SlideShare une entreprise Scribd logo
1  sur  25
Télécharger pour lire hors ligne
ALGAE:
             A FAST ALGEBRAIC ESTIMATION OF
            INTERFEROGRAM PHASE OFFSETS IN
                SPACE VARYING GEOMETRIES




      Stefano Tebaldini, Guido Gatti, Mauro Mariotti d’Alessandro, and Fabio Rocca

                                 Politecnico di Milano
                        Dipartimento di Elettronica e Informazione

IGARSS 2010, Honolulu
ALGebraic Altitude Estimation
ALGAE is an algebraic procedure for the geometrical interpretation of
  interferometric measurements from a multi-baseline SAR system
                              Features:
• Joint estimation of terrain topography and phase offsets
• Handles the case where the normal baselines undergo a large
  variation along the imaged swath
• Compatible with different kinds of a-priori information to carry out
  absolute phase calibration
• Fast
• Robust
Problem Statement
          SAR Interferometry has repeatedly been shown to constitute a major tool for the
          retrieval of terrain topography at vast scales
               • SAR imaging provide information about the target to sensor distance
                Information from multiple (≥2) images can be merged to locate the target in 3D
                             Track N
                                                               •   Interferometric phase differences provide high accuracy
                                                                   measurements, being sensitive to wavelength scale
               Track n                                             variations of the target to sensor distance
                                                                                          4
                                                                                               r     rm 
                                       rN
                                                                                  nm 
                                                                                   P             P      P

Reference                        rn                                                            n
 Track



                  θ
                         r
   elevation




                                            P   Pulse Envelope
                                                Wavelength
                                                ground range
               azimuth
Problem Statement
          SAR Interferometry has repeatedly been shown to constitute a major tool for the
          retrieval of terrain topography at vast scales
               • SAR imaging provide information about the target to sensor distance
                Information from multiple (≥2) images can be merged to locate the target in 3D
                         Track N
                                                              •   Interferometric phase differences provide high accuracy
                                                                  measurements, being sensitive to wavelength scale
               Track n                                            variations of the target to sensor distance
                                                                                     4
                                                                                          r     rm  drnP  drm 
                                      rN+drN
                                                                           P
                                                                                           P      P            P

Reference
                            rn +drn                                         nm
                                                                                          n
 Track
                                                              •   Though, distance measurements are affected by
                                                                  Propagation Disturbances (PDs), arising from
                  θ                                               uncompensated delay of the Radar echoes
   elevation




                   r + dr                                          o   Propagation through the atmosphere
                                                                   o   Residual platform motion

                                                              •   PDs make the retrieval of absolute topography nearly an
                                       P       Pulse Envelope     ill-posed problem in absence of a-priori information
                                               Wavelength
                                               ground range
               azimuth
Problem Statement

      •          Problem sensitivity is easily discussed considering phase variation w.r.t. target height:

                                                           4 nm P
                                                                                                        Kz  
                                                                                                                     1
                                         P
                                                 Kznmz P
                                                                    z                        z   P                        P
                                           nm
                                                             sin 
                                                                                                                nm          nm
                      Track m
 Track n
                                                              Kznm = Height to phase conversion factor for tracks n and m
             θ                                        •   Height error due to PDs is readily obtained as:
                  r
 elevation




                                                                                      sin  P
                                                                                 ez 
                                                                                   P
                                                                                            dr
                                Δθ                                                     nm
                                                                  drP = Total propagation error at point P
                                           P
                                             ΔzP      •   For a typical InSAR configuration Δθ = 1/1000 – 1/100
                                      ground range
                                                          => error amplification is huge
 azimuth
Problem Statement

      •          Problem sensitivity is easily discussed considering phase variation w.r.t. target height:

                                                                  4 nm P
                                                                                                            z  Kznm  nm
                                                                                                                                  1
                                                      Kznmz           z
                                                  P                     P                                        P         P


 Track n
                      Track m                     nm
                                                                    sin 
                                                                            Kznm = Height to phase conversion factor for tracks n and m
             θ                                                  •       Height error due to PDs is readily obtained as:
                  r
 elevation




                                                                                                    sin  P
                                                                                               ez 
                                                                                                 P
                                                                                                          dr
                                    Δθ                                                               nm
                                                                                drP = Total propagation error at point P
                                                  P
                                R                   ΔzP         •       For a typical InSAR configuration Δθ = 1/1000 – 1/100
                                     ΔzR
                                             ground range
                                                                        => error amplification is huge
 azimuth

       •     However, PDs typically exhibit a large decorrelation length w.r.t. to the SAR resolution cell
                 o     Atmospheric delay is uniform within about 1 km
                 o     The dynamics of platform deviations from nominal trajectory is slow w.r.t. to platform velocity

             This information allows accurate topography retrieval w.r.t. to a reference point
                                                                                                     sin 
                      P
                        nm        R
                                     nm     Kznm z  z  P       R
                                                                                  ezP  ezR 
                                                                                                     nm
                                                                                                           dr P  dr R   ezP
Problem Statement

       •         Still, the problem changes when the spatial variation of the height to phase conversion
                 factors is relevant. In this case:

                          Track m                              nm   nm  Kznmz P  Kznmz R
                                                                 P       R      P          R


                                                               Kznm z P  z R   Kznm  Kznm z R
 Track n
                                                                  P                      P      R

                 θ
                      r
 elevation




                                                               •   A new term arises, that depends on
                                        Δθ
                                                                     o   The spatial variation of Kz
                                                                     o   The true height of the reference point w.r.t. the
                                                    P                    reference ground plane
                                    R                 ΔzP
                                         ΔzR                   •   Impact on height estimation:
                                               ground range
 azimuth
                                                                                         Kznm  R
                                                                                            R
                                                                              e  e  1  P ez
                                                                               P     R
                                                                                      
