39     12     36     30  
20    93 E   85 E   71 E   94 E   43 E   47 E   42 E
21    39     41     38     29     27     35     20 E
22    68 E  106 E   35 E   85 E   68 E   96 E   68 E
23    32     67     40     34     31     30     46  
24    -      -      34     33     27     29     26  
25    20     28     26     25     50     19     33  
26    38     17     29     66     27     32     29  
27    10     14     41     28     24     30     50  
28    22     32     25     20     24     52     36  
29    14     18     19     22     20     26     24  
31    29     55     15     25     22     45     50  
 
MEAN  37     48     34     40     33     39     37
---------------------------------------------------

REMARKS: (1) AS all days
         (2) PRN24 few data on day 30 (possible manoeuvre)
         (3) PRN16 manoeuvre on day 33 
                
CLOCK ESTIMATION:  ALGO was used as time reference



STATIONS USED BY GFZ INCLUDING STATISTICS

Sampling rate: 6 minutes         
                                                          
 IGS  INTERNAL         OBSERVATIONS for DAY
-----------------------------------------------------------
 CODE  STA#                30   31   32   33   34   35   36
-----------------------------------------------------------
onsa  105001   I'92      1577 1639 1626 1591 1636 1595 1636
kosg  110001 F I'92      1509 1409 1331  877 1051 1304 1711
madr  120001 F I'92      1664 1712 1609 1542 1375  839  112
mate  130001 F           1439 1256 1225 1216 1195 1296 1350
trom  150001 F I'92      1718 1763 1764 1676 1697 1738 1622
wetb  160001 F I'92      1371  993 1206 1248 1267 1268 1260
mets  180001   I'92      1474 1434 1575 1416 1291 1395 1420
usud  200002             1701 1487 1131 1080 1149 1455 1752
taiw  220001 F I'92      1540 1432 1520 1455 1385 1383 1581
tidb  305001 F           1626 1558 1179  548 1407 1056 1226
yar1  310001 F I'92      1646 1446 1334 1497 1363 1267 1392
hob1  320001             1653 1619 1645 1553 1577 1648 1655
algo  400001 F I'92      1349 1177 1390 1356 1199 1363 1345
stjo  405001 F           1686 1703 1751 1674 1692 1747 1739
wes2  408001             1677 1664 1673 1595 1619 1689 1710
gold  410001 F I'92       429 1654 1649 1515 1152 1126 1429
jplm  415001 F           1577 1224 1187 1186 1222 1090    0
fair  420001 F I'92      1540 1399 1355 1387 1390 1385 1470
yell  470001 F I'92         0  868 1756 1679 1696 1754 1600
drao  475001 F           1622 1449 1339 1510 1403 1244 1411
rcm5  482001   I'92      1598 1288 1289 1601 1757 1745 1757
sant  500001 F I'92      1507 1329 1154 1060 1189 1236  458
kour  510001 F           1499 1543 1458 1422 1440 1476 1549
fort  520001             1598 1570 1582 1516 1570 1631 1598
hart  600001 F I'92      1167 1045 1034  918 1003  874 1170
masp  610001 F I'92      1626 1706 1702 1646 1627 1678 1736
kokb  700001 F I'92       893 1370 1512 1300 1302 1404 1492
pama  710001             1468 1228 1149 1064 1244 1186 1051
mcmu  800002             1621 1313  645  638 1420 1453 1441
-----------------------------------------------------------

Note: F    - indicates a constrained fiducial site ( to 1-2 mm )
      I'92 - indicates that initial station coordinates are from ITRF'92



SATELLITES STATISTICS

                OBSERVATIONS for DAY
PRN      30   31   32   33   34   35   36
------------------------------------------
  1    1469 1484 1448 1409 1395 1387 1437
  2    1690 1641 1630 1555 1723 1720 1649
  3    1605 1792 1557 1644 1740 1730 1607
  4    1791 1713 1876 1855 1701 1673 1768
  5    1684 1555 1585 1603 1638 1655 1569
  7    2031 2000 1894 1679 1657 1822 1676
  9    1449 1375 1407 1543 1543 1475 1504
 12    1713 1787 1715 1723 1791 1770 1658
 13    1897 2130 2050 1980 2011 2035 2090
 14    1689 1592 1522 1607 1150 1480 1503
 15    1720 1573 1645 1516 1566 1626 1502
 16    1716 1589 1383    0 1117 1398 1507
 17    1454 1248 1168 1428 1395 1480 1343
 18    1649 1541 1497 1547 1649 1425 1582
 19    1509 1576 1448 1315 1515 1377 1473
 20    1548 1491 1573 1436 1465 1428 1362
 21    1613 1503 1524 1481 1504 1429 1363
 22    1553 1433 1463 1477 1509 1330 1350
 23    1635 1459 1558 1457 1551 1461 1474
 24     638 1576 1677 1528 1539 1620 1640
 25    1575 1621 1581 1438 1543 1504 1382
 26    1609 1402 1477 1405 1449 1450 1450
 27    1524 1463 1488 1477 1638 1561 1499
 28    1610 1443 1479 1574 1455 1407 1347
 29    1692 1612 1537 1498 1616 1500 1476
 31    1712 1679 1588 1591 1458 1582 1462
-----------------------------------------



SOLUTION CHARACTERISTICS

1. Software used :   EPOS.P.V2
2. Definition of Terrestrial Reference Frame
     Fiducial-free adjustment of all station coordinates.
     These  coordinates are then fixed in the determination of ERPs and ORBITS
 
3. Data used:
   - undifferenced carrier phases
   - 32 h arc solutions   

5. Adjusted parameters:
   - state vector of all satellites
   - coordinate corrections 
   - daily ERPs
   - tropospheric zenith path delay (4 h)
   - y-bias, solar radiation scaling factor
   - ambiguities
   - STA and SV clock parameters of each observation epoch
    



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