[IGSREPORT-2204] Wk 0828 JPL Analysis Report
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Tue Dec 5 10:07:13 PST 1995
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IGS Electronic Report Tue Dec 5 10:07:13 PST 1995 Message Number 2204
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Author: D C Jefferson
Subject: Wk 0828 JPL Analysis Report
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JPL ANALYSIS REPORT GPS-WEEK 0828 (DAYS 323-329, DATES 1995 Nov 19 - Nov 25)
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Submitted by the JPL IGS/FLINN Analysis Team:
J F Zumberge, D C Jefferson, M B Heflin, M M Watkins, F H Webb
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 (128.149.70.41),
directory pub/jpligsac/0828. These files have also been sent to the CDDIS.
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filename contents
______________________________________________________________________________
jpl08287.sum This text file.
jpl08287.erp Earth rotation parameters for GPS week 828.
jpl08287.snx Ground station coordinates for GPS week 828, SINEX format.
jpl0828[0-6].sp3 GPS ephemerides for GPS week 828, sp3 format.
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Mean Orbit Repeatability (see table below): 20.4 cm
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: Data from PRN12 excluded days 323 and 324. No data available from this satellite thereafter.
WARNING: NLIB (not ALGO) used as reference clock on days 327 and 328.
WARNING: PIE1 (not ALGO) used as reference clock on day 329.
WARNING: Data from CMP9, FARB, HART, LHAS, PAMA, SANT, TABL, WETT excluded day 323.
WARNING: Data from JOZE, KOKB, MATE, ONSA, PAMA, SANT, TABL, WETT excluded day 324.
WARNING: Data from KOKB, MATE, ONSA, SANT excluded day 325.
WARNING: Data from CMP9, FAIR, LONG, MATE, MONP, ONSA excluded day 326.
WARNING: Data from BOR1, BRAN, GRAS, HART, KELY, MATE, MONP, NOTO, OHIG, SEY1, TABL, UPAD excluded day 327.
WARNING: Data from HART, KOSG, TABL, WETT excluded day 328.
WARNING: Data from ANKR, NOTO, TABL, WETT excluded day 329.
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 828 (1995 Nov 19 - Nov 25)
MJD XPole Ypole UT1R-UTC LODR Xsig Ysig UTsig LODsig Nr Nf Nt Xrt Yrt
10**-5" usec us/d 10**-5" us us/d 10**-5"/d
50040.50 -4443 9302 -335970 2654 6 7 12 12 37 8 24 -391 129
50041.50 -4815 9397 -338615 2637 5 6 12 12 37 10 24 -402 127
50042.50 -5260 9521 -341255 2642 5 6 12 12 37 11 24 -404 117
50043.50 -5683 9634 -343919 2686 5 5 13 13 37 12 24 -386 85
50044.50 -6083 9660 -346577 2631 5 6 12 12 37 9 24 -360 77
50045.50 -6400 9797 -349220 2655 5 6 12 12 37 8 24 -368 119
50046.50 -6752 9981 -351890 2685 5 5 12 12 37 10 24 -344 155
END ERP TABLE
The following table indicates the "3-dimensional orbit repeatability", as
