IDS's first contribution to the realization of the ITRF (International Terrestrial Reference Frame)
was the provision of individual solutions for ITRF2005 by two analysis centers (IGN, LEGOS-CLS).
Previously, DORIS solutions produced by four groups had been included in the ITRF computations:
ITRF94, ITRF96, ITRF97: contributions of CSR, GRGS and IGN 
ITRF2000: contributions of AUSLIG, GRGS and IGN

Find below elements about the IDS contribution to the following ITRS realizations:

ITRF2020 | ITRF2014 | ITRF2008 | ITRF2005

 

 

 


Contribution to ITRF2020

(ITRF web page)

The IDS 16 series is the DORIS contribution to the ITRF2020. This product is referenced with a DOI: 10.24400/312072/i01-2021.001 (follow the link to read more). 

See the page: "IDS 16 - Contribution to ITRF2020

 

 

 


Contribution to ITRF2014

(intially scheduled to be ITRF2013) (ITRF web page)

Data Analysis Summary of the DORIS weekly SINEX series used in the IDS combination for the realization of ITRF2014

 

 Sinex Series
 Name  grgwd40  gscwd23  gopwd43  esawd10  ignwd15  inawd08
 Description form  TBD  TBD  TBD  TBD  TBD  TBD
 Analysis Center
 Name  CNES/ CLS  NASA/ GSFC  GOP  ESA/ ESOC  IGN  INASAN
 Contact  H. Capdeville  F. Lemoine  P. Stepanek  M. Otten  P. Willis  S. Kuzin
 Additionnal contacts  J.M. Lemoine, L. Soudarin  D. Chinn  N/A  N/A  N/A  S. Tatevian
 Software
 Name and version  GINS v 13.2d1  GEODYN  Bernese 5.0 (DORIS development version)  NAPEOS 3.7  GIPSY-OASIS II  GIPSY-OASIS II (v. 6.2)
 SINEX Method (NEQ or COV)  COV  NEQ  COV  NEQ  COV  COV
 Data weights (data reduction)  0.3 mm/s  2.0 mm/s (upweighted at NEQ stage, sat by sat basis)  3 mm (range difference)  0.5 mm/s  0.51 mm/s for SPOT2, SPOT3, SPOT4, TOPEXENVISAT, CRYOSAT2; 0.4 mm/s for SPOT5, JASON2, HY2A and SARAL  0.51 mm/s for SPOT2, SPOT3, SPOT4, TOPEX, ENVISAT, CRYOSAT2; 0.4 mm/s for SPOT5, JASON2
 If COV, Station Constraint  10 m  N/A  10 m  NEQ  10 m  10 m
 If COV, EOP Constraint  15 m  N/A  Xp, Yp 500 mas  NEQ  5 m  5 m
 Satellite
 satellites included in weekly SINEX  start-end  start-end  start-end  start-end  start-end  
 SPOT2  03/01/1993 -
 18/07/2009
 03/01/1993 -
 18/07/2009
 03/01/1993 -
 14/07/2009
 03/01/1993 -
 13/07/2009
 03/01/1993 -
 14/07/2009
 03/01/1993 -
 14/07/2009
 SPOT3  30/01/1994 -
 16/11/1996
 30/01/1994 -
 16/11/1996
 01/02/1994 -
 12/11/1996
 02/02/1994 -
 12/09/1996
 02/02/1994 -
 14/11/1996
 01/02/1994 -
 13/11/1996
 SPOT4  03/05/1998 -
 22/06/2012
 03/05/1998 -
 31/12/2012
 10/05/1998 -
 22/06/2013
 03/05/1998 -
 24/06/2012
 01/05/1998 -
 18/06/2013
 01/05/1998 -
 23/06/2013
 SPOT5  16/06/2002 -
 27/12/2014
 16/06/2002 -
 31/12/2012
 16/06/2002 -
 30/08/2014
 17/06/2002 -
 31/12/2013
 11/06/2002 -
 31/12/2013
 11/06/2002 -
 31/12/2013
 TOPEX  03/01/1993 -
 30/10/2004
 03/01/1993 -
 30/10/2004
 03/01/1993 -
 30/10/2004
 03/01/1993 -
 31/10/2004
 01/01/1993 -
 01/11/2004
 03/01/1993 -
 01/11/2004
 ENVISAT  21/07/2002 -
 07/04/2012
 21/07/2002 -
 07/04/2012
 21/07/2002 -
 07/04/2012
 21/07/2002 -
 07/04/2012
 11/04/2002 -
 08/04/2012
 02/06/2002 -
 08/04/2012
 JASON1  31/10/2004 -
 12/07/2008
 31/10/2004 -
 12/07/2008
 N/A  TBD  N/A  N/A
 JASON2  13/07/2008 -
 27/12/2014
 13/07/2008 -
 31/12/2012
 13/07/2008 -
 30/08/2014
 14/07/2008 -
 31/12/2013
 12/07/2008 -
 31/12/2013
 12/07/2008 -
