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How does InSAR work? Gareth Funning University of California, Riverside

Presentation on the background theory of InSAR

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Page 1: Presentation on the background theory of InSAR

How does InSAR work?

Gareth FunningUniversity of California, Riverside

Page 2: Presentation on the background theory of InSAR

Outline

• Basics of SAR and InSAR• Application to earthquakes, and other examples• Limitations• The future

Page 3: Presentation on the background theory of InSAR

InSAR

InterferometricSyntheticApertureRadar

pretend you have a big radar antenna

use wave interference

emit microwaves, measure echoes

Page 4: Presentation on the background theory of InSAR

SAR: how it works

1. Satellite emits radar pulse2. Radar is backscattered3. Amplitude and phase of echo

recorded at the satellite

Page 5: Presentation on the background theory of InSAR

flight direction

ground sw

ath5 km

Page 6: Presentation on the background theory of InSAR

flight direction

ground sw

ath

Page 7: Presentation on the background theory of InSAR

flight direction

ground sw

ath

synthetic aperture(5 km instead of 10 m!)

resolution 20 m instead of 5 km!

Page 8: Presentation on the background theory of InSAR

• SAR imaging uses amplitude (intensity) of backscattered echoes

• Radar sees through clouds—all-weather imaging is possible

• Don’t need illumination by the Sun—can image day and night

• Surface roughness and slopes control the strength of the backscatter

• Applications: ship tracks, ice tracking, oil slicks, land-use changes, planetary

JPL

Page 9: Presentation on the background theory of InSAR

Kilauea caldera, Hawaii

JPL

Slopes facing toward satellite have bright backscatter

Slopes facing away from satellite show dark backscatter and/or shadowing

Flig

ht d

irecti

on

Look direction

Page 10: Presentation on the background theory of InSAR

Kilauea caldera, Hawaii

JPL

Areas of vegetation are “rough” and have bright backscatter

Sedimentary drainages are comparatively smooth and have less backscatter

Page 11: Presentation on the background theory of InSAR

What about the phase?

~780 km

~6 cm

Phase is a function of the distance from the satellite to the ground.

ERS-1

Page 12: Presentation on the background theory of InSAR

Pass 1 Pass 2

InSAR: How it works

Page 13: Presentation on the background theory of InSAR

Pass 1: pre-movement Pass 2: post-movement

phase shift due to ground motion

phase=1 phase=2

InSAR: How it works

Page 14: Presentation on the background theory of InSAR

phase shift varies with distance from the fault

InSAR: How it works

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Image A - 12 August 1999

Image B - 16 September 1999

Interferogram = Phase A - Phase B

Remove phase from topography

satellite positionsearth curvature

Tim Wright

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(0) 0 mm range change

(-1) 28 mm range decrease

(-2) 57 mm range decrease

(-10) 283 mm range decrease

(-20) 567 mm range decrease

17 August 1999, Izmit earthquake (Turkey)Tim Wright

Page 17: Presentation on the background theory of InSAR

A’

A

17 August 1999, Izmit earthquake (Turkey)Tim Wright

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10 km

2008 Wells, Nevada

Each cycle ofblue => yellow => red= 28 mm of displacement (half of the radar wavelength)away from the satellite

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data model data – model

Weston et al., 2012

Strike: 172°Dip: 38°Rake: –95°Mw: 6.06

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“wrapped” “unwrapped”

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50 km

Original unwrapped dataDownsampling

OptimizationSlip model

-1.3

1.3

Disp (m)

0

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Schmidt and Burgmann (2003)

Pritchard and Simons (2004) Wdowinski et al (2006)

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Los Angelestime span = 1 day

Page 24: Presentation on the background theory of InSAR

July 1992–March 1993 February 1993–March 1993

Snow!Atmosphere!

Page 25: Presentation on the background theory of InSAR

Decorrelation• Changes in radar scattering properties of pixels• Vegetation, snow, flooding, the passing of time… • Longer radar wavelengths less susceptible

Atmospheric “noise”• Refraction of microwaves by water vapor• “Static” part can resemble topography• “Turbulent” part can resemble deformation

Page 26: Presentation on the background theory of InSAR

Sentinel

12 (and then 6) day repeat in same orbitmean post event wait => 3 daysascending + descending => mean wait < 3 days

SENTINEL-1A and -1BEuropean Space AgencyLaunch Q2 2014, 2016

Page 27: Presentation on the background theory of InSAR

ALOS-2 by Japanese Aerospace Exploration Agency14-day repeat in same orbit23 cm wavelength – less decorrelation

Launched Summer 2014