                                                                                                                     Space Variant
                                                                                          Kznm 
                                                                               z     z                               Error
                                                                                              
             •       Even if PDs are perfectly compensated for by the phase locking operation, the error about the
                     reference point height results in a space variant error propagating throughout the scene
                      o      Particularly relevant for airborne geometries, where Kz can undergo a variation by a factor 3

                     Handling space varying geometries require precise external information about
                     the sensor to target distances for the reference point
An Algebraic Interpretation
The problem can be cast in general terms as:                         nP  KznP z P  nP
                                   Unwrapped
                                                                                                            PD at point P
                                   Interferometric phase
                                                           Height to phase     Target height at point P      in track n
                                   at point P in track n
                                                           conversion factor at w.r.t. the reference
                                                           point P in track n       topography

 Stacking all phase measurements we get:
                                                                         z                              Topography
                                                                Gm  G                                 [NP × 1]

                                                                          
                                                Data
                                              [N∙NP × 1]                                            Parameters describing
                                                                                                      PDs in all tracks
                                                                 Forward Operator                         [Nα × 1]
Forward Problem                                                  [N∙NP × (Nα+ NP)]

This problem admits the general solution:
   z                                          The null space determines the ambiguity of the problem
      G   NG c                           o     Data fit is invariant w.r.t. to the choice of c
    
                                              The constants c represent the degrees of freedom of the
       Pseudo-                  Set of
                               arbitrary
                                              problem, providing the proper access point to plug
     Inverse of G Null Space
                    of G       constants      external information into the solution
Inverse Problem
An Algebraic Interpretation


   Remarks:
   •   Linearization about a reference topography does not entail any loss of generality, the
       eventual ambiguity or ill-conditioning of the inversion being intrinsic to the nature of the
       problem
   •   Linearization error can be recovered through iterative inversion methods (Newton-Raphson)
An Algebraic Interpretation


   Remarks:
   •       Linearization about a reference topography does not entail any loss of generality, the
           eventual ambiguity or ill-conditioning of the inversion being intrinsic to the nature of the
           problem
   •       Linearization error can be recovered through iterative inversion methods (Newton-Raphson)


       Remarks (II):                                              z
       •    How many parameters for the PDs?             Gm  G  
                                                                   
       •    Correct choice depends on
             o   Extent of the imaged scene
             o   Physics of PDs (i.e.: atmosphere, dynamics of platform motion…)
             o   Precision of motion compensation procedures previously applied

       •    In this work we assume a constant phase offset in each track           nP  n   N  N
            The assumption is simplistic, yet:
             o   Valid on limited areas
             o   Allows the discussion of the effects of space varying geometries
An Algebraic Interpretation

  For the case of constant phase offsets it may be shown that:
       •    The forward operator allows a 1D null space if and only if the height to phase
            conversion factors undergo the same spatial variation in all tracks, i.e.:
                                        k , K 
                                             n
                                                      P
                                                            s.t. :       KznP  kn  K P                   (C1)

       •    If C1 is fulfilled, the general solution for terrain topography is given by:
                                  z P  zInversion  c  zNullspace            zNullspace  K P 
                                         P                P                     P                 1




  We distinguish three cases:
Spaceborne InSAR                          Airborne InSAR - Ideal                      Airborne InSAR – Real
Kz can be considered constant if the      Assuming parallel trajectories C1 is        C1 is not fulfilled
    swath is not too large                   fulfilled with                           => The problem is well posed
 => C1 is fulfilled with:                         kn  bn / b1                        => Retrieval of absolute terrain
                                                                                         topography is theoretically
              kn  Kzn                            K P  K P r P , sin  P              possible
               KP 1                      => Terrain topography is retrieved
=> Terrain topography is retrieved            up to a space varying –
    up to a constant                          topography dependent – term
           z P  zInversion  c                  z P  zInversion  c  K P 
                  P                                     P                       1
ALGebraic Altitude Estimation
                                                                               Spaceborne
Absence of the null space is only apparently an




                                                                 Singular
                                                                  Values
advantage
                                                                                                0
• The problem is extremely ill-conditioned, the last                         Airborne - Ideal
Singular Value being very close to zero




                                                                 Singular
                                                                  Values
• Consistent with the arising of a 1D null space in nominal                                     0
conditions                                                                    Airborne - Real




                                                                Singular
                                                                 Values
                                                                                                0.002



                                         ALGAE
• The forward operator is modified by zeroing the last Singular Value (Truncated SVD)
     Ill-conditioning problems are solved, at the expense of the arising of a 1D null space

                                         z P  zInversion  c  zNullspace
                                                P                P



• The value of c is then determined according to the available a-priori information
     o Point match with an accurately measured reference point
     o Best global match with coarse reference DEM
     o Zeroing mean slope
     o Other….
Experimental Results
The boreal forest in the Krycklan catchment, northern Sweden, has been investigated in
the framework of the ESA campaign BioSAR 2008
Scene:
 o   Boreal forest
 o   Hilly topographic, height variations up to 200 m

Data has been acquired by the airborne system E-SAR,
flown by DLR
Data focusing, calibration, and co-registration have
been performed by DLR

