- Page 1 and 2: T 8 A N A L Y S I S CENTER WORKSHOP
- Page 3 and 4: FOREWORD The 1998 Analysis Centre W
- Page 5 and 6: TABLE OF CONTENTS Foreword . . . .
- Page 7 and 8: S. Schaer, W. Gurtner, J Feltens Th
- Page 9 and 10: Programme of Workshop 1
- Page 11 and 12: @esa m=l, ::=mlllll lx= mj:n IGS AN
- Page 13 and 14: ,.,,. ,:, -.. ., ,,.Y @esa 9=II::=R
- Page 15 and 16: EXECUTIVE SUMMARYl G. Beutler The 1
- Page 17 and 18: activities one has the problem that
- Page 19: future tasks are clearly defined. M
- Page 23 and 24: Ionosphere The position paper “IG
- Page 25 and 26: SUMMARY RECOMMENDATIONS OF THE DARM
- Page 27 and 28: 6. That a (super) combination of G-
- Page 29 and 30: Annex IGS Fiducials for ITRF Refere
- Page 31 and 32: ● coordinates and velocities of t
- Page 33 and 34: archiving, site and RINEX standards
- Page 35 and 36: it is unlikely that a single person
- Page 37 and 38: GOVERNING BOARD The Governing Board
- Page 39 and 40: Topic 1: The IGS Analysis Products
- Page 41 and 42: used, the consistency between all t
- Page 43 and 44: Consistency between the IGS orbits
- Page 45 and 46: Table 1. Median daily repeatabiliti
- Page 47 and 48: Of course the inclusion of bad sate
- Page 49 and 50: consistent with the IGS reference f
- Page 51 and 52: GNAAC, of providing station coordin
- Page 53 and 54: One large future “customer” of
- Page 55 and 56: seconds. A format for station and s
- Page 57 and 58: Zumberge, J. F., M. B. Heflin, D. C
- Page 59 and 60: INTRODUCTION PRECISE HIGH-RATE SATE
- Page 61 and 62: FIXED STATION CLOCKS APPROACH A sec
- Page 63 and 64: 250 -150- - -250- 3.00 3.33 3.66 4.
- Page 65 and 66: HIGH-RATE STATION CLOCKS One advant
- Page 67 and 68: INTRODUCTION THE IGS/BIPM TIME TRAN
- Page 69 and 70: A type of point positioning likely
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differences. This is probably suffi
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Topic 2: Orbit Prediction and Rapid
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The factors that limit the accuracy
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Table 1. Number of stations availab
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Table 3. Effect of different pertur
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Table 4. Orbit fit (7-day) and orbi
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A more than twofold improvement in
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60 40 Ii . . . ..- ● E WC.W 2 heu
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10 5 t t + IV (cm) ☞ ☞ IGS rapi
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Broc~dcast orbits for non—eclipsi
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Table 1. Effect of different Pertur
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where aD~, aDC, aDS, aye, aye, ays,
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: : m . > > : ~ ~ g z 2 CPS WEK (a)
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Table 2. Selected “optimal” orb
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lines in both plots showing the Do
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The RPR model is based on the time
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likely caused by the eclipsing sate
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Appendix This Appendix gives some s
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NEW SOLAR RADIATION PRESSURE MODELS
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120 100 20 \ lm 10m J-IA c Ic predi
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Using the current GNSS systems, use
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meter, this will be sufficient to p
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Standards and meteorological loggin
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decades, This package has been exte
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mainly due to the bad geometrical c
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corrections can be compensated by c
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These results can be compared with
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BACKGROUND POTENTIAL USE OF ORBIT P
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were used to validate the basic des
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METOP a.m. GRAS data as parl 0( the
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parameters of both the ‘model wor
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A critical aspect is given by the d
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Topic 3: IGS Reference Frame Realis
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“A global IGS reference system”
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determinations (largely free of the
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Fig. 2. of IGS he Proposed set of 5
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software. As seen from Table 2 and
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of about 0.2 mas are expected, it i
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. All the A-SINEX files (with stati
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choose (unconstrained, minimum) to
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and semiannual effects for some sta
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Zumberge, J. F, M.B. Heflin, D.C. J
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Africa/Arabia : BAHR r,e,n,s Z12 0.
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However there will be something lik
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TROM TSKB VILL WES2 WTZR YAR1 YELL
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Sigma CAS1 DAV1 MCM4 OHIG KERG Mean
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Example #1: Minimum datum (rotation
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APPENDIX VI SUGGESTIONS AND DISCUSS
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Table 1: 7 parameter orbit and stat
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ITRF96 AND FOLLOW ON FOR 1998 Claud
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Table 1. Global ITRF96 residuals pe
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INTRODUCTION IGS REFERENCE STATIONS
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Class D: Velocity residuals larger
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(MCM466001MO03). These stations sho
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ABSTRACT ESTIMATION OF NUTATION TER
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that the VLEII formal errors will o
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with oj denoting a combination of t
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Figure 5. 0.20 0.15 0.10 0.05 0.00
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GLOBALLY CONSISTENT RIGID PLATE MOT
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I The velocity of a point that is f
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mass (which we assume to be Euler
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otated into ITRF using a 14-paramet
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can arise because the station actua
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. In northern Algeria, convergence
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Topic 4: IGS Products for Troposphe
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that all coordinates refer to the s
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GFZ are extracted for 90 days at th
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15. ~2. CODE 9. 6. 3, 00 15. 12, 9.
