SAOCOM 1A Interferometric Error Model and...
Transcript of SAOCOM 1A Interferometric Error Model and...
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SAOCOM 1A Interferometric Error Model and Analysis
Pablo A. Euillades, Leonardo D. Euillades, Mario Azcueta and Gustavo Sosa
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Presentation Overview Objective Present SAOCOM system interferometric error model and
analysis for DInSAR applications. Structure
1. SAOCOM system brief description 2. General considerations for the analysis 3. DInSAR accuracy results 4. Conclusions
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SAOCOM Mission Overview
• Constellation of two satellites, SAOCOM 1A and 1B
• Space Agency: CONAE (Argentina) • Polarimetric L-Band SAR (1.275
GHz) • Sun synchronous nearly circular
frozen polar orbit (620 km) • 16 day repeat cycle (one satellite) • 8 day repeat cycle (two satellites) • Mission lifetime: 5 years • Launch Date:
• SAOCOM 1A: 11/2016 • SAOCOM 1B: 2017
http://www.conae.gov.ar/index.php/english/satellite-missions/saocom/introduction
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SAOCOM Mission Overview
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Error Model
p q
r
B
pq sep inc angle
model parameters
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Error Model Residual Orbital Variance
Residual Topographic Variance
Decorrelation Variance
(Pepe A., 2006)
(Pepe A., 2006)
(Bamler & Hartl., 1998)
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Implementation Python programmed Application
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Analysis Considerations
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Results: Base Scenario LO
S Di
spla
cem
ent E
rror
[cm
]
Extension [m]
Nea
r Ran
ge
Far R
ange
Bperp=0, γtemp=0.99
Bperp=0, γtemp=0.6
Bperp=2km, γtemp=0.99
Bperp=2km, γtemp=0.6
Phase Aliasing Limit
Sout
h Be
lridg
e
Cruz
de
Pied
ra M
arac
aibo
Nab
esna
Gla
cier
Tasm
an G
laci
er
Ups
ala
Glac
ier
Mor
eno
Glac
ier
Lascar
Kilauea
Chaiten
Las V
egas
Huds
on
Yello
wst
one
Segu
am
Fogo
*volcanic deformation examples taken from http://www.geo.cornell.edu/eas/PeoplePlaces/Faculty/matt/volcano_table.html
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Analysis Considerations
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LOS
Disp
lace
men
t Err
or [c
m]
Extension [m] Fa
r Ran
ge
Bperp=0, γtemp=0.99
Bperp=0, γtemp=0.6
Bperp=2km, γtemp=0.99
Bperp=2km, γtemp=0.6
Phase Aliasing Limit
Results: Realistic Scenario
Nea
r Ran
ge
Sout
h Be
lridg
e
Cruz
de
Pied
ra M
arac
aibo
Nab
esna
Gla
cier
Tasm
an G
laci
er
Ups
ala
Glac
ier
Mor
eno
Glac
ier
Lascar
Kilauea
Chaiten
Las V
egas
Huds
on
Yello
wst
one
Segu
am
Fogo
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Results for Stripmap Modes LO
S de
form
atio
n er
ror [
cm]
Acquisition Mode (beam)
10km Realistic Scenario 10km range, 11 deg slope, Bperp=2km, 3400m height change, γtemp=0.6, atmospheric signal
10k Base Scenario 10km range, 0 deg slope, Bperp=0, flat relief, γtemp=0.99, no atmospheric signal
10km Intermediate 10km range, 2 deg slope, Bperp=1km, 300m height change, γtemp=0.75, atmospheric signal
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Stacking After Emardson et al (2003) Atmospheric Delay in InSAR Applications
Minimum detectable deformation rate
Tobs=16 days (1 satellite) Torb=5 years σ btw 1.8 – 16.6 mm
vmin = 0.9 - 8 mm/year/100km
Beam S7 Dual Polarization:
Tobs=8 days (2 satellites) Torb=5 years σ btw 1.8 – 16.6 mm
vmin = 0.6 – 5.7 mm/year/100km
Tobs=8 days (2 satellites) Torb=7 years σ btw 1.8 – 16.6 mm
vmin = 0.34 – 3.4 mm/year/100km
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Conclusions
• SAOCOM SAR Interferometric capabilities have been studied by considering relevant error terms.
• Expected error is systematically lower in Dual Polarization Modes than in Quad Polarization ones.
• Expected error of modes S5DP to S9DP are between ~0.6cm and ~1.4cm depending on the atmospheric influence considering a reasonable scenario (already described)
• After a 5 years mission, deformation gradients compatible with inter-seismic tectonic deformation could be characterized through time-series processing.
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That’s all...
Thank you for your attention!!!
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Number of pixels between p and q
The displacement between p and q can be expressed:
limit: