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    Jan Kouba

    Geodetic Survey Div.

    NRCan

    Canada

    IGS Products and Applications

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    Content

    IGS Combined Products

    Objectives

    Description

    Precision/availability

    Consistency

    Use of IGS Products

    Relative Positioning

    Precise Point Positioning/Navigation

    Compatibility

    Scientific Applications

    IGS Products Limitations and Solutions

    Future Developments

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    IGS PRODUCTS

    Support practical positioning and scientific applications of GPS, such as

    surveying, navigation and national geodetic control networks

    monitoring of Earth rotation, deformation and atmosphere (trop. & ion.)

    easy access and contributions to ITRF, time transfers, etc.

    Provides convenient and precise IGS reference system through

    the core IGS combined products: orbits, Earth rotation parameters (ERP), station

    positions/velocities and satellite/station clocks

    additional combined products, consistent with the core products: tropospheric

    zenith path delays (ZPD), ionospheric TEC (total electron count) maps and

    associated rec./satellite diff. calibration biases (DCB)

    IGS combined orbits (since 1994) ; clocks and ERP (since 1995); station

    positions (since 1996) and tropospheric ZPD (since 1997)

    IGS Products are more precise and reliable than the individual AC solutions

    (up to 8 Analysis Center solutions combined)

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    IGS Product Description

    Core Combined Products: orbits/clocks/ ERP/station positions

    IGS Final orbit, clock and ERP combined solutions (12 day delay)

    IGS Rapid orbit, clock and ERP combined solutions (17 hour delay)

    IGS Predicted orbit and clock combined solutions (1 hour before the observation day) Nine Associate ACs (AACs) produce regional station position solutions in SINEX format

    Up to eight ACs, AACs contribute global orbit, ERP, global station position (SINEX)

    solutions and up to five ACs clock solutions

    Combined Zenith Path Delay (ZPD)

    seven ACs, produced by GFZ, since Jan. 1997

    Weekly files by site, 2 hour resolution (four weeks delays)

    Combined Global Ionosphere Maps of Total Electron Content (TEC)

    Five ACs, AACs, Combined TEC and DCBs (Differential Code Biases) in IONEX format,

    produced by ESA since June 1998

    Daily files, 2 hour resolution (four weeks delay)

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    Analysis Center Functions

    IGS Analysis Centers (AC): are the basis of all IGS products, improved IGSproducts are largely due to AC improvements

    Typically performs continuously (daily): three types of global solutions(Predicted, Rapid and Final) utilizing complex and sophisticated software, often

    developed in house over many years

    Conforming to IGS/IERS standards, but innovations are encouraged.

    Documentation on an each AC

    ) approach is at the IGS CB Archives:

    http://igscb.jpl.nasa.gov/igscb/center/analysis/

    ccc

    .acn

    Continuously involved in research & developments: striving for the bestsolutions and sharing scientific results amongst AC colleagues

    Helpful and healthy competitions amongst all ACs

    Associate Analysis Centers (AACs):

    typically do not perform all global solutions, e.g. the Rapid only, or only certainspecific solution products, such as:

    RNAAC (Regional Network AAC), GNAAC (Global Network AAC), IAAC(Ionospheric AAC) etc.

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    IGS PRODUCT Table

    IGS Combined Product Precision

    Product Available Interval Precision

    Satellite Orbits&clocks orbits clocks

    Predicted Real-time 15 min 50 cm 30 ns

    Rapid 17 hours 15 min 10 cm .5 ns

    Final 12 days 15 min 5 cm .3 ns

    IGS Combined (Prelim.) Station Positions Velocities

    Weekly solutions 2-4 weeks 7 days 3-5 mm 1-3mm/y

    Earth Rotation Parameters parameters rates/LODRapid PM 17 hours 1 day .2 mas. .4 mas/d

    Final PM 12 days 1 day .1 mas .2 mas/d

    Rapid UT /LOD 17 hours 1 day .10 ms .06 ms/d

    Final UT /LOD 10 days 1 day .05 ms .03 ms/d

    Tropospheric ZPD

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    IGS Orbit Improvement

    1994 to Mid 1999

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    IGS PRODUCTS (AC performance)