Data-set under analysis
o    P-Band
o    Look Directions: South West and
     North East (6 + 6 tracks)
o    Nominal look between 25° and 55°
o    100 MHz pulse bandwidth
o    1.6 m azimuth resolution
o    2.12 m slant range resolution
o    40 m horizontal baseline aperture
o    Imaged area is 2.3 × 9.5 km2
Pre-Processing
Pre-Processing Operations
• The Algebraic Synthesis technique is used to extract contributions from ground-only scattering,
thus avoiding being affected by vegetation bias
• The retrieved ground-only contributions are processed with the Phase Linking algorithm to
estimate the ground phases with respect to a common Master
• Ground phases are unwrapped, and used as input for ALGAE


    Multi-Baseline,                  Phase
   Multi-Polarimetric               Linking                       Unwrapped
         Data                      Algorithm                    interferometric                  ALGAE
                                                                 ground phases
                              Best Estimate of the
                                Ground Phases
       Algebraic               with respect to a     Algebraic Synthesis:
       Synthesis               Common Master             “Algebraic Synthesis of Forest Scenarios from Multi-
                                                         baseline PolInSAR data” –Tebaldini – TGARS vol 47, no 12,
                                                         Dec.2009
                                 2-Dimensional
                                     Phase
     Ground-only                                     Phase Linking:
                                  Unwrapping
     Contributions                                       “On the Exploitation of Target Statistics for SAR
                                                         Interferometry Applications” – Monti Guarnieri and Tebaldini –
                                                         TGARS vol 46, no 11, Nov.2008
Algebraic Synthesis
Algebraic Synthesis (AS)  technique for the decomposition of Ground and Volume
scattering basing on multi-polarimetric and multi-baseline SAR surveys

                                                Track n
                       y n wi                Polarization wi
                                                                                                                               Track N
          Re{yn(w1)}               Re{yn(w2)}                   Re{yn(w3)}


                                                                                                             Track n           HH HV
                                                                                                                               VH VV
          Im{yn(w1)}               Im{yn(w2)}               Im{yn(w3)}

                                                                                                   Track 1             HH HV
                                                                                                                       VH VV

                           Volume Contributions                                                              HH HV
                                                       60
                                                       50
                                                       40                                                    VH VV
                                                       30
                                                       20
                                                       10
                                                        0
                                                      -10
                                                            200     600    1000    1400   1800   2200
   Algebraic
   Synthesis
                           Ground Contributions                                                         Ground
                                                     60
                                                     50
                                                     40
                                                     30
                                                     20
                                                     10
                                                      0
                                                    -10
                                                          200      600    1000    1400    1800   2200
Algebraic Synthesis
Algebraic Synthesis (AS)  technique for the decomposition of Ground and Volume
scattering basing on multi-polarimetric and multi-baseline SAR surveys

                                                Track n
                       y n wi                Polarization wi
                                                                                                                             Track N
          Re{yn(w1)}               Re{yn(w2)}                   Re{yn(w3)}


                                                                                                           Track n           HH HV
                                                                                                                             VH VV
          Im{yn(w1)}               Im{yn(w2)}               Im{yn(w3)}

                                                                                                 Track 1             HH HV
                                                                                                                     VH VV

                           Volume Contributions                                                            HH HV
                                                       60
                                                       50
                                                       40                                                  VH VV
                                                       30
                                                       20
                                                       10
                                                        0
                                                      -10
                                                            200     600   Further details in: POLARIMETRIC AND
                                                                           1000 1400 1800  2200
   Algebraic                                                              STRUCTURAL PROPERTIES OF FOREST
   Synthesis                                                              SCENARIOS AS IMAGED BY LONGER
                           Ground Contributions                           WAVELENGTH SARS       Ground
                                                     60
                                                     50
                                                     40                   Poster Session: THP2.PA.3 - Radar Mapping
                                                     30
                                                     20
                                                     10
                                                                          Thursday, July 29, 14:55 - 16:00
                                                      0
                                                    -10
                                                          200      600    1000   1400   1800   2200
Phase Linking
Retrieving the set of the ground interferometric coherences does not solve the problem of
retrieving the ground phases, since ground scattering can be affected by decorrelation
phenomena such as:
       • Temporal decorrelation             • Superficial decorrelation                     • Thermal noise


This problem is solved by the Phase Linking algorithm
 • Multi-baseline Maximum Likelihood estimation of the phases associated with the optical path
   lengths from a target to the N SAR sensors, accounting for target decorrelation phenomena

   Interferogram phases:                                                                               Track N

   n  y ref  y    4 r ref  r n    ref   n   + Phase Noise                   Track n
                    n
                           
                                                                                                             rN
       Linked phases:                                                       Reference                   rn
                                          Minimum Variance Phase             Track
    n  4 r ref  r n    ref   n + Noise given N tracks
         
                                                                                                      rref


                                                                                elevation
 rn : distance to the n-th SAR sensor
 αn : Propagation Disturbance in the n-th acquisition
                                                                                                                  ground range
Preliminary Analysis
                  LIDAR DEM                        Ground Range Slope   Ground Range Slope




    350

    300                                     10
    250

    200                                      0
    150

                                            -10
•     Ground coherence is extremely
      high
                                                   Ground Coherence     Ground Coherence
       excellent ground visibility
       excellent temporal stability
•     A slight trend w.r.t. the incidence
      angle can be (correctly!)
      appreciated in both directions        1
•     The spatial variation of ground
      coherence is clearly correlated       0.75
      with terrain slope, regardless of
      heading direction                     0.5
Preliminary Analysis
                                                   Height to Phase Conversion Factors
                                                   Track 1                  Track 2 (Master)
•   South-West Data-set




                                  slant range
•   Large range variation
     range and look angle
    variation within the imaged
    swath
•   Large azimuth variation                        Track 3                      Track 4
     Platform motion
                                  slant range