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10 4 8. 2. I 890. 893. 8%. 899. 902
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18. 12. n 6. 2 ~ ‘“ N -6. -12.
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L 10. I 5. r o. L-- 97250. 40. 35.
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1. Verification of DWD Weather Fore
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5. DAILY BKG SOLUTION, GREF PART, D
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ESTIMATING HORIZONTAL GRADIENTS OF
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ABSTRACT IGS PRODUCTS FOR THE IONOS
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POTENTIAL PARTICIPANTS IN A ROUTINE
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TOWARDS A COMBINED IGS IONOSPHERE P
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GOALS AND NEXT STEPS For the near f
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IONEX: The ionosphere Map EXchange
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From method (1) to method (3), one
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Reading and Writing IONEX Modules F
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I I I I I I I I I contained in curr
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Table 2: Ionosphere map file — da
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1000 1000 1000 1000 1000 1000 1000
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1000 1000 1000 1000 1000 1000 1000
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Table 2: Differential code biases
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This equation can be rewritten in f
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In practice, the combined biases (r
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w o z w & LLl IL LL E DENT -BRUS (D
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10.00 ‘ - — 5.00 ‘- -- 0.00
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In a similar way as Wanninger (1994
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anging fi-om a few minutes to sever
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CONCLUSIONS The paper has outlined
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ABSTRACT MONITORING THE IONOSPHERE
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check and/or improve well-known ion
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1990). Collecting more and more TEC
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References Davies K., W. Degenhardt
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The main part of the paper will the
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One indicator of accuracy is the da
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Figure 3: Global TEC map from GE fi
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90 45 0 -45 -90 -100 -90 0 90 10< F
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When comparing the TEC maps in Figu
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Chapman Profile approach, thus prov
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points, but represent the integral
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Cosz cosine of slant range zenith d
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if not linear - the unknown paramet
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geometrical conditions can arise, a
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Establishment of Linearized Observa
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spending tracking data, the SST opt
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THE ROLE OF GPS DATA IN IONOSPHERIC
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(e.g., using the 40 and 360 MHz sig
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Retrospective nowcasting Retrospect
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(chairman: R. Leitinger, Austria, c
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● ● ● ● 24-hour global iono
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G .- 0 y 180 -150 -120 -90 -60 -30
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E 9 .2 ?: j ~ ?4 ?30 ~“ ~z % :’
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c c E c .- E! !2 %0 . m t 1 1 0 200
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,$ ., L r 1 (a) TEc maps Figure8. 2
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Rothacher, M., G. Beutler, E. Brock
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Experiences of the BKG in Processin
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RINEX N-l?ite for GPS modified Kepl
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The combined SP3-fde includes also
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1) Set up n single difference ambig
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0.10 a) z g 0.06 0.02 Figure 5: Fra
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[ 1) Compute triple difference resi
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PRECISE AUTONOMOUS EPHEMERIS DETERM
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ephemeris message will be computed
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The solution to the problem can be
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integration period, e.g. 5 minutes
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LATITUDE (DEG) 9L . . 6& - ;+5 ,- o
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First from the generation of the si
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it is believed that, with dedicated
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needed in order to use them as yard
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close to the maximum. It was decide
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Summary IGS Related Activities at t
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Table 1. Point positioning using NR
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ESA/ESOC IGS ANALYSIS CENTRE POSTER
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ESTIMATION OF MANOEUVRES Manoeuvres
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TROPOSPHERIC ESTIMATES Tropospheric
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Sever (JPL) and Gerd Gendt (GFZ). S
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A REVIEW OF GPS RELATED ACTIVITIES
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2.5 2.0 1.5 ~ 1.0 % E 0.5 x 0.0 -0.
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TEC from the CORS Network Figure 4
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REFERENCES Cartwright, D.E., and R.
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In recent years, the Bulletin A pol
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frequency reference. A second recei
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THE IGS REGIONAL NETWORK ASSOCIATE
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IJJcl UKJ 4“’’’’’’’
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W.-,-,- ,,, IJJ3 d , , , ,. . . . !
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Variations of weekly SIR R solution
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Variations of weekly SIR R solution
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Variations of weekly SIR R solution
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w’ —— L .sT41w.!l. c8Q#_. .J
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T HE N EWCASTLE G LOBAL N ETWORK A
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6 5 4 23 2 1 0 S TRATEGY Figure 2:
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IGS Workshop Dinner, Jagschloss Kra