 31/12/2013
 CRYOSAT2  20/06/2010 -
 27/12/2014
 20/06/2010 -
 31/12/2012
 30/05/2010 -
 30/08/2014
 30/05/2010 -
 31/12/2013
 30/05/2010 -
 31/12/2013
 30/05/2010 -
 31/12/2013
 HY2A  02/10/2011 -
 27/12/2014
 TBD  01/01/2012 -
 30/08/2014
 02/10/2011 -
 31/12/2013
 01/10/2011 -
 31/12/2013
 N/A
 SARAL  17/03/2013 -
 27/12/2014
 TBD  N/A  TBD  15/03/2013 -
 31/12/2013
 N/A
 Arc cut
 Arc lengths  3.5 days nominally (minimum 1 day)  7.0 days, typically  1 day  1 day  1 day  1 day
 Handle of Manoeuvers  Break arc and Restart at 12am or 12pm; estimated from 2012/01/01  Truncate arc before maneuver. Restart 1-2 hrs afterward.  daily arc not processed  Included for all satellites with manoeuvre info, others excluded for that day  Break arc and start or end at 12:00  Break arc and start or end at 12:00
 Handle of Data gaps  Arcs truncated for large data gaps and Restarted.  Arcs truncated for large data gaps and restarted.  daily arcs with large data gaps not processed  Nothing  daily arcs with large data gaps not processed  daily arcs with large data gaps not processed
 Additional margins  6hrs before and 6 hrs after for POD but not in SINEX  None  None  None  3hrs before and 3 hrs after for POD but not in SINEX  3hrs before and 3 hrs after for POD but not in SINEX
 Reference System
 Earth reference system  DPOD2008v12  DPOD2008v12  DPOD2008v12  DPOD2008v12  DPOD2008 v1.13  DPOD2008 v1.13
 Celestial reference system  inertial J2000  inertial J2000  inertial J2000  inertial J2000  inertial J2000  inertial J2000
 Polar motion and UT1  IERS C04 08  IERS C04  IERS C04  IERS C04 08  IERS Bulletin A  IERS Bulletin A
 Background C21, S21    IERS 2010 (Equation 6.5, Petit and Luzum, 2010)  IERS 2010 Conventions  IERS 2010 (Equation 6.5, Petit and Luzum, 2010)  IERS 2003  IERS 2003
 Pole model    IERS 2010, (Table 6.6, Petit & Luzum, 2010)  IERS 2010 Conventions  IERS 2010, (Table 6.6, Petit & Luzum, 2010)  IERS 2010  IERS 2010
 Precession/Nutation  IERS 2010 using NRO origin  IERS 2003  IERS 2003  IERS 2010  IERS 2010  IERS 2010
 Station coordinates  DPOD2008v12  DPOD2008v12  DPOD2008v12  DPOD2008v12  DPOD2008 v1.13  DPOD2008 v1.13
 Displacement of reference points
 Solid Earth tidal displacement  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions
 Ocean loading  FES 2012  GOT4.8  FES 2004  EOT11a  FES 2004  FES 2004
 Tidal atmospheric loading  S1/S2 Ray & Ponte (2003)  none  N/A  S1/S2 Ray & Ponte (2003); Also P1, K1; T2, R2.  not applied  not applied
 Non tidal atmospheric loading  none  not applied  N/A  none  not applied  not applied
 Solid pole tide displacement  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions
 Ocean pole tide displacement  none  Applied.  N/A  not applied  applied  applied
 Tidal Geocenter    Applied, GOT4.7  N/A      
 Satellite reference
 Mass and center of gravity  initial values and time evolution from IDS files "sat"mass.txt  Initial values and time history from IDS files.  Initial values from IDS files  Initial values and time history from IDS files.  Initial values and time history from IDS files  Initial values and time history from IDS files
 Attitude Model  nominal laws  Attitude model, generally; Quaternions for off-nominal TOPEX arcs; Quaternions for Jason-1, Jason-2. Ejo/TU Delft quaternions for Cryosat-2  nominal laws, GSC tunned for SPOTs  nominal laws  nominal laws  nominal laws