                                                   Track 5                      Track 6
                                  slant range




                                                    azimuth                      azimuth
Preliminary Analysis
                                                            Ground Phases
                                                 Track 1                    Track 2 (Master)
•   South-West Data-set
•   LIDAR DEM removed



                                slant range
•   Fringes are high quality,
    consistently with the
    observed high ground
    coherence                                    Track 3                        Track 4
•   Fringes are correlated
                                slant range




    with the Kz
     non-perfect
    compensation of platform
    deviation from nominal
    trajectories
                                                 Track 5                        Track 6
                                slant range




                                                  azimuth                        azimuth
ALGAE - Results
South West data-set

                Least Square Solution                Null Space



                              Look Direction
ALGAE - Results
South West data-set
        Null Space - High Pass Component                                  ALGAE Solution




•   Null space = along range trend + azimuth oscillations        •   Along-range errors recovered
•   The null space is added so as to zero the mean range slope   •   Along-azimuth errors partly recovered
ALGAE - Results
South West data-set

                Least Square Solution                   Null Space




        Look Direction




•   Same reference point as in the SW data-set brings
    to a large trend in the LS solution
ALGAE - Results
South West data-set

        Null Space - High Pass Component                                  ALGAE Solution




•   Null space = along range trend + azimuth oscillations        •   Along-range errors recovered
•   The null space is added so as to zero the mean range slope   •   Along-azimuth errors partly recovered
Conclusions
Space varying geometries result in space variant topographic errors that can not be fixed by
evaluating terrain topography w.r.t. one reference point

ALGAE defines an algebraic framework where space variance and propagation disturbances are
explicitly accounted for
     o   Propagation disturbances represented as constant phase offsets and estimated along with topography
     o   The degree of freedom provided by the concept of null space is compatible with different kinds of
         a-priori information, either local or global
     o   Fast
     o   Robust

Residual DEM errors:
     o characterized by a large spatial decorrelation length
     o correlated with the flight direction
     => Presence of residual phase terms due to residual platform motion  Insufficiency of the constant
          phase offset model

Future researches:
• Incorporate more sophisticated models to describe propagation disturbances, taking into account
both the physics of atmospheric propagation and platform motion

Contenu connexe

Tendances

Foss4g2009tokyo Realini Go Gps
Foss4g2009tokyo Realini Go GpsFoss4g2009tokyo Realini Go Gps
Foss4g2009tokyo Realini Go GpsOSgeo Japan
 
4-IGARSS_2011_v4.ppt
4-IGARSS_2011_v4.ppt4-IGARSS_2011_v4.ppt
4-IGARSS_2011_v4.pptgrssieee
 
5_1555_TH4.T01.5_suwa.ppt
5_1555_TH4.T01.5_suwa.ppt5_1555_TH4.T01.5_suwa.ppt
5_1555_TH4.T01.5_suwa.pptgrssieee
 
Synchronous Time and Frequency Domain Analysis of Embedded Systems
Synchronous Time and Frequency Domain Analysis of Embedded SystemsSynchronous Time and Frequency Domain Analysis of Embedded Systems
Synchronous Time and Frequency Domain Analysis of Embedded SystemsRohde & Schwarz North America
 
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...sipij
 
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...Chief Technologist Office
 
Від побудови сейсмічних зображень до інверсії
Від побудови сейсмічних зображень до інверсіїВід побудови сейсмічних зображень до інверсії
Від побудови сейсмічних зображень до інверсіїSergey Starokadomsky
 
GeoStreamer PESA News 042009 Andrew Long
GeoStreamer PESA News 042009 Andrew LongGeoStreamer PESA News 042009 Andrew Long
GeoStreamer PESA News 042009 Andrew LongAndrew Long
 
IDS Survey on Entropy
IDS Survey  on Entropy IDS Survey  on Entropy
IDS Survey on Entropy Raj Kamal
 
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...pmloscholte
 
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assay
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba AssayPitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assay
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assayinscore
 
Effects of Long Duration Motions on Ground Failure - Steve Kramer
Effects of Long Duration Motions on Ground Failure - Steve KramerEffects of Long Duration Motions on Ground Failure - Steve Kramer
Effects of Long Duration Motions on Ground Failure - Steve KramerEERI
 

Tendances (15)

Foss4g2009tokyo Realini Go Gps
Foss4g2009tokyo Realini Go GpsFoss4g2009tokyo Realini Go Gps
Foss4g2009tokyo Realini Go Gps
 
4-IGARSS_2011_v4.ppt
4-IGARSS_2011_v4.ppt4-IGARSS_2011_v4.ppt
4-IGARSS_2011_v4.ppt
 
5_1555_TH4.T01.5_suwa.ppt
5_1555_TH4.T01.5_suwa.ppt5_1555_TH4.T01.5_suwa.ppt
5_1555_TH4.T01.5_suwa.ppt
 
Synchronous Time and Frequency Domain Analysis of Embedded Systems
Synchronous Time and Frequency Domain Analysis of Embedded SystemsSynchronous Time and Frequency Domain Analysis of Embedded Systems
Synchronous Time and Frequency Domain Analysis of Embedded Systems
 
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...
SHIPS MATCHING BASED ON AN ADAPTIVE ACOUSTIC SPECTRUM SIGNATURE DETECTION ALG...
 
Hl3413921395
Hl3413921395Hl3413921395
Hl3413921395
 
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...
Molecular Rayleigh Scattering to Measure Fluctuations in Density, Velocity an...
 
