Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment...

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Lyons and Sandwell, JGR, 2003 Landers EQ Hector Mine EQ

Transcript of Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment...

Page 1: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

Lyons and Sandwell, JGR, 2003

LandersEQ

Hector MineEQ

Page 2: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

http://topex.ucsd.edu/gmtsar

Page 3: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
Page 4: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

forming interferogram

Page 5: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
Page 6: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
Page 7: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

B = Bsin θ −α( )

B⊥ = Bcos θ −α( )

∂φ∂ρ

=−4πBλρ

cos θ −α( )sinθ

cosθ − ρb

)*+

,-.

φ − φe( ) ≅ −4πreBcos θ −α( )λρbsinθ

(r − re )

phase due to curved earth

phase due to topography

Perpendicular baseline MATTERS!

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total phase

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Phase from curved Earth

Page 10: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

total phase

Page 11: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

Critical Baseline

Page 12: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

Phase from topography

Page 13: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

phase minus spherical earth

Page 14: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

How high is Toro Peak?

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deformation and topography

Page 16: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
Page 17: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
Page 18: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

Lyons and Sandwell, JGR, 2003

LandersEQ

Hector MineEQ

Page 19: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine

Triggered slip on Southern San Andreas Fault

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Need for Precise Orbits1.  proper focus

2.  transform from geographic radar coordinates

3.  image alignment

4.  flattening interferogram

Brute force algorithm given precise orbit subroutine pick target point fly satellite along orbit and identify point of closest approach(This is inefficient but computers are fast so don’t waste time coding.)

Page 21: Landers Hector Mine EQ - UNAVCO · transform from geographic radar coordinates 3. image alignment 4. flattening interferogram Brute force algorithm given precise orbit subroutine
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GMTSAR

2-pass processingno ground controlseamless abutment of frames along track

stacking for time seriesone master and many slavesprimary, secondary, tertiary, image alignment

ScanSAR Interferometrypossible but not easycode needs refinement