defined in IGS Mail Message 37, for GPS week 828:
["3d rss" = sqrt(xrms**2 + yrms**2 + zrms**2)]
JPL ORBIT REPEATABILITY TABLE GPS week 828 (1995 Nov 19 - Nov 25)
95 11 19 95 11 20 95 11 21 95 11 22 95 11 23 95 11 24 95 11 25
prn 3d rss (m)
1 0.26 0.23 0.26 0.33 0.30 0.22 0.21
2 0.16 0.17 0.20 0.34 0.28 0.10 0.11
4 0.11 0.13 0.19 0.29 0.33 0.12 0.10
5 0.14 0.10 0.19 0.32 0.33 0.26 0.22
6 0.15 0.15 0.12 0.14 0.12 0.09 0.14
7 0.13 0.17 0.14 0.19 0.16 0.20 0.16
9 0.16 0.15 0.13 0.15 0.28 0.12 0.19
14 0.15 0.10 0.16 0.13 0.10 0.11 0.20
15 0.33 0.25 0.21 0.24 0.16 0.13 0.32
16 0.24 0.19 0.11 0.21 0.25 0.11 0.15
17 0.21 0.27 0.14 0.19 0.22 0.28 0.32
18 0.12 0.07 0.11 0.10 0.31 0.23 0.17
19 0.24 0.44 0.31 0.15 0.23 0.21 0.17
20 0.21 0.21 0.21 0.33 0.34 0.24 0.23
21 0.11 0.30 0.31 0.14 0.24 0.13 0.12
22 0.13 0.10 0.15 0.20 0.33 0.21 0.19
23 0.39 0.44 0.54 0.79 0.71 0.47 0.52
24 0.15 0.16 0.11 0.15 0.24 0.06 0.13
25 0.12 0.11 0.15 0.24 0.20 0.18 0.16
26 0.10 0.12 0.19 0.13 0.14 0.12 0.18
27 0.18 0.09 0.17 0.13 0.17 0.17 0.22
28 0.15 0.18 0.23 0.27 0.22 0.15 0.15
29 0.12 0.14 0.18 0.10 0.34 0.33 0.23
31 0.17 0.16 0.26 0.17 0.16 0.19 0.16
_______________________
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 828 (1995 Nov 19 - Nov 25)
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)
| | | | | | |
|___ |__ |_______ |_______ |___ |___ |__
ALBH 2.9 22.7 3.19 38.4 4.00 2.61
ALGO* 4.7 .124 1.39 43.9 4.05 3.04
ANKR 1.5 .246e+04 -.276e-02 59.4 4.60 2.08
AREQ 6.9 79.7 .545e-01 45.6 5.59 2.63
AUCK 4.9 72.0 .111 40.1 4.68 2.74
BOR1 1.0 2.07 -.675 34.0 3.00 2.94
BRMU 5.9 105. .610e-01 41.5 6.02 2.90
BRUS 2.0 .298 1.49 61.5 4.00 2.80
CAS1 6.9 16.2 348. 57.3 5.03 1.69
CHAT 1.0 89.2 .715e-01 87.0 5.00 1.85
CICE 4.9 83.7 .568e-01 32.2 3.69 2.77
CRO1 6.9 128. .514e-01 44.1 6.47 2.24
FAI2 .9 .234 -.325 45.0 4.00 2.33
FAIR* 6.0 .124 -.437 . 4.33 2.06
FORT 1.7 80.0 -.214e-01 50.5 6.54 2.90
GODE 1.0 .277 16.0 44.0 4.00 2.57
GOLD* 6.3 .692 -.627 . 3.00 2.44
GRAS 1.0 78.9 .543e-01 36.0 4.00 2.52
GUAM 6.9 91.7 .575e-01 50.4 8.38 2.46
HART* 3.9 47.3 10.7 . 8.00 1.86
HOB2 6.0 .185 -.166 48.5 4.88 2.80
IISC 2.9 117. -.229 65.4 5.32 2.20
IRKT 3.7 91.9 .219 53.1 4.00 2.71
JOZE 1.0 45.3 985. 57.0 8.00 2.31
KELY 2.4 .169e+05 3.37 59.3 6.00 1.92
KERG 6.9 138. -277. . 5.46 2.50
KIRU 6.0 3.12 11.7 54.5 7.00 2.10
KIT3 3.7 109. .190 98.4 4.26 2.85
KOK2 6.4 25.9 .150 54.9 5.51 2.37
KOKB* 3.9 .126 -1.77 . 5.81 2.28
KOSG* 4.9 24.6 2.72 . 3.82 2.23
KOUR 6.9 2.93 40.6 . 8.30 2.07
LHAS 4.7 .199e+04 .242 77.1 4.22 2.36
MAC1 4.9 .459e+05 -.327e+04 32.8 3.88 2.41
MADR* 6.3 .197 -.498 . 4.75 2.33
MAS1 2.5 444. .475 152. 6.08 1.62
MCM4 5.8 102. -.122 46.0 5.36 1.69
MDO1 2.0 1.30 -.592 33.0 4.00 2.92
MDVO .8 .238 10.6 71.0 5.00 2.38
METS .9 .564e-01 -13.2 108. 3.00 1.91