Від побудови сейсмічних зображень до інверсії
Від побудови сейсмічних зображень до інверсіїВід побудови сейсмічних зображень до інверсії
Від побудови сейсмічних зображень до інверсії
 
GeoStreamer PESA News 042009 Andrew Long
GeoStreamer PESA News 042009 Andrew LongGeoStreamer PESA News 042009 Andrew Long
GeoStreamer PESA News 042009 Andrew Long
 
IDS Survey on Entropy
IDS Survey  on Entropy IDS Survey  on Entropy
IDS Survey on Entropy
 
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...
1988 a study of the thermal switching behavior in gd tbfe magneto‐optic films...
 
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assay
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba AssayPitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assay
Pitt Conn 2012 Fi Cs As Invited Sers Talks Ba Assay
 
Caballero
CaballeroCaballero
Caballero
 
Effects of Long Duration Motions on Ground Failure - Steve Kramer
Effects of Long Duration Motions on Ground Failure - Steve KramerEffects of Long Duration Motions on Ground Failure - Steve Kramer
Effects of Long Duration Motions on Ground Failure - Steve Kramer
 
elba11
elba11elba11
elba11
 

En vedette

Jackson072311.ppt
Jackson072311.pptJackson072311.ppt
Jackson072311.pptgrssieee
 
FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...
 FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE... FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...
FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...grssieee
 
Constructing a long time series of soil moisture using SMOS data with statist...
Constructing a long time series of soil moisture using SMOS data with statist...Constructing a long time series of soil moisture using SMOS data with statist...
Constructing a long time series of soil moisture using SMOS data with statist...grssieee
 
TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE
  TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE  TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE
TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTUREgrssieee
 
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIES
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIESTHE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIES
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIESgrssieee
 
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...grssieee
 
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODEL
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODELSEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODEL
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODELgrssieee
 
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...grssieee
 

En vedette (9)

Jackson072311.ppt
Jackson072311.pptJackson072311.ppt
Jackson072311.ppt
 
FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...
 FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE... FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...
FR2.L10.3: TOWARDS VALIDATION OF SMOS LAND PRODUCTS USING THE SYNERGY BETWEE...
 
Constructing a long time series of soil moisture using SMOS data with statist...
Constructing a long time series of soil moisture using SMOS data with statist...Constructing a long time series of soil moisture using SMOS data with statist...
Constructing a long time series of soil moisture using SMOS data with statist...
 
TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE
  TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE  TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE
TH4.L10.1: SMOS SMAP SYNERGISMS FOR THE RETRIEVAL OF SOIL MOISTURE
 
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIES
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIESTHE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIES
THE SENTINEL-1 MISSION AND ITS APPLICATION CAPABILITIES
 
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...
TWO-POINT STATISTIC OF POLARIMETRIC SAR DATA TWO-POINT STATISTIC OF POLARIMET...
 
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODEL
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODELSEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODEL
SEGMENTATION OF POLARIMETRIC SAR DATA WITH A MULTI-TEXTURE PRODUCT MODEL
 
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...
Tangent height accuracy of Superconducting Submillimeter-Wave Limb-Emission S...
 
Slideshare ppt
Slideshare pptSlideshare ppt
Slideshare ppt
 

Plus de grssieee

GMES SPACE COMPONENT:PROGRAMMATIC STATUS
GMES SPACE COMPONENT:PROGRAMMATIC STATUSGMES SPACE COMPONENT:PROGRAMMATIC STATUS
GMES SPACE COMPONENT:PROGRAMMATIC STATUSgrssieee
 
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETER
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETERPROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETER
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETERgrssieee
 
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...grssieee
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...grssieee
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...grssieee
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...grssieee
 
test 34mb wo animations
test  34mb wo animationstest  34mb wo animations
test 34mb wo animationsgrssieee
 
2011_Fox_Tax_Worksheets.pdf
2011_Fox_Tax_Worksheets.pdf2011_Fox_Tax_Worksheets.pdf
2011_Fox_Tax_Worksheets.pdfgrssieee
 
DLR open house
DLR open houseDLR open house
DLR open housegrssieee
 
DLR open house
DLR open houseDLR open house
DLR open housegrssieee
 
DLR open house
DLR open houseDLR open house
DLR open housegrssieee
 
Tana_IGARSS2011.ppt
Tana_IGARSS2011.pptTana_IGARSS2011.ppt
Tana_IGARSS2011.pptgrssieee
 
Solaro_IGARSS_2011.ppt
Solaro_IGARSS_2011.pptSolaro_IGARSS_2011.ppt
Solaro_IGARSS_2011.pptgrssieee
 
Sakkas.ppt
Sakkas.pptSakkas.ppt
Sakkas.pptgrssieee
 
Lagios_et_al_IGARSS_2011.ppt
Lagios_et_al_IGARSS_2011.pptLagios_et_al_IGARSS_2011.ppt
Lagios_et_al_IGARSS_2011.pptgrssieee
 
IGARSS-GlobWetland-II_2011-07-20_v2-0.ppt
IGARSS-GlobWetland-II_2011-07-20_v2-0.pptIGARSS-GlobWetland-II_2011-07-20_v2-0.ppt
IGARSS-GlobWetland-II_2011-07-20_v2-0.pptgrssieee
 

Plus de grssieee (20)

GMES SPACE COMPONENT:PROGRAMMATIC STATUS
GMES SPACE COMPONENT:PROGRAMMATIC STATUSGMES SPACE COMPONENT:PROGRAMMATIC STATUS
GMES SPACE COMPONENT:PROGRAMMATIC STATUS
 
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETER
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETERPROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETER
PROGRESSES OF DEVELOPMENT OF CFOSAT SCATTEROMETER
 
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...
DEVELOPMENT OF ALGORITHMS AND PRODUCTS FOR SUPPORTING THE ITALIAN HYPERSPECTR...
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
 
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
EO-1/HYPERION: NEARING TWELVE YEARS OF SUCCESSFUL MISSION SCIENCE OPERATION A...
 