 Gravity
 Gravity field (static)  EIGEN-6S2  GOCO02s  EIGEN-6S2 after 2002.0, EIGEN-GL04S1 before 2002.0  EIGEN-6S2  EIGEN-6S2.extended.v2.gfc  GOCO2S
 Gravity field (time varying)  EIGEN-6S2 up to degree 95 including time variable terms up to degree 50 (bias & drift per yr from 2002 to 2012, periodic 18.6, 1, 0.5yrs)  (1) to 5x5 - fit to SLR,DORIS time series; (2) > 5x5. Annual terms from GSFC-derived GRACE solutions.  EIGEN-6S2 after 2002.0,var. terms up to deg. 50. No harmonic terms before 2002.0  EIGEN-6S2 up to degree 120 including time variable terms up to degree 50 (bias & drift per yr from 2002 to 2012, 1, 0.5yrs)  from EIGEN-6S2.extended.v2.gfc  (1) to 4x4 - fit to SLR,DORIS time series; (2) > 4x4. Annual terms from GSFC-derived GRACE solutions
 Solid Earth tides  IERS 2010 conventions  IERS 2003  IERS 2010 conventions  IERS 2010 conventions  IERS 2010  IERS 2010
 Ocean tides  FES 2012 (32 principal waves, + 60 admittance waves) up to degree 50  GOT4.8  FES 2004  EOT11a up to degree order 50  FES 2004  FES 2004
 Atmospheric gravity  3hr ERA-interim / ECMWF up to degree 50  ECMWF-6hr (Re-analysis) to 50x50  ECMWF-6hr up to 20X20  AGRA-6hr to 20x20  not applied  not applied
 Air Tides     Ray and Ponte (2003), S1, S2; K1, P1, R2, T2            
 Non tidal oceanic gravity  TUGO R12 up to degree 50 TUGO R12 up to degree 50  N/A  N/A  N/A  not applied  not applied
 Atmospheric tides  none (considered through the ECMWF atmospheric data)  Terms removed from ECMWF fields applied separately  N/A  none  not applied  not applied
 Earth pole tide  IERS 2010 conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions
 Ocean pole tide  Desai 2002 up to degree 12  Desai, 2002. Applied to 50x50  C21, S21 IERS Conventions 2010  IERS 2010 Conventions  IERS 2010 Conventions  IERS 2010 Conventions
 Third bodies  Sun, Moon, Mars, Venus, Jupiter, Saturn, Uranus and Neptune ephemeris : DE421 (JPL)  Sun, Moon, Planets: DE403 (JPL)  Sun, Moon, Major Planets DE405  Sun, Moon, Planets: DE405 (JPL)  Sun, Moon, Planets: DE421 (JPL)  Sun, Moon, Planets: DE421 (JPL)
 Surface forces and empiricals
 Radiation Pressure model  Thermo-optical coefficient from pre-launch box and wing model, with smoothed Earth shadow model; models from CNES document for all satellites except tuned macromodels for Spot-2, -3, -4, Jason2  SPOT-2, SPOT-3: Macromodel Updated from LeBail et al. (2010); SPOT-4: LeBail et al. (2010); SPOT-5: Le Bail et al. (2010) + variable solar array pitch modelled after January 2008; Cryosat2: CNES (7plate) macromodel; Jason-2: CNES (Modified macromodel); TOPEX: Marshall et al. (1995), Marshall and Luthcke (1994); University of College London (UCL) models for Jason-1, and Envisat.  Thermo-optical coefficient from pre-launch box and wing model, with smoothed Earth shadow model; models from CNES document for all satellites except tuned macromodels for Spot-2, -3, -4  CNES model for all satellites except for Jason-1/2 (tuned), TOPEX (GSFC values) and Enivsat (ANGARA model)  CNES model for all satellites except for Jason-2 (tuned) and Cryosat2 (modified CNES 7plate macromodel)  CNES model for all satellites except for Jason-2 (tuned) and Cryosat2 (modified CNES 7plate macromodel)
