Transcript
Page 1: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Improved Method for Measuring the Improved Method for Measuring the Satellite-to-Satellite TEC in the IonosphereSatellite-to-Satellite TEC in the Ionosphere

byby

S. SyndergaardS. SyndergaardH.-H. Benzon H.-H. Benzon G. B. LarsenG. B. Larsen

M. B. Sørensen M. B. Sørensen P. Høeg P. Høeg

Atmosphere Ionosphere Remote Sensing DivisionAtmosphere Ionosphere Remote Sensing DivisionDanish Meteorological InstituteDanish Meteorological Institute

Page 2: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Setting the scene: Ionosphere occultation principleSetting the scene: Ionosphere occultation principle

Page 3: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Ionosphere tomography combining ground Ionosphere tomography combining ground and space measurementsand space measurements

Convenient toassume straight lines

Page 4: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

GPS observables and traditional TEC measureGPS observables and traditional TEC measure

Disregarding troposphere, clocks & ambiguity bias:

1

21

1 )1( dsNfCL e

2

22

2 )1( dsNfCL e

2112 LLTEC

• On occultation links the traditional measure is not exactly the straight line TEC

• Discrepancy becomes appreciable for large electron density gradients

Page 5: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Occultation geometryOccultation geometry

Page 6: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

S-S TEC with first order dispersion correctionS-S TEC with first order dispersion correction

2

22

121

12011

ffCTECTEC

w h e r e

da

dsNda

daTECd

sss eGL

22

0

)(

• Mainly proportional to the square of vertical TEC gradients• Accuracy depends on validity of spherical symmetry assumption

(“major” term) (“minor” term)

Page 7: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Simulated TEC residuals, double Chapman layersSimulated TEC residuals, double Chapman layers

E-layer:Max. dens.: 2·1011 m-3

Scale height: 5 km

F-layer:Max. dens.: 3·1012 m-3

Scale height: 60 km

Page 8: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

GPS/MET ionosphere profile, occ. 641, Feb 20 1997GPS/MET ionosphere profile, occ. 641, Feb 20 1997

Local time: 12:30Latitude: 36 NLongitude: 144 ESolar flux: 73

Page 9: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

GPS/MET TEC profile, occ. 641, Feb 20 1997GPS/MET TEC profile, occ. 641, Feb 20 1997

Local time: 12:30Latitude: 36 NLongitude: 144 ESolar flux: 73

Page 10: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

GPS/MET estimated TEC residuals, occ. 641, Feb 20 1997GPS/MET estimated TEC residuals, occ. 641, Feb 20 1997

Page 11: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Ørsted ionosphere profile, April 18 1999Ørsted ionosphere profile, April 18 1999

Local time: 14:45Latitude: 33 SLongitude: 13 WSolar flux: 113

Page 12: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Ørsted TEC profile, April 18 1999Ørsted TEC profile, April 18 1999

Local time: 14:45Latitude: 33 SLongitude: 13 WSolar flux: 113

Page 13: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Ørsted estimated TEC residuals, April 18 1999Ørsted estimated TEC residuals, April 18 1999

Page 14: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Alternative estimate of straight line S-S TECAlternative estimate of straight line S-S TEC

)()(

)( 0122

21

0221

22

22

21

22

21

0 sLffsL

ff

ffCffTEC

2122

21

22

21

12 )(LL

ffCffTEC

• Corrects for first order dispersion effects• Not sensitive to spherical asymmetry• Drawback: clocks and POD needs to be solved (removed)

traditional combinationfor comparison( )

Page 15: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

Simulated TEC residuals, spherical asymmetry conditionsSimulated TEC residuals, spherical asymmetry conditions

Page 16: Improved Method for Measuring the  Satellite-to-Satellite TEC in the Ionosphere by S. Syndergaard

URSI XXVI General Assembly, Toronto, Canada, 13-21 August 1999

SummarySummary

• Satellite-to-satellite TEC L1 - L2 may give TEC errors of order 10 TECU

• Not a big problem at low solar activity or night time (error < 1 TECU)

• May be a problem at day time, solar maximum

• Dispersion correction reduce errors depending on spherical symmetry assumption

• Alternative dual frequency combination can be applied, but then one needs to solve for clocks and POD

• Results can be used in ionosphere tomography to obtain more accurate straight-line satellite-to-satellite TEC


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