Test
TestTest
Test
 
test 34mb wo animations
test  34mb wo animationstest  34mb wo animations
test 34mb wo animations
 
Test 70MB
Test 70MBTest 70MB
Test 70MB
 
Test 70MB
Test 70MBTest 70MB
Test 70MB
 
2011_Fox_Tax_Worksheets.pdf
2011_Fox_Tax_Worksheets.pdf2011_Fox_Tax_Worksheets.pdf
2011_Fox_Tax_Worksheets.pdf
 
DLR open house
DLR open houseDLR open house
DLR open house
 
DLR open house
DLR open houseDLR open house
DLR open house
 
DLR open house
DLR open houseDLR open house
DLR open house
 
Tana_IGARSS2011.ppt
Tana_IGARSS2011.pptTana_IGARSS2011.ppt
Tana_IGARSS2011.ppt
 
Solaro_IGARSS_2011.ppt
Solaro_IGARSS_2011.pptSolaro_IGARSS_2011.ppt
Solaro_IGARSS_2011.ppt
 
Sakkas.ppt
Sakkas.pptSakkas.ppt
Sakkas.ppt
 
Rocca.ppt
Rocca.pptRocca.ppt
Rocca.ppt
 
Lagios_et_al_IGARSS_2011.ppt
Lagios_et_al_IGARSS_2011.pptLagios_et_al_IGARSS_2011.ppt
Lagios_et_al_IGARSS_2011.ppt
 
IGARSS-GlobWetland-II_2011-07-20_v2-0.ppt
IGARSS-GlobWetland-II_2011-07-20_v2-0.pptIGARSS-GlobWetland-II_2011-07-20_v2-0.ppt
IGARSS-GlobWetland-II_2011-07-20_v2-0.ppt
 

