Transcript
Page 1: Introduction to Radio Occultations

Slide 12nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Introduction to Radio Introduction to Radio OccultationsOccultations

Georg Bergeton Larsen

GRAS SAF Project ManagerAtmosphere Ionosphere Research Division (AIR)

Danish Meteorological Institute (DMI)Copenhagen

Page 2: Introduction to Radio Occultations

Slide 22nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Outline of presentationOutline of presentation

• The satellite system

• Derivation of atmosphere parameters – Bending angle– Refractivity– Temperature– Humidity

• Distribution of measurements

• Advantages and limitations

• Satellite missions

• Summary

Page 3: Introduction to Radio Occultations

Slide 32nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

The satellite systemThe satellite system

The GPS constellationThe GPS constellation

The occultation measurementThe occultation measurement

Page 4: Introduction to Radio Occultations

Slide 42nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

GRAS Atmosphere profilingGRAS Atmosphere profiling

t1 t2

t3

GPS

Metop

Page 5: Introduction to Radio Occultations

Slide 52nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Neutral Atmosphere Bending AngleNeutral Atmosphere Bending Angle

• The bending angle is computed from the atmospheric phase delay

• Ionosphere correction on bending angle

22

21

22

212

1 )()()(

ff

afafa

Page 6: Introduction to Radio Occultations

Slide 62nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Refractivity profileRefractivity profile

• The refractivity is determined using the Abel transform

• Uncertainty: 0.3 % measurement range: 4 - 450 N-units

))(1

exp()(22

a ax

dxxa

curveRa

ahN

)(,10)1( 6

Page 7: Introduction to Radio Occultations

Slide 72nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Atmosphere ParametersAtmosphere Parameters

• The density of the dry atmosphere is computed by assuming an ideal gas

• where Rd = 0.287 J/(gK) and k1=77.6 K/hPa, k2 = 37,39104 K2/hPa, k3 = 70,40 K/hPa. The pressure profile is now obtained by using hydrostatic equilibrium

• Uncertainty: 0.3 % measurement range: 10-1100 mb

T

Pk

T

Pk

T

PkN wwd

3221

)(1

)(1

zNRk

zd

z

dry dzzgzzP ')'()'()(

Page 8: Introduction to Radio Occultations

Slide 82nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Temperature profileTemperature profile

• The temperature profile is derived by using the ideal gas law and the estimated profiles of refractivity and pressure.

• Uncertainty: 1K measurement range: 180K - 335 K

)(

)()( 1

zN

zPkzT dry

dry

Page 9: Introduction to Radio Occultations

Slide 92nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Water vapor profileWater vapor profile

• The water vapor pressure is derived by an iterative process using T(z) from NWP model (Offline Products) and using the 1DVAR method (NRT Products).

• 1) Total pressure

• 2) Water vapor pressure

• 3) Total density

• Equations 1) to 3) are solved with the dry pressure as initial input in eq. 1) and Rw=0.461 J/(gK).

• Uncertainty: < 20 % Measurement range: 1 - 45 mb • Assumed uncertainty on T(z) less than 1K

z

dzzgzzP ')'()'()(

2

1 )())()()(()(

k

zTzPkzTzNzPw

)(

)(1

)(

)(1)(

zT

zP

R

R

zT

zP

Rz w

w

d

d

Page 10: Introduction to Radio Occultations

Slide 102nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

GRAS SAF Prototype TemperatureGRAS SAF Prototype TemperatureProfile from CHAMP DataProfile from CHAMP Data

Page 11: Introduction to Radio Occultations

Slide 112nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Retrieved Water Vapour ProfileRetrieved Water Vapour Profile

GPS/MET occultation Feb 9, 1997 at UT 16:15 lat: –14 lon: 141

Tdry

TNWP

eocc

esaturated

Page 12: Introduction to Radio Occultations

Slide 122nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Distribution of GRAS measurementsDistribution of GRAS measurements

GRAS occultations during 24 hrs. Approximately 600 atmosphere profiles distributed globally

Distribution of NWP Radio sondes

Page 13: Introduction to Radio Occultations

Slide 132nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Advantages and limitations of GPS Advantages and limitations of GPS Atmosphere ProfilingAtmosphere Profiling

• Absolute measurement♦ The basics of the observations are a measurement of time. Calibration of

clocks can be achieved using assisting ground observations.

• Global coverage♦ The geometry of the observation leads for one satellite to evenly distributed

data on a 24-hour interval. Observations over seas and oceans (covering 70% of the Earth) minimize the major error source concerning accuracy of weather forecast and climate models.

• High vertical resolution♦ The vertical resolution limited by the Fresnel zone of the observation leads to

information of atmosphere phenomena with scale sizes less than 1 km.

• Insensitive to clouds and precipitation♦ The wavelengths applied makes the measurement transparent to clouds and

rain hampering other space techniques.

Page 14: Introduction to Radio Occultations

Slide 142nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

Satellite missions Satellite missions

• Research / demonstration• GPS-Met (1995-97)• Ørsted (1999-)• CHAMP (2000-)• SAC-C (2000-)• GRACE• FedSat

• Operational• METOP/GRAS (2005-) • NPOESS/GPSOS (2010-)

• Constellations of micro-satellites• COSMIC (2006-)• ACE+ (2008-)

Page 15: Introduction to Radio Occultations

Slide 152nd GRAS SAF User Workshop, LO-Skolen, Helsingør, June 11 - 13, 2003

SummarySummary

• Key parameters and method introduced – Bending angle

– Refractivity

– Temperature

– Humidity

• Examples and distribution of RO measurements

• Advantages and limitations– Global coverage (not synoptic)

– High vertical resolution (averaged horizontally)

– Insensitive to clouds

• Satellite missions– GRAS on Metop - first operational RO mission


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