    BROADCAST (BRD), IGS PREDICTED (IGP) and IGS UTRA_RAPID

    (IGU) ORBIT RMS WITH RESPECT TO THE IGS RAPID (IGR)

    ORBITS

    0

    1

    2

    3

    4

    5

    6

    7

    16-Nov-99 16-Dec -99 15-Jan-00 14-Feb-00 15-Mar-00 14-Apr-00 14-May-00

    DATE

    WEIGHTEDRMS(m)

    brd

    igp

    igu

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    IGS Orbit Comparison

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    Earth Rotation Parameters

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    Consistency of IGS Products

    Consistent with the current international conventions

    International Earth Rotation Service (IERS) Conventions 1996

    International Terrestrial Frame (ITRF)(currently ITRF97)

    IGS CORE products (orbits/clock/ERP/stations) are mutually consistent

    Since December 1998, combination of minimally constrained AC solutions

    Nearly exact ITRF transformations (e.g. for the ITRF97-ITRF96 and the future

    changes)

    ITRF realizations used for IGS Products (for more details see the presentationon: IGS ITRF Realization and Transformations) :

    ITRF92 - Jan 2, 1994(Wk 0730) to Dec 31, 1994 (Wk 0781) ITRF93 - Jan 1, 1995(Wk 0782) to Jun 29, 1996 (Wk 0859)

    ITRF94 - Jun 30, 1996(Wk 0860) to Feb 28, 1998 (Wk 0946)

    ITRF96 - Mar 1, 1998(Wk 0947) to July 31, 1999 (Wk1020)

    ITRF97 - Aug 1, 1999(Wk 1021) to present (since Feb 27, 2000 IGSITRF97 (SINEX))

    IGS satellite clock solutions are aligned to the GPS time via broadcast clockcorrections:

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    USE of IGS PRODUCTS

    IGS Products greatly enhance and simplify (no need for complex global

    GPS solutions) all GPS analyses and applications such as:

    Positioning/navigation

    Global, Regional and Local

    Relative positioning with respect to the IGS station Polyhedron of about 200 stations atthe mm/ppb level (IGS orbits/ERP and station positions can be fixed even for

    baselines 2000 km and longer). No need for precise satellite clocks (nearly

    eliminated)

    Absolute, precise point positioning ppp) worldwide, with respect to the IGSReference Frame IGS orbit/clocks/ERP held fixed) at mm precision level

    Absolute, precise point navigation worldwide (ground, air, LEO satellites - no basestations needed ), at a cm precision level

    Global Change Monitoring: solid Earth, atmosphere and oceans

    ERP monitoring

    plate motion and crustal deformation monitoring, volcanoes, etc.

    monitoring of atmosphere (troposphere and ionosphere)

    Precise time and freq. transfers (future contributions to UTC)

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    Relative Positioning

    Relative position precision at ppb/mm

    IGS Orbits, ERP, base station position solutions can be held fixed at the IGS

    solutions for all, even extreme, baseline lengths at ppb/mm precision level (in

    ITRF insensitive to ERP)

    When using double differencing, potentially more robust (than precise point

    positioning), the IGS products ease data cleaning, ambiguity fixing

    Complete covariance/correlation matrix available (e.g. for in SINEX format)

    Suitable for continental, regional, national ITRF densification (e.g. EUREF -

    normal equation matrix stacking of RNAAC SINEX solutions)

    Warning: fixing IGS orbits/ERP implies very precise reference orientation and scale

    even for (SINEX) unconstrained solutions (I.e. no stations fixed)

    For long baselines (~ 1000km) ITRF orientation/scale changes need to be taken into

    account prior normal matrix stacking

    Insensitive to incompatibilities and clock errors

    Insensitive to clock errors and all small (cm) ITRF changes for baselines

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    Relative Positioning

    Relative Positioning Rrequirements for cm Precision ( double differenced phase data with, or without phase

    ambiguity fixing ; ~ 1 h occupancy)

