[IGSREPORT-539] GFZ Analysis Report (week 716)

G. G.
Mon Oct 11 15:29:11 PDT 1993


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IGS Electronic Report     11-OCT-1993 15:29:11       Message Number 539
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>From : G. Dick
Subj : GFZ Analysis Report (week 716)

******************************************************************************
GFZ ANALYSIS REPORT   GPS-WEEK 0716 (DAYS 269-275, DATES 26-09-93 TO 02-10-93)
******************************************************************************

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) 310 648
              tel: (0331) 310 252 


PRODUCT SUMMARY

FILES SENT TO IGN: 
______________________________________________________________________________
gfz07167.sum           this text file
gfz07167.erp           Earth rotation parameters 
gfz0716[0-6].eph       Daily orbit ephemerides , SP1 format
______________________________________________________________________________


ERP RESULT

 
  MJD        X        Y      UT1-IAT     XSIG    YSIG                   STA SAT 
           arcsec   arcsec     sec      arcsec  arcsec   
49256.500 -0.09509  0.36175 -27.562242  0.00004 0.00004  0.0 0. 0. 0. 0. 28 25
49257.500 -0.09423  0.36380 -27.564408  0.00004 0.00003  0.0 0. 0. 0. 0. 27 25
49258.500 -0.09436  0.36584 -27.566574  0.00004 0.00003  0.0 0. 0. 0. 0. 28 25
49259.500 -0.09425  0.36764 -27.568740  0.00004 0.00003  0.0 0. 0. 0. 0. 27 25
49260.500 -0.09453  0.36958 -27.570962  0.00004 0.00003  0.0 0. 0. 0. 0. 28 25
49261.500 -0.09469  0.37105 -27.573184  0.00004 0.00004  0.0 0. 0. 0. 0. 27 25
49262.500 -0.09420  0.37293 -27.575406  0.00004 0.00004  0.0 0. 0. 0. 0. 26 25
-------------------------------------------------------------------------------


  MJD          LODR    +/-
             (ms/day)

49256.5000    2.3574  0.004
49257.5000    2.2830  0.004
49258.5000    2.2932  0.004
49259.5000    2.3034  0.004
49260.5000    2.2843  0.004
49261.5000    2.3542  0.004
49262.5000    2.4142  0.004
-----------------------------



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)

---------------------------------------
                 RMS for DAY
PRN   269  270  271  272  273  274  275
---------------------------------------
  1    29   31   37   27   37   30   34
  2    27   25   36   26   19   27   25  
  3    17   11   11   15   10   12   12
  5    74   73   68   61   70   46   36
  7    32   44   53   50   36   56   31
  9    20   23   24   20   20   24   22
 12    19   22   21   14   11   21   14
 13    42   17   21   16   18   33   35
 14    23   22   20   21   17   19   29
 15    44   38   14   36   34   50   24
 16    33   49   56   19   35   13   18
 17    21   16   16   18   16   22   13
 18    36   35   29   36   30   32   32
 19    17   21   15   17   17   21   14 
 20    22   18   29   23   18   25   25
 21    41   31   44   26   33   29   30
 22    15   20   18   18   17   18   25
 23    30   38   25   45   24   44   24
 24    46   13    -   27   14   23   16
 25    13   14   13    9   15   14   11
 26    29   36   27   33   27   53   27
 27    18   19   17   13   11   18   13
 28    22   23   23   19   29   44   20
 29    35   30   29   31   28   31   36
 31    31   31   32   29   28   45   22

MEAN   32   31   32   29   27   33   25
---------------------------------------

REMARKS: (1) AS on days 269-271
         (2) new satellite PRN05 was included in processing
         (3) on day 270 manoeuver of satellite PRN24


STATIONS USED BY GFZ INCLUDING STATISTICS

Sampling rate: 6 minutes
                                                          
 IGS  INTERNAL         OBSERVATIONS for DAY
 CODE  STA#       269  270  271  272  273  274  275
----------------------------------------------------
onsa  105001      1627 1568 1563 1628 1651 1632 1677
kosg  110001      1647 1450 1196  214  646 1470 1606
madr  120001      1608 1423 1565 1703 1593 1610 1610
mate  130001      1551 1522 1519 1552 1541 1507 1521
trom  150001      1716 1645 1587 1170  797 1641 1627
wetb  160001      1628 1579 1678 1689 1680 1487 1127
mets  180001      1686 1591 1413 1494 1547 1615 1591
usud  200002       932  928  967 1005  997 1349 1615
taiw  220001      1372 1289 1328 1380 1379 1337 1263
tidb  305001      1682 1639 1669 1704 1609 1615 1458
yar1  310001      1591 1608 1581 1607 1591 1586 1593
hob1  320001      1603 1575 1589 1582 1645 1695 1676
algo  400001      1516 1453 1569 1711 1699 1660 1687
stjo  405001      1680 1333 1453 1693 1679 1584 1687
wes2  408001      1580 1612 1658 1716 1717 1649 1686
gold  410001      1440 1488 1491 1529 1487 1250 1150
jplm  415001      1658 1605 1643 1663 1655 1622 1528
fair  420001       870    0 1048 1717 1735 1689 1676
yell  470001      1635 1631 1670 1670 1660 1616 1589
drao  475001      1468 1485 1512 1534 1548 1524 1533
rcm4  481001      1654 1586  575    0  349    0    0
sant  500001      1573 1593 1581 1651 1610 1447 1454
kour  510001      1566 1533 1598 1610 1579 1523 1504
hart  600001      1269 1191 1282 1348 1333 1225 1257
masp  610001      1717 1666 1737 1736 1729 1705 1679
kokb  700001      1708 1698 1667 1686 1449 1715 1671
pama  710001      1476 1600 1542 1507 1605 1011    0
mcmu  800001      1772 1778 1709 1690 1239  387 1570
----------------------------------------------------



SATELLITES STATISTICS

                OBSERVATIONS for DAY
PRN     269  270  271  272  273  274  275
------------------------------------------
  1    1853 1801 1779 1765 1672 1734 1754
  2    1557 1563 1508 1553 1498 1532 1505
  3    1987 1942 1948 1811 1891 1871 1897
  5    1447 1321 1371 1395 1508 1602 1547
  7    1740 1707 1685 1641 1589 1593 1548
  9    1674 1598 1646 1572 1568 1575 1472
 12    1805 1665 1684 1622 1596 1689 1637
 13    1896 1762 1741 1639 1628  593  672
 14    1796 1784 1746 1713 1700 1639 1750
 15    1532 1481 1512 1475 1392 1368 1390
 16    1532 1402 1434 1477 1516 1535 1582
 17    1573 1476 1470 1529 1596 1556 1536
 18    1855 1792 1815 1821 1793 1808 1848
 19    1647 1609 1630 1600 1581 1595 1574
 20    1986 1899 1896 1806 1798 1846 1774
 21    1525 1445 1475 1497 1420 1487 1482
 22    1998 1974 1999 1968 1927 1966 1880
 23    1490 1469 1358 1382 1333 1364 1449
 24    1642  867 1121 1586 1687 1717 1642
 25    2239 2190 2157 2107 2025 2016 1964
 26    1520 1537 1541 1539 1562 1492 1535
 27    1632 1604 1669 1642 1619 1567 1595
 28    1781 1736 1744 1658 1584 1675 1610
 29    1755 1696 1727 1674 1649 1660 1743
 31    1763 1749 1734 1717 1617 1671 1649
 -----------------------------------------



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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