ALGAE: An Algebraic Estimation of Interferogram Phase Offsets

  • 1. ALGAE: A FAST ALGEBRAIC ESTIMATION OF INTERFEROGRAM PHASE OFFSETS IN SPACE VARYING GEOMETRIES Stefano Tebaldini, Guido Gatti, Mauro Mariotti d’Alessandro, and Fabio Rocca Politecnico di Milano Dipartimento di Elettronica e Informazione IGARSS 2010, Honolulu
  • 2. ALGebraic Altitude Estimation ALGAE is an algebraic procedure for the geometrical interpretation of interferometric measurements from a multi-baseline SAR system Features: • Joint estimation of terrain topography and phase offsets • Handles the case where the normal baselines undergo a large variation along the imaged swath • Compatible with different kinds of a-priori information to carry out absolute phase calibration • Fast • Robust
  • 3. Problem Statement SAR Interferometry has repeatedly been shown to constitute a major tool for the retrieval of terrain topography at vast scales • SAR imaging provide information about the target to sensor distance  Information from multiple (≥2) images can be merged to locate the target in 3D Track N • Interferometric phase differences provide high accuracy measurements, being sensitive to wavelength scale Track n variations of the target to sensor distance 4 r  rm  rN nm  P P P Reference rn  n Track θ r elevation P Pulse Envelope Wavelength ground range azimuth
  • 4. Problem Statement SAR Interferometry has repeatedly been shown to constitute a major tool for the retrieval of terrain topography at vast scales • SAR imaging provide information about the target to sensor distance  Information from multiple (≥2) images can be merged to locate the target in 3D Track N • Interferometric phase differences provide high accuracy measurements, being sensitive to wavelength scale Track n variations of the target to sensor distance 4 r  rm  drnP  drm  rN+drN  P  P P P Reference rn +drn nm  n Track • Though, distance measurements are affected by Propagation Disturbances (PDs), arising from θ uncompensated delay of the Radar echoes elevation r + dr o Propagation through the atmosphere o Residual platform motion • PDs make the retrieval of absolute topography nearly an P Pulse Envelope ill-posed problem in absence of a-priori information Wavelength ground range azimuth
  • 5. Problem Statement • Problem sensitivity is easily discussed considering phase variation w.r.t. target height: 4 nm P  Kz   1  P  Kznmz P z z P P nm  sin  nm nm Track m Track n Kznm = Height to phase conversion factor for tracks n and m θ • Height error due to PDs is readily obtained as: r elevation sin  P ez  P dr Δθ  nm drP = Total propagation error at point P P ΔzP • For a typical InSAR configuration Δθ = 1/1000 – 1/100 ground range => error amplification is huge azimuth
  • 6. Problem Statement • Problem sensitivity is easily discussed considering phase variation w.r.t. target height: 4 nm P z  Kznm  nm 1   Kznmz  z P P P P Track n Track m nm  sin  Kznm = Height to phase conversion factor for tracks n and m θ • Height error due to PDs is readily obtained as: r elevation sin  P ez  P dr Δθ  nm drP = Total propagation error at point P P R ΔzP • For a typical InSAR configuration Δθ = 1/1000 – 1/100 ΔzR ground range => error amplification is huge azimuth • However, PDs typically exhibit a large decorrelation length w.r.t. to the SAR resolution cell o Atmospheric delay is uniform within about 1 km o The dynamics of platform deviations from nominal trajectory is slow w.r.t. to platform velocity This information allows accurate topography retrieval w.r.t. to a reference point sin   P nm   R nm  Kznm z  z P R  ezP  ezR  nm dr P  dr R   ezP
  • 7. Problem Statement • Still, the problem changes when the spatial variation of the height to phase conversion factors is relevant. In this case: Track m  nm   nm  Kznmz P  Kznmz R P R P R  Kznm z P  z R   Kznm  Kznm z R Track n P P R θ r elevation • A new term arises, that depends on Δθ o The spatial variation of Kz o The true height of the reference point w.r.t. the P reference ground plane R ΔzP ΔzR • Impact on height estimation: ground range azimuth  Kznm  R R e  e  1  P ez P R  Space Variant Kznm  z z Error   • Even if PDs are perfectly compensated for by the phase locking operation, the error about the reference point height results in a space variant error propagating throughout the scene o Particularly relevant for airborne geometries, where Kz can undergo a variation by a factor 3 Handling space varying geometries require precise external information about the sensor to target distances for the reference point
  • 8. An Algebraic Interpretation The problem can be cast in general terms as: nP  KznP z P  nP Unwrapped PD at point P Interferometric phase Height to phase Target height at point P in track n at point P in track n conversion factor at w.r.t. the reference point P in track n topography Stacking all phase measurements we get: z Topography   Gm  G   [NP × 1]   Data [N∙NP × 1] Parameters describing PDs in all tracks Forward Operator [Nα × 1] Forward Problem [N∙NP × (Nα+ NP)] This problem admits the general solution: z The null space determines the ambiguity of the problem    G   NG c o Data fit is invariant w.r.t. to the choice of c   The constants c represent the degrees of freedom of the Pseudo- Set of arbitrary problem, providing the proper access point to plug Inverse of G Null Space of G constants external information into the solution Inverse Problem
  • 9. An Algebraic Interpretation Remarks: • Linearization about a reference topography does not entail any loss of generality, the eventual ambiguity or ill-conditioning of the inversion being intrinsic to the nature of the problem • Linearization error can be recovered through iterative inversion methods (Newton-Raphson)
  • 10. An Algebraic Interpretation Remarks: • Linearization about a reference topography does not entail any loss of generality, the eventual ambiguity or ill-conditioning of the inversion being intrinsic to the nature of the problem • Linearization error can be recovered through iterative inversion methods (Newton-Raphson) Remarks (II): z • How many parameters for the PDs?   Gm  G     • Correct choice depends on o Extent of the imaged scene o Physics of PDs (i.e.: atmosphere, dynamics of platform motion…) o Precision of motion compensation procedures previously applied • In this work we assume a constant phase offset in each track  nP  n N  N The assumption is simplistic, yet: o Valid on limited areas o Allows the discussion of the effects of space varying geometries
  • 11. An Algebraic Interpretation For the case of constant phase offsets it may be shown that: • The forward operator allows a 1D null space if and only if the height to phase conversion factors undergo the same spatial variation in all tracks, i.e.:  k , K  n P s.t. : KznP  kn  K P (C1) • If C1 is fulfilled, the general solution for terrain topography is given by: z P  zInversion  c  zNullspace zNullspace  K P  P P P 1 We distinguish three cases: Spaceborne InSAR Airborne InSAR - Ideal Airborne InSAR – Real Kz can be considered constant if the Assuming parallel trajectories C1 is C1 is not fulfilled swath is not too large fulfilled with => The problem is well posed => C1 is fulfilled with: kn  bn / b1 => Retrieval of absolute terrain topography is theoretically kn  Kzn K P  K P r P , sin  P  possible KP 1 => Terrain topography is retrieved => Terrain topography is retrieved up to a space varying – up to a constant topography dependent – term z P  zInversion  c z P  zInversion  c  K P  P P 1