 Radiation pressure scale coefficient  1 coef/day but strongly constrainted (1. e-4) to: 1.03 for Topex; 1.07 for Spot-2; 1.07 for Spot-3; 1.16 for Spot-4; 1.05 for Spot-5; 1.05 for Envisat; 0.94 for Jason-1, 0.97 for Jason-2; 1.00 for Cryosat-2; 0.86 for HY-2A; 1.00 for Saral  Cr=1.00 for satellites except, For Jason-2: Cr= 0.945; For Envisat Cr=1.0041747;  1 coeff/day. First iteration without 1-rev parameters, in second iteration constrained (1.e-1)  fixed, TOPEX 1.03 SPOT-2/3 1.08 SPOT-4 0.98 SPOT-5 1.04 JASON-1 1.0 JASON-2 0.98 ENVISAT 0.98 CRYOSAT-2 1.0 HY-2A 1.0  fixed: TOPEX 1.03; SPOT-2/3 1.08; SPOT-4 1.13; SPOT-5 1.03; JASON-2 0.92; ENVISAT 1.02; CRYOSAT2 1.05; SARAL 1.08; HY2A 0.88  fixed: TOPEX 1.03; SPOT-2/3 1.08; SPOT-4 1.13; SPOT-5 1.03; JASON-2 0.92; ENVISAT 1.02; CRYOSAT2 1.05
 Earth radiation  Albedo and IR pressure values interpolated from ECMWF 6hr grids  Knocke et al. (1988)  apriori model using CERES data  Monthly mean Albedo and IR maps at 2.5x2.5 degrees  Albedo correction applied  Albedo correction applied
 Atmospheric density model  DTM 94, with best available solar activity  MSIS86  MSIS86  MSIS2000  DTM94  DTM2000
 Drag coefficients  Adjusted; Spots, Envisat, Cryosat2, HY-2A, Saral: 1 coef/4 hours (1/1hr in high solar activity periods) ; Topex,Jasons: 1 coef/half day  Cd/8hrs (TOPEX, Jason-1, Jason-2); Cd/1-2 hrs for 800-km satellites depending on solar flux.  adjusted 1 coeff./30 minutes for 800-km atellites, 1 coeff./6 hours for others  TOPEX, Jason 4 a day rest 10 drag coefficients a day  Cd/8hrs (TOPEX, Jason-2); Cd/1hr for SPOT-2,3,4,5, ENVISAT, CRYOSAT2, HY2A and SARAL  Cd/8hrs (TOPEX, Jason-2); Cd/1hr for SPOT-2,3,4,5, ENVISAT, CRYOSAT2
 1/rev empiricals  2 coeff cos-sin /orbital period in normal direction ; 2 coeff cos-sin /orbital period in tangential direction ; per arc  Opr/day along+ cross-track  Opr/day along (cross not adjusted)  Opr/day along+ cross-track  Opr/day along + cross-track  Opr/day along + cross-track
 DORIS measurements
 Troposphere Model  GPT2/VMF1  Saastamoinen  Saastamoinen  Saastamoinen  none  none
 Weather (meteorological data)     GPT  GPT  GPT  not used  not used
 Troposphere mapping function     GMF  GMF  GMF  VMF1  GMF
 Troposphere correction  One zenith delay/pass (wet tropo scale factor adjusted) + one daily tropospheric gradient per station in North & East directions  Scale factor/pass estimated for wet correction only.  One zenith delay/pass (wet tropo scale factor adjusted)  One zenith delay/pass  (wet tropo scale factor adjusted) + one daily tropospheric gradient per station in North & East directions  wet tropospheric delay estimated per station with reset for some passes only if separated by more than 20 minutes  wet tropospheric delay estimated per station with reset for some passes only if separated by more than 20 minutes
 2nd order ionosphere  Not applied  Not applied  N/A  Not applied  Not applied  Not applied
 Frequency  1 frequency bias adjusted per pass  Range-rate bias adjusted/pass; Change in nominal beacon frequency accommodated with modification of partial derivatives.  1 frequency bias adjusted per pass  Range-rate bias adjusted/pass; Change in nominal beacon frequency accommodated with modification of partial derivatives.  1 frequency bias adjusted per station clock if separated by more than 20 minutes + 1 frequency bias per satellite clock (except 1) if separated by more than 20 minutes  1 frequency bias adjusted per station clock if separated by more than 20 minutes + 1 frequency bias per satellite clock (except 1) if separated by more than 20 minutes
