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SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS SCIENCE PRODUCTS 15 th International Laser Ranging Workshop Canberra, Australia October 2006 Mars Topography MGS MGS NEAR ICESat

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Page 1: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

SCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTSSCIENCE PRODUCTS

15th International Laser Ranging

Workshop

Canberra, Australia

October 2006Mars Topography

MGS

MGS

NEAR

ICESat

Page 2: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

........SLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFESLR INVESTIGATION LIFE--------CYCLECYCLECYCLECYCLECYCLECYCLECYCLECYCLE

Tracking Data Analysis

Data QA

Tracking calibration

Instrument engineering

Reference Frame Modeling

Geocenter motion

Polar Motion and Earth Orientation

Orbit Determination

Force Modeling

Global Data Evaluation

Orbit DQ

Instrument/Sensor Analysis

Sensor Data Calibrations

Use of Laboratory DataAtmospheric Modeling

Tropospheric Refraction

Science Products

Geophysical Models

Analysis Methods

Science Interpretation

Satellite Form

Modeling & Frame

S/C Attitude

Page 3: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

PRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATIONPRECISION ORBIT DETERMINATION

Altimeter Mission Support

± 2 cm orbits for TOPEX and

Jason

.

Interplanetary Applications

Precision Orbits for NEAR

2m Orbits for Mars Global Surveyor

assisted with Laser Altimeter

Crossovers

Satellite Laser Ranging

state-of- the-art precision OD

mm tracking site locations

mm/yr tectonic motion determination

monitoring time varying gravity effects

30 Years of

SLR Leadership

Page 4: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Calibrating GNSS orbits with SLR tracking

data (Urschl et al)

SLR observations are very useful for independent validation of microwave orbits.

Page 5: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

PRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVEPRECISION ORBITS for GIOVE--------AAAAAAAA

Manoeuvrers

Consistency Tests to

Optimize Results

Page 6: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Lageos Node Combination Residual

Compared to Predicted LT Effect

(Pavlis)

Lageos Node Combination Residual

Compared to Predicted LT Effect

(Pavlis)

µEIGEN-GRACE02S = 0.992 ± 0.05LLR (Murphy) = ± .001

Lageos II Modeled and Observed Spin

Orientation Needed for Advanced

Thermal Models (Noomen); Lageos

Spin Modeling (Kucharski)

Lageos II Modeled and Observed Spin

Orientation Needed for Advanced

Thermal Models (Noomen); Lageos

Spin Modeling (Kucharski)

Advances in Physical Understanding

11+ years

Page 7: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

CCCCCCCC2,02,02,02,02,02,02,02,0: Comparison: SLR : Comparison: SLR : Comparison: SLR : Comparison: SLR : Comparison: SLR : Comparison: SLR : Comparison: SLR : Comparison: SLR vsvsvsvsvsvsvsvs GRACE GRACE GRACE GRACE GRACE GRACE GRACE GRACE

monthly (monthly (monthly (monthly (monthly (monthly (monthly (monthly (LemoineLemoineLemoineLemoineLemoineLemoineLemoineLemoine))))))))

GeophysicalFluids

SLR

Page 8: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

C2,0: SLR 30 yr Evolution C2,0: SLR 30 yr Evolution

((LemoineLemoine))

Rate of Radial Displacement Predicted Rate of Radial Displacement Predicted from PGR Model Developed from ICEfrom PGR Model Developed from ICE--

5G (Peltier)5G (Peltier)

Post Glacial Rebound

30 years

Page 9: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Terrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference FrameTerrestrial Reference Frame(Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, (Polar Motion, Earth Rotation, GeocenterGeocenterGeocenterGeocenterGeocenterGeocenterGeocenterGeocenter, Station Motion), Station Motion), Station Motion), Station Motion), Station Motion), Station Motion), Station Motion), Station Motion)

SUB-CM EARTH MEASUREMENTS

mm-level Geodesy requires

understanding of the reference

frame and its distortions to acute

levels of precision.

.

Page 10: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Lambeck:• AuScope

Katherine

Page 11: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

International Terrestrial Reference Frame

Page 12: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Geocenter Monitoring Using SLR(Govind)

Page 13: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Optimal Combination of Techniques (Gambis)

Page 14: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Improved Treatment of Time Varying Signals (Coulot)

Page 15: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

SLR vs VLBI Scale: 1.7ppb???

DGFI

IGN

?

Page 16: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

WWW Based Service to Compare Geodetic Time Series (Deleflie)

Page 17: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

LASER SATELLITE ALTIMETRYLASER SATELLITE ALTIMETRY

• Laser Altimetry

– Earth/planetary topography

– Biospheric monitoring

– Interplanetary applications

Sea Surface Topography

TOPEX

Mars Topography

Europa Ice Sheets

EROS

Sea Surface Topography

• Mars Global Surveyor

• Near Earth Asteroid Rendezvous .

• ICESat

• Shuttle Laser Altimeter

• Lunar Reconnaissance Orbiter

• Mercury Messenger

Calipso

Page 18: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from Mars Surface Topography from

MGS/MOLAMGS/MOLAMGS/MOLAMGS/MOLAMGS/MOLAMGS/MOLAMGS/MOLAMGS/MOLA

Page 19: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

First Sea Ice Thickness Maps From First Sea Ice Thickness Maps From ICESatICESat

Sea Ice Thickness

May 15 – Jun 24, 04Sea Ice Thickness

Feb 18 – Mar 21, 04

Sea Ice Thickness

Oct 4 – Nov 18, 03

SummerWinter Fall

Nu

mb

er

Nu

mb

er

Nu

mb

er

Page 20: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

SIMULATIONS FOR LRO

• Simulations of a Lunar Orbiter

mission flying an altimeter were

undertaken in support of GSFC’s

proposal for this round of

Discovery Missions. These

simulations assessed the efficacy

of using altimeter cross over data

to improve satellite positioning

and gravity recovery on the far

side of the moon

Page 21: Summary 1-science products - NASA2m Orbits for Mars Global Surveyor assisted with Laser Altimeter Crossovers ... • Simulations of a Lunar Orbiter mission flying an altimeter were

SummarySummarySummarySummarySummarySummarySummarySummary

• Observations Acquired by SLR, LLR, and Laser Altimetry are Major and Unique Science Resources

• Major Advancements in Modeling

– Gravity field accuracy

– Astrodynamic forces

– Thermal characterization of satellite components

– SLR data analysis techniques and correction algorithms

• Limitations

– Best SLR precision ~ 1-2 mm; Best orbit reductions ~ 1-2 cm

– Significant signal remains to be understood and exploited

– Terrestrial Reference Frame:

• Results are currently analysis center specific and rely on processing approaches

• Significant and pressing need for resolution