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Satellite Altimetry OCTAS lecture January 2005,

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Least Squares Collocation. Global Marine Altimetric Gravity Field ... This will be treated in the subsequent Least Squares Collocation interpolation procedure. ... – PowerPoint PPT presentation

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Title: Satellite Altimetry OCTAS lecture January 2005,


1
Satellite AltimetryOCTAS lecture January 2005,
  • Ole B. Andersen.

2
Content
  • The radar altimetric observations (1)
  • Altimetry data
  • Contributors to sea level
  • Crossover adjustment
  • From altimetry to Gravity and Geoid (2)
  • Geodetic theory
  • FFT for global gravity fields
  • Least Squares Collocation
  • Global Marine Altimetric Gravity Field (3)
  • Accuracy assesment
  • Applications

3
Content 2
  • Radar altimetry Frontiers (4)
  • Altimetric gravity field in shallow water
  • Altimetric gravity field in polar regions
  • Merging altimetry with airborne data.
  • Mean sea surface and ocean variability
  • Time variation (5)
  • Long Term Sea Level Change.
  • El Nino Monitoring
  • Ocean Tides.
  • Real Time altimetry
  • Laser Altimetry (6).
  • Difference with radar altimetry
  • Gravity from ICESAT
  • High resolution Ice-rif monitoring

4
Altimetric Observations 2
Accurate ranging to the sea surface is based On
accurate time-determination. P. Berry will give
much more on this.
Typical ocean waveforms Registred at 20 Hz The
20 Hz height values are Too noisy and averaged to
give 1 Hz values (7 km averaging).
5
Sampling the Sea Surface (Quick Time Movie).
6
OngoingSatellitemissions
7
Sampling the sea surface.
1 Day
3 Days
8
Orbit Parameters
The coverage of the sea surface depends on the
orbit parameters (inclination of the orbit plane
and repeat period).
TOPEX/JASON - 10 Days
9
5 ongoing missions JASON-1 TOPEX
TDM GFO ERS-2 ENVISAT. One/two track every
day. Real time altimetry (JASON) 4-6 hours
5-7 cm accuracy.
10
GEOSAT / GFO ERS1 / ERS2 / ENVISAT
ERM
GM
ERS GM mission 1994 GEOSAT GM mission 1985
GEOSATERS GM data is ESSENTIAL for high
resolution Gravity Field mapping.
11
The orbital height of the space craft minus the
altimeter radar ranging to the sea
surface corrected for path delays and
environmental corrections Yields the sea
surface height
where N is the geoid height above the
reference ellipsoid, ? is the ocean
topography, e is the error The Sea surface
height mimicks the geoid. MSS N MDT e
-gt GOCINA OCTAS
12
Altimetric observations
The magnitudes of the contributors ranges up
to The geoid NREF /- 100 meters
Terrain effect NDTM /- 30
centimeters Residual geoid ?N /- 2
meters Mean dynamic topography ?MDT /-
1.5 meter Time varying Dyn topography ?(t)
/- 5 meters. (Tides storms El Nino)
What We want for Global Gravity is So we need
to account for the rest.
13
Remove - Restore.
  • Remove-restore technique enhancing signal to
    noise.
  • Remove a global spherical harmonic geoid model
    (EGM96)
  • Remove terrain effect
  • Remove Mean dynamic topography from model.
  • Restore the EGM96 global gravity field
  • Restore the Terrain effect
  • PROBLEM
  • What about time varying signals
  • What about Errors.

14
Time Varying Signal Errors.
Tides contribute nearly 80 to sea level
variability. removed using Ocean tide Model
(AG95, GOT, FES2002, NAO99) Time variable signals
are averaged out in ERM data but not in GM data.
  • eorbit is the radial orbit error
  • etides is the errors due to remaining tidal
    errors
  • erange is the error on the range corrections.
  • eretrak is the errors due to retracking
  • enoise is the measurement noise.

15
Errorstime varying signals.
  • ERM data. Most timeerror average out.
  • Geodetic mission data ?(t) is not reduced
  • Must limit errors to avoid orange skin effect
  • NOTICE ERRORS ARE LONG WAVELENGTH

16
Enhancing the altimetry for gravity
  • Two approaches to limit long wavelength (time
    error signal).
  • Use sea surface slopes
  • Using crossover adjustment.
  • Motivation for crossover
  • The residual geoid signal is stationary at each
    location.
  • Consequently the residual geoid observations /sea
    surface height observations
  • should be the same on ascending and descending
    tracks at crossing locations.
  • Timevarying Dynamic sea level orbital related
    signals should not be the same, and should be
  • Motivation for sea surface slopes
  • Theoretically straight forward wrt gravity field
    computation.
  • Using sea surface slopes reduces long wavelength
    errors
  • THERE IS LITTLE (IF NO) NEED FOR XOVER
    ADJUSTMENT.
  • Short wavelength part of dynamic topography is
    enhanced
  • At extreme latitudes only east-west slopes are
    represented
  • At Equator mainly north-south slope are
    represented.



17
Crossover Adjustment
  • dkhi-hj.
  • dAxv
  • where x is vector containing the unknown
    parameters for the
  • track-related errors.
  • v is residuals that we wish to minimize
  • Least Squares Solution to this is
  • Constraint is needed cTx0
  • Case of bias mean bias is zero

18
Crossover adjustment 2.
  • Modelling track related errors.
  • Bias (short tracks) Rank 1
  • Bias Tilt (medium tracks) Rank 4
  • Higher order (long tracks) Rank 6
  • Rank deficiencĂ˝ can be solved by fixing arcs
    (arbitrerely).
  • Better to apply minimum variance of free surface
    constraint. (free cross over adjustment)

19
Before
20
After Crossover
21
Data are now ready for computing gravity /
geoid.
  • Corrected the range for as many known signals as
    possible.
  • Removed Long wavelength Geoid part will be
    restored.
  • Limited errors time varying signal (Long
    wavelength).
  • Still small long wavelength errors can be seen in
    sea surface heights. This will be treated in the
    subsequent Least Squares Collocation
    interpolation procedure.
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