 Relativity  Schwarzschild model + Lense-Thirring + geodesic precession  Schwarzschild model + Lense thirring + geodesic precession  Schwarzschild model + Lense-Thirring + geodesic precession  Schwarzschild model + Lense thirring + geodesic precession  Schwarzschild model + Lense-Thirring + geodesic precession  Schwarzschild model + Lense-Thirring + geodesic precession
 Weight  models: 0.3 mm/s; measurements: derived from observation standard deviation in data files  2 mm/s. upweighted per satellite at NEQ level.  3 mm (range difference)  0.5mm/s  0.51 mm/s for SPOT2, SPOT3, SPOT4, TOPEX, ENVISAT, CRYOSAT2; 0.4 mm/s for SPOT5, JASON2 , HY2A and SARAL  0.51 mm/s for SPOT2, SPOT3, SPOT4, TOPEX, ENVISAT, CRYOSAT2; 0.4 mm/s for SPOT5, JASON2
 Elevation angle cutoff  12 degrees  10 degrees  10 degrees  7 degrees  7 degrees  12 degrees
 Downweighting law  Downweighting law for elevation <= 20 deg; Weight of the observation is multiplied by the factor elevation**2/400 with elevation in degrees)  none  none  TBD (currently sin(elevation) after 2002)  1/sqrt(sin(elevation))  1/sin(elevation)
 Satellite system  Center of mass - antenna phase center vector computed from macro model + attitude law; no phase law applied  tracking point offset applied using offset information and attitude law and quaternions for spacecraft.  Center of mass - antenna phase center vector computed from macro model + attitude law; no phase law applied  Center of mass - antenna phase center vector computed from macro model + attitude law; no phase law applied  Center of mass - antenna phase center vector computed from macro model + attitude law; no phase law applied  Center of mass - antenna phase center vector computed from macro model + attitude law; no phase law applied
 Ground system  Phase centre / reference point vector from manufacturer values; phase law applied (Alcatel, Starec version 2013)  Phase correction + vertical eccentricity applied in GEODYN or through modification of DPOD2008v12 station coordinates  Phase centre / reference point vector from manufacturer values; phase law applied (Alcatel, Starec version 2013)     Phase centre / reference point vector from manufacturer values; phase law applied (Alcatel, Starec)  Phase centre / reference point vector from manufacturer values; phase law not applied (Alcatel, Starec)
 DORIS System Time Bias     Model applied for TOPEX/Poseidon derived from SLR-DORIS arcs.  N/A        no bias correction applied to satellite clock
 South Atlantic Anomaly  Corrective model for Jason-1; corrected measurements for Spot-5 from 2006 only  Corrective model applied for Jason-1; Corrective model applied for SPOT-5 (2006.0 - onward)  Corrected measurements for Spot-5 (2006.0 - onward). Jason-1 data not used at all  Corrective model for Jason-1; corrected measurements for Spot-5 from 2006 only  Jason-1 data not used at all; corrective model applied for SPOT-5 (2006.0 - onward) . A few stations removed for SPOT-5 data (Arequipa, Cachoeira, Easter Island, Kourou)  Jason-1 data not used at all; corrective model applied for SPOT-5 (2006.0 - onward)