NLIB 1.9 . . 37.5 4.00 2.79
NOTO 2.9 .177 -14.1 31.4 4.34 3.04
OHIG 1.4 .552e+05 .411 54.8 4.44 1.20
PAMA 4.9 11.7 .407 . 13.0 .835
PERT 6.9 38.0 16.5 50.0 5.09 2.88
PIE1 1.0 . . 36.0 4.00 2.88
QUIN 1.8 .108e+04 -.163 46.0 5.00 1.99
RCM5 5.8 .783 .367 49.7 4.36 3.03
SANT* 3.9 .172 .341 . 5.00 2.43
SEY1 5.8 .821e+07 -.150e+05 . 8.67 1.61
SHAO 6.9 88.0 .531e-01 116. 4.31 1.82
STJO 5.9 2.93 2.09 46.6 4.39 2.81
THU1 2.7 67.7 -.115 50.3 5.00 2.51
TID2 .9 .215 -.289 47.0 5.00 3.55
TIDB* 6.7 .597 .315 . 5.03 2.58
TMGO .7 79.1 -.222 42.0 5.00 3.11
TROM* 3.9 5.52 204. . 4.79 1.53
TSKB 3.0 13.6 -57.7 56.8 3.97 2.94
USUD 2.9 1.00 -.172 36.7 4.69 2.51
VILL .9 .605e+04 4.25 56.0 5.00 3.03
WETT* 2.9 .151 .552 . 6.67 2.18
YAR1* 5.8 170. .520 . 4.26 2.22
YELL* 5.9 .115 .151 43.4 4.00 2.28
ZWEN 1.8 103. -.103 60.0 4.53 2.25
PRN01 6.9 79.3 596. 57.7 5.59 2.22
PRN02 6.9 79.4 -210. 50.7 5.45 2.52
PRN04 6.7 81.1 54.3 55.8 5.72 2.05
PRN05 6.9 79.7 10.9 57.8 5.18 2.11
PRN06 6.9 81.5 3.01 54.8 5.30 2.36
PRN07 6.9 80.6 712. 53.8 5.45 2.21
PRN09 6.6 81.4 -1.86 58.2 5.32 2.18
PRN14 6.9 81.5 11.9 54.3 5.31 2.33
PRN15 6.4 3.42 245. 57.7 5.30 2.06
PRN16 6.9 81.5 -144. 54.2 5.72 2.15
PRN17 6.8 82.1 -98.7 54.4 5.45 2.21
PRN18 6.9 82.2 -4.31 51.4 5.59 2.20
PRN19 6.8 82.2 146. 53.2 5.46 2.18
PRN20 6.9 82.2 57.8 57.6 5.30 2.11
PRN21 6.8 80.7 -7.75 57.6 5.31 2.63
PRN22 6.9 80.7 265. 50.9 5.45 2.46
PRN23 6.9 81.0 3.94 57.7 5.45 2.18
PRN24 6.7 81.6 279. 58.2 5.58 2.06
PRN25 6.8 82.8 .508 56.3 5.73 2.16
PRN26 6.9 80.0 -115. 51.8 5.73 2.35
PRN27 6.8 80.4 10.2 53.7 5.60 2.30
PRN28 6.9 1.85 49.3 94.6 4.74 2.74
PRN29 6.9 80.4 3.36 49.3 5.46 2.44
PRN31 6.9 79.8 56.3 52.8 5.59 2.31
_______________________
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
95 11 19 95 11 20 95 11 21 95 11 22 95 11 23 95 11 24 95 11 25
prn 3d rss (m)
1 6.0 4.6 5.5 5.9 3.3 4.3 5.2
2 4.7 9.8 9.4 9.2 9.1 12.2 9.7
4 4.9 6.0 5.9 5.5 5.3 6.1 5.0
5 5.4 8.7 7.1 7.8 9.4 10.4 10.1
6 3.9 4.2 4.6 3.8 4.0 4.6 5.4
7 5.2 5.3 5.2 4.4 5.7 5.2 5.0
9 6.4 4.6 5.8 5.5 3.6 4.8 5.1
14 2.2 2.8 3.5 3.8 2.2 2.4 2.8
15 4.8 4.7 4.0 5.5 6.5 5.7 4.9
16 5.2 4.6 5.4 5.5 7.1 6.4 4.8
17 5.0 4.6 4.0 3.1 3.6 3.9 4.8
18 5.6 6.1 5.8 5.1 5.5 5.0 5.3
19 5.1 5.9 5.7 4.8 4.9 4.8 5.4
20 7.7 8.5 8.9 6.0 8.9 10.2 10.8
21 5.2 5.9 5.5 5.1 4.2 5.1 2.9
22 8.0 8.1 3.3 4.4 5.3 7.1 10.4
23 4.6 2.8 3.8 2.8 3.1 2.3 6.0
24 5.8 5.6 5.5 5.5 6.4 5.5 5.1
25 7.3 8.2 6.3 6.0 6.1 7.9 9.1
26 12.2 14.6 14.0 11.5 12.8 11.5 12.3
27 5.1 5.6 6.2 6.4 8.4 9.0 8.6
28 3.0 3.1 4.0 4.9 4.7 6.7 3.3
29 4.0 3.9 3.2 4.9 4.6 3.5 4.2
31 2.5 3.0 2.5 3.1 4.3 2.7 2.5
_______________________
END COMPARISON OF BROADCAST NAVIGATION MESSAGE WITH PRECISE EPHEMERIDES
[Mailed From: djeff at cobra.jpl.nasa.gov]
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