    IGS Products/ Baseline < 10 km 10 100 km 100 1000 km >1000 km

    IGS Orbits No (Broadcast) IGS Rapid IGS Rapid/Final IGS Final

    IGS ERP**** No No No NoIGS Sat Clocks No No No IGS Rapid/Final

    IGS Iono Delays IGS iono* IGS iono* No** No**

    IGS Tropo Delays Nominal/IGS tropo IGS tropo/ estimate Estimate Estimate

    IGS ITRF Trasform No No No Yes

    ERROR MODELS

    IGS Ant phase center No Yes*** Yes*** Yes

    Solid Earth tides No No Yes Yes

    Ocean loading No No Yes YesRelativity correction No No Yes Yes

    Sat phase wind up No No No Yes

    Single frequency data; ** Two frequency data; *** For different antenna types only;

    **** IGS ERP implied by IGS Orbits

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    Precise Point Positioning

    IGS combined Orbits, clocks held fixed in single point solutions

    Equivalent to back substitution into complex, global (IGS) solutions

    An efficient, flexible and convenient interface/access to the IGS reference frame

    mm precision level for static point positioning worldwide, no base (IGSPolyhedron) station positions/data required

    cm precision level for (epoch by epoch, ground, air, LEO sarellite) navigation, no

    base (DGPS) station positions/data required.

    Efficient and precise solutions for station clocks and tropospheric ZPDs

    Disadvantages (wrt to double differencing/relative positioning)

    More difficult to clean/edit data and/or to fix integer phase ambiguities

    Sensitive to clock errors and to incompatibilities (see below) and even small

    reference (ITRF) changes; orbits/clocks/ERP must be consistent

    Correlation/variance matrix (amongst stations) lost and not available, thus not

    well suited for national/continental ITRF (SINEX) densification

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    Precise Point Positioning

    Static Point Positioning Requirements (undifferenced phase/pseudorange data; < 1 h occupancy)

    IGS Products/precision < 1 cm 1 10 cm 10 100 cm >100 cm

    IGS Orbits IGS Final IGS Rapid/Final IGS Rapid/UltraR No (Broadcast)

    IGS ERP*** No No No No

    IGS Sat Clocks IGS Final IGS Rapid/Final IGS Rapid/UltraR No (Broadcast)

    IGS Iono Delays No** No** IGS iono* IGS iono*

    IGS Tropo Delays Estimate Estimate/IGS tropo IGS tropo/estimate Standard/nominalIGS ITRF Trasform Yes No No No

    ERROR MODELS

    IGS Ant phase centre Yes Yes No No

    Solid Earth tides Yes Yes Yes No

    Ocean loading Yes Yes No No

    Relativity corrections Yes Yes Yes Yes

    Sat phase wind up Yes Yes No No

    * Single frequency data; ** Two frequency data; *** IGS ERP implied by IGS Orbits

    Note:in near future,the Ultra Rapid IGS orbits (Ultra R )

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    Precise Point Positioning (PPP)

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    Precise Navigation

    Navigation/Kinematic Point Positioning Requirements (undifferenced phase and pseudorange data;

    instantaneous occupancy)

    IGS Products/ precision < 10 cm 1050 cm 50500 cm >500 cm

    IGS Orbits IGS Final IGS Rapid/Final IGS Rapid/Final No (Broadcast)

    IGS ERP *** No No No No

    IGS Sat Clocks IGS Final IGS Rapid/Final IGS Rapid/Final No (Broadcast)

    IGS Iono Delays No** No** IGS iono* IGS iono*

    IGS Tropo Delays Estimate Estimate/IGS tropo IGS tropo/estimate Standard/nominal

    IGS ITRF Trasform Yes No No No

    ERROR MODELS

    IGS Ant phase centre Yes No No NoSolid Earth tides Yes Yes No No

    Ocean loading Yes No No No

    Relativity corrections Yes Yes Yes No

    Sat phase wind up Yes No No No

    * Single frequency data; ** Two frequency data *** IGS ERP implied by IGS Orbits

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    Compatibility

    IGS CORE products (orbits/clock/ERP/stations)

    Mutually compatible and consistent since Dec 1998

    Consistency of orbits and clocks is of utmost importance for precise point positioning

    IGS station (SINEX) solutions are compatible/consistent with IGS antenna offsets (station logfiles) and the antenna calibration (phase center) tables (IGS_01.pcv) at IGSCB Archives