 

 

 

 


Contribution to ITRF2008

(ITRF web page

(First iteration Feb. 2009) (Last iteration Nov. 2009)
The IDS-3 SINEX time series may be downloaded at documents/BC/combinations/ITRF2008-IDS/IDS-3/

ITRF2008 Call

 

IDS Analysis

Two IDS Analysis Working Group meetings have been organized in March and June 2008 in Paris, Bureau des Longitudes, and an IDS workshop in Nice, 12-14 November 2008. Eight DORIS analysis centers participated including four official analysis centers (IGN; LCA ; GOP ; ESA), and four candidate analysis centers (NCL - University of Newcastle; GAU - Geoscience Australia; INA - Institute of Astronomy, Russian Academy of Sciences, and GSC - NASA Goddard Space Flight Center). All these centers are working to provide SINEX solutions for inclusion in the IDS combined solution that will be submitted to the IERS for ITRF2008.

This is an important step for IDS Analysis centers! Indeed for ITRF2005, only two individual DORIS solutions were included: IGN and LCA. A main goal was to improve the models and processing strategies of the new ACs, to discuss the standards and to get ready for the IDS contribution to ITRF2008.


The IDS Analysis Centers are listed hereafter. Analysis activities are coordinated by F. Lemoine.

Analysis Center Acron. Contact
 Geodetic Observatory of Pecny, Czech Republic  gop  Petr Stepanek
 Institute of Astronomy, Russian Academy of Sciences (INASAN), Russia  ina  Sergey Kuzin
 Surya Tatevian
 CNES/CLS, France  lca  Laurent Soudarin
 Hugues Capdeville
 Jean-Michel Lemoine
 IGN/IPGP, France  ign  Pascal Willis
 Marie-Line Gobinddass
 ESA/ESOC, Germany  esa  Michiel Otten
 Geoscience Australia, Australia
 (with support of GSFC)
 gau  Ramesh Govind
 Frank Lemoine
 GSFC, USA  gsc  Frank Lemoine
 University of Newcastle, UK  ncl  Philip Moore


The IDS combinations of weekly solutions for the station coordinates and the Earth Orientation Parameters are realized with CATREF, the IGN/LAREG Software.

 Coordination Center   Acron.   Contact 
 CLS/CNES  ids (TBC)  Jean-Jacques Valette
 Philippe Yaya
 Pascale Ferrage
 LAREG/IGN (software and strategy support)  -  Zuheir Altamimi

 

Weekly SINEX series contributions

The following table summarizes the AC submissions and associated main models as well as the DORIS SINEX series provided for the contribution to ITRF2008.
See also the DORIS satellites constellation history status.