  • 12. ALGebraic Altitude Estimation Spaceborne Absence of the null space is only apparently an Singular Values advantage 0 • The problem is extremely ill-conditioned, the last Airborne - Ideal Singular Value being very close to zero Singular Values • Consistent with the arising of a 1D null space in nominal 0 conditions Airborne - Real Singular Values 0.002 ALGAE • The forward operator is modified by zeroing the last Singular Value (Truncated SVD) Ill-conditioning problems are solved, at the expense of the arising of a 1D null space z P  zInversion  c  zNullspace P P • The value of c is then determined according to the available a-priori information o Point match with an accurately measured reference point o Best global match with coarse reference DEM o Zeroing mean slope o Other….
  • 13. Experimental Results The boreal forest in the Krycklan catchment, northern Sweden, has been investigated in the framework of the ESA campaign BioSAR 2008 Scene: o Boreal forest o Hilly topographic, height variations up to 200 m Data has been acquired by the airborne system E-SAR, flown by DLR Data focusing, calibration, and co-registration have been performed by DLR Data-set under analysis o P-Band o Look Directions: South West and North East (6 + 6 tracks) o Nominal look between 25° and 55° o 100 MHz pulse bandwidth o 1.6 m azimuth resolution o 2.12 m slant range resolution o 40 m horizontal baseline aperture o Imaged area is 2.3 × 9.5 km2
  • 14. Pre-Processing Pre-Processing Operations • The Algebraic Synthesis technique is used to extract contributions from ground-only scattering, thus avoiding being affected by vegetation bias • The retrieved ground-only contributions are processed with the Phase Linking algorithm to estimate the ground phases with respect to a common Master • Ground phases are unwrapped, and used as input for ALGAE Multi-Baseline, Phase Multi-Polarimetric Linking Unwrapped Data Algorithm interferometric ALGAE ground phases Best Estimate of the Ground Phases Algebraic with respect to a Algebraic Synthesis: Synthesis Common Master “Algebraic Synthesis of Forest Scenarios from Multi- baseline PolInSAR data” –Tebaldini – TGARS vol 47, no 12, Dec.2009 2-Dimensional Phase Ground-only Phase Linking: Unwrapping Contributions “On the Exploitation of Target Statistics for SAR Interferometry Applications” – Monti Guarnieri and Tebaldini – TGARS vol 46, no 11, Nov.2008
  • 15. Algebraic Synthesis Algebraic Synthesis (AS)  technique for the decomposition of Ground and Volume scattering basing on multi-polarimetric and multi-baseline SAR surveys Track n y n wi   Polarization wi Track N Re{yn(w1)} Re{yn(w2)} Re{yn(w3)} Track n HH HV VH VV Im{yn(w1)} Im{yn(w2)} Im{yn(w3)} Track 1 HH HV VH VV Volume Contributions HH HV 60 50 40 VH VV 30 20 10 0 -10 200 600 1000 1400 1800 2200 Algebraic Synthesis Ground Contributions Ground 60 50 40 30 20 10 0 -10 200 600 1000 1400 1800 2200
  • 16. Algebraic Synthesis Algebraic Synthesis (AS)  technique for the decomposition of Ground and Volume scattering basing on multi-polarimetric and multi-baseline SAR surveys Track n y n wi   Polarization wi Track N Re{yn(w1)} Re{yn(w2)} Re{yn(w3)} Track n HH HV VH VV Im{yn(w1)} Im{yn(w2)} Im{yn(w3)} Track 1 HH HV VH VV Volume Contributions HH HV 60 50 40 VH VV 30 20 10 0 -10 200 600 Further details in: POLARIMETRIC AND 1000 1400 1800 2200 Algebraic STRUCTURAL PROPERTIES OF FOREST Synthesis SCENARIOS AS IMAGED BY LONGER Ground Contributions WAVELENGTH SARS Ground 60 50 40 Poster Session: THP2.PA.3 - Radar Mapping 30 20 10 Thursday, July 29, 14:55 - 16:00 0 -10 200 600 1000 1400 1800 2200
  • 17. Phase Linking Retrieving the set of the ground interferometric coherences does not solve the problem of retrieving the ground phases, since ground scattering can be affected by decorrelation phenomena such as: • Temporal decorrelation • Superficial decorrelation • Thermal noise This problem is solved by the Phase Linking algorithm • Multi-baseline Maximum Likelihood estimation of the phases associated with the optical path lengths from a target to the N SAR sensors, accounting for target decorrelation phenomena Interferogram phases: Track N  n  y ref  y    4 r ref  r n    ref   n + Phase Noise Track n n  rN Linked phases: Reference rn Minimum Variance Phase Track  n  4 r ref  r n    ref   n + Noise given N tracks  rref elevation rn : distance to the n-th SAR sensor αn : Propagation Disturbance in the n-th acquisition ground range
  • 18. Preliminary Analysis LIDAR DEM Ground Range Slope Ground Range Slope 350 300 10 250 200 0 150 -10 • Ground coherence is extremely high Ground Coherence Ground Coherence  excellent ground visibility  excellent temporal stability • A slight trend w.r.t. the incidence angle can be (correctly!) appreciated in both directions 1 • The spatial variation of ground coherence is clearly correlated 0.75 with terrain slope, regardless of heading direction 0.5
  • 19. Preliminary Analysis Height to Phase Conversion Factors Track 1 Track 2 (Master) • South-West Data-set slant range • Large range variation  range and look angle variation within the imaged swath • Large azimuth variation Track 3 Track 4  Platform motion slant range Track 5 Track 6 slant range azimuth azimuth
  • 20. Preliminary Analysis Ground Phases Track 1 Track 2 (Master) • South-West Data-set • LIDAR DEM removed slant range • Fringes are high quality, consistently with the observed high ground coherence Track 3 Track 4 • Fringes are correlated slant range with the Kz  non-perfect compensation of platform deviation from nominal trajectories Track 5 Track 6 slant range azimuth azimuth
  • 21. ALGAE - Results South West data-set Least Square Solution Null Space Look Direction
  • 22. ALGAE - Results South West data-set Null Space - High Pass Component ALGAE Solution • Null space = along range trend + azimuth oscillations • Along-range errors recovered • The null space is added so as to zero the mean range slope • Along-azimuth errors partly recovered
  • 23. ALGAE - Results South West data-set Least Square Solution Null Space Look Direction • Same reference point as in the SW data-set brings to a large trend in the LS solution
  • 24. ALGAE - Results South West data-set Null Space - High Pass Component ALGAE Solution • Null space = along range trend + azimuth oscillations • Along-range errors recovered • The null space is added so as to zero the mean range slope • Along-azimuth errors partly recovered
  • 25. Conclusions Space varying geometries result in space variant topographic errors that can not be fixed by evaluating terrain topography w.r.t. one reference point ALGAE defines an algebraic framework where space variance and propagation disturbances are explicitly accounted for o Propagation disturbances represented as constant phase offsets and estimated along with topography o The degree of freedom provided by the concept of null space is compatible with different kinds of a-priori information, either local or global o Fast o Robust Residual DEM errors: o characterized by a large spatial decorrelation length o correlated with the flight direction => Presence of residual phase terms due to residual platform motion  Insufficiency of the constant phase offset model Future researches: • Incorporate more sophisticated models to describe propagation disturbances, taking into account both the physics of atmospheric propagation and platform motion