    IGS satellite clock solutions are based on/compatible with the following

    assumptions/conventions:

    Periodical special relativistic correction : - 2 . X .V/c2 applied

    Cross correlation type of pseudoranges : C/A; P2= C/A + P2-P1)

    : P1, P2 (After April 2, 2000, Wk 1056)

    Adopted satellite antenna offsets (X,Y,Z m)

    Block II/IIA : 0.279 0.000 1.023 (in the satellite fixed frame)

    Block IIR : 0.000 0.000 0.000

    no L1-L2 satellite/receiver calibration delayed applied

    Ionospheric TEC grid maps, satellite/receiver calibration biases must be of the same solutions

    and

    corresponding mapping function and DCBs must be used for all ionospheric applications to derive

    slant ionospheric delays)

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    Compatibility

    Solid Earth tides have once and twice daily periods; can reach up to 300 mm in height and

    up to 50 mm in latitude and longitude.

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    Compatibility

    Ocean Loading Effects have once and twice daily periods; can reach up to 50 mm in height

    and up to 10 mm in latitude and longitude.

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    Scientific Applications

    Earth Orientation Parameter (EOP) monitoring

    IGS Polar Motion rates of unprecendeted precision (0.1 mas/day) and resolution

    (1 day, or even 2 hours for CODE AC solutions )

    Continuously available with delays of less than 24h (IGS Rapid)

    Independent short period (

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    Scientific Applications

    Correlation between Polar Motion Rates (Xrt, Yrt (not shown)) and OAM+AAM is nearly always better

    than 0.8 (except for the low signal period at or below 0.25 mas/d)

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    Water Vapor Estimates Comparison

    at Station Potsdam

    Partial Water Vapor (PWV) from GPS at IGS station POTS (Germany) agrees with

    Water Vapor Radiometer (WVR), well within one mm (Courtesy of GFZ).

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    Limitations and Solutions

    IGS Combined Orbits :

    In 24 h files with 15 min sampling (0-23:45 GPS time); can be easilyconcatenated to span daily boundaries; easily be fitted with low order

    polynomials for continuous representation

    Small daily discontinuities (at the dm level)

    Possible orbit origin offsets (biases at the cm level)

    Improvements at the AC level, I.e. smaller daily AC orbit discontinuities

    (

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    Recent Changes and Improvements

    IGS Preliminary SINEX Combined Products became official

    From Feb 20/00 (GPS Week 1050), aligned to ITRF97 ( using min. constraints)

    SeeIGS Mail 2740

    for more details

    New IGS ITRF97 realization (through the IGS SINEX combined solution

    IGS00P04.snx

    product)

    From Feb 27/00 (GPS Week 1051); delay increased from 10 to 12 days

    Improved ITRF97 realization for the IGS Final orbits/ERP/clocks

    No noticeable changes to the IGS users (no transformation, no steps )

    SeeIGS Mail 2750

    and

    2751

    for more details

    New Pseudorange bias convention

    starts on Apr 02/00(wk 1056)

    P1, P2replace the current convention: C/A, P2= C/A + (P2-P1)

    Important forIGS clock users (precise point positioning, time transfers)

    SeeIGS Mail 2744

    for more details and the adopted C/A-P1 biases

    IGS Ultra-Rapid Comb. Orbits/clocks

    testing started Mar 2/00

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    Future Developments

    Improved IGS ITRF realization (see the next presentation)

    Weekly, Preliminary SINEX combinations, official since Feb 20, 2000

    Up to 250 IGS Polyhedron stations IGS Combined SINEX solutions

    Continuous plate motion monitoring/quality check (under way)

    Ultra Rapid products Pilot Project (

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    QUESTIONS?

    Jan Kouba

    Geodetic Survey Division

    Natural Resources Canada (NRCan)

    615 Booth Street

    Ottawa, Canada K1A OE9

    [email protected]

    Tim Springer (The IGS AC Coordinator)

    Astronomical Institute, Univ. Bern

    [email protected]

    For details on IGS Products, see the IGS Annual Reports

    http://igscb.jpl.nasa.gov/overview/pub.html