 AC  Software  Sol. Id.  Type (1)  Data span  Satellites (2)  Earth Gravity
Field
 Constraint  EOPs  Desc.
 gop  BERNESE 5.0  wd31  var-cov  1999.0-2006.9  Spot 2/4/5
 Topex Envisat
 Jason-1 in 2002
 EIGEN-GL04S annual, 100X100  loose  motion, rate  dsc
 more
 ina  GYPSY/OASIS 4.03  wd03  var-cov  1997.0-2008.8  Spot 2/5
 Spot 4 (except 05/98-01/99)
 Topex Envisat
 GGM01C
 fixed, 120x120
 loose  motion
 rate (constrained)
 LOD, UT1
 dsc
 more
 lca  GINS/DYNAMO  wd20  var-cov  1993.0-1998.4
 1999.4-2002.0
 2002.0-2008.0
 Spot 2/3/4/5
 Topex & Envisat
 (Topex/Envisat orbits with SLR)
 EIGEN_GL04S
 drift, annual
 semi-annual
 95x95
 loose  motion  dsc
 readme
 more
 ign  GYPSY/OASIS 5.0  wd08  var-cov  1993.0-2008.8  Spot 2/3/4/5
 Topex Envisat
 GGM03S
 fixed, 120x120
 loose  motion
 rate (constrained)
 LOD, UT1
 dsc
 readme
 more
 gau  GEODYN  wd06  var-cov  2003.0-2008.8  Spot 2/4/5
 Envisat
 Jason-1
 GGM02C
 annual, 160x160
 loose  motion
 UT1
 dsc
 more
 esa  NAPEOS  wd01  NEQ  1998.0-2008.0  Spot 2/4/5
 Envisat
 (Envisat orbits with SLR)
 EIGEN-GL05C  loose  motion, rate
 LOD
 dsc
 more

(1) var-cov: variance-covariance, NEQ: Normal Equation
(2) Specific recommendation for Jason-1 is to exclude Jason-1 data after 2003 because of the USO sensitivity to SAA (cf AWG-June 2008)

 

Compliancy with IERS Call

The delivered SINEX are not yet fully compliant with the IERS call for participation requirements. The non compliant items are the followings:

  • 3 ACs (ina, ign, gau/gsc) provide UT1 in the set of EOPs for each day while the call only expects VLBI to provides UT1,
  • lca AC applies atmospheric correction while it is requested NOT to correct for any geophysical fluid loading effects, except for tidal ocean loading.

Concerning the last issue, LCA will provide a new SINEX series for which the weekly mean value of the atmospheric loading correction is removed.

 

SINEX preprocessing

The preprocessing of the SINEX solutions is realized per AC series and includes the following steps:

  • verification of DORIS station identification (dome #, mnemo)
  • rejection of stations over the whole time period (never used),
  • rejection of stations over specific periods (partially used),
  • verification of solution number and discontinuities (breaks - to be consolidated before weekly combination by analysis of all AC stations times series -),
  • when NEQ provided, inversion of free singular equations,
  • projection using minimal constraints and rejection of perturbating stations,
  • weekly comparison with ITRF2005 at epoch of each solution,
  • analysis and rejection of high residual stations.
gop ina lca ign esa gau gsc ncl
 vs ITRF2005  t7p-I05  t7p-I05  t7p-I05  t7p-I05  t7p-I05  t7p-I05  t7p-I05  
 Internal Coherency  T7p-IC  T7p-IC  T7p-IC  T7p-IC  T7p-IC  T7p-IC    
 Report  sum  sum  sum  sum  sum  sum  sum  sum
 Residuals                

(to be completed)

 

Per week Combination

The weekly combination results from a 7-parameter transformation calculated every week using an IDS ITRF2005 datum . This datum results from a selection of DORIS stations having the best on position (< 1 cm) and velocity (< 2 mm/yr), and included in the week solution to be processed. For each week, the steps are as follows:

  • datum generation with selection of common stations to all ACs SINEX and propagation at epoch of the solutions,
  • first CATREF combination,
  • residual analysis and station rejection (minimum number needed),
  • weighting with variance factor,
  • iteration process and final combined solution with TRF parameters.

Note that at least 3 solutions are needed to generate a weekly combined solution. That is to say that a combination is possible over the 1997.0-2008.8 period.

Combination results (under construction)

 

 

 

IDS recommendations (Pascal Willis, Laurent Soudarin, Herve Fagard, John Ries, Ron Noomen) Version 1.0 November 15, 2005 

This document is supplemented by the following files:

ids_station_breaks.txt [text file]: list of epochs of discontinuities in DORIS stations (in ITRF format)

ids_period_to_delete.txt [text file]: list of DORIS observation periods that should be disregarded (in ITRF format)

ids_core_evolution.mov [movie] evolution in time of the proposed DORIS core network (in one or more movie formats).