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Gravity Field Recovery from satellite-to-satellite tracking missions

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Gravity Field Recovery from

satellite-to-satellite tracking missions

M. Weigelt 1 , M.G. Sideris 1 , N. Sneeuw 2

1 Geomatics Engineering, University of Calgary

2 Geodätisches Institut, Universität Stuttgart

mlbweige@ucalgary.ca

Astro 2006 13th Canadian Astronautics Conference and 53rd Annual General Meeting

27 th April, 2006

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Applications

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Gravity from Space: why?

terrestrial gravimetry: inhomogeneous

satellite altimetry:

ocean topography:

5 decades of satellite observations

S

lm

< SH order > C

lm

SH deg ree

EGM96s significant digits

-60 -40 -20 0 20 40 60

0

20

40

60

0 1 2 3 4

(4)

principle: hi-lo SST

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Satellite system: CHAMP

principle of high-low SST measurement

mission duration: 7+ years

orbit height: ~ 400 km inclination: ~ 87°

Key instruments:

• GPS receiver

• Accelerometer CHAMP = CHAllenging Minisatellite Payload

source: GFZ-Potsdam

source: GFZ-Potsdam

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principle: lo-lo SST

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Satellite system: GRACE

Initial orbit height: ~ 485 km Inclination: ~ 89°

Key technologies:

• GPS receiver

• Accelerometer

• K-Band Ranging System mission duration: 5+ years 14 monthly solutions of the gravity field available

 time variable gravity field

GRACE = Gravity Recovery and Climate Experiment

source: GFZ-Potsdam

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principle: SGG

SGG

Earth

mass anomaly

GPS - satellites

SST - hl

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Satellite system: GOCE

planned: 2007

Initial orbit height: ~ 270 km Inclination: ~ 96.5°

GOCE = Gravity Field and steady-state Ocean Circulation Explorer

source: GOCE-Projektbuero

Key technologies:

GPS

• Gradiometer

• Ion thruster system

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spatial resolution

50

/ 2 400 km

= 1 month L

T

100

/ 2 200 km

= 1 month L

T

300 / 2 70 km

= N/A L

T

Resolution

(11)

Accuracy

source: GOCE-Projektbuero

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Open issues

Aliasing:

Monitoring  formation flying

January 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

June 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

January 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

June 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

-11 -10.5 -10 -9.5 -9 -8.5 -8 -7.5 -7

Time-variable gravity:

Tapley et al.

23 Juli 2004

Science 305:503-505 January 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

June 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

January 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

June 2003

Snm - | - Cnm

-60 -40 -20 0 20 40 60

0 10 20 30 40 50 60

-11 -10.5 -10 -9.5 -9 -8.5 -8 -7.5 -7

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Gravity Field Recovery from

satellite-to-satellite tracking missions

M. Weigelt 1 , M.G. Sideris 1 , N. Sneeuw 2

1 Geomatics Engineering, University of Calgary

2 Geodätisches Institut,Universität Stuttgart

mlbweige@ucalgary.ca

Astro 2006 13th Canadian Astronautics Conference and 53rd Annual General Meeting

27 th April, 2006

Questions?

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