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•Remote
  Remote Sensing Laboratory   •Sensing
  Universitat Politècnica de Catalunya
                              •Laboratory




    Phase error assessment of
MIRAS/SMOS by means of Redundant
        Space Calibration

Rubén Dávila(1), Francesc Torres(1), Nuria Duffo(1), Ignasi
 Corbella(1), Miriam Pablos(1) and Manuel Martín-Neira (2)

(1) Remote Sensing Laboratory. Universitat Politècnica de Catalunya,
    Barcelona.SMOS Barcelona Expert Centre
(2) European Space Agency (ESA-ESTEC). Noordwijk. The Netherlands




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•Remote
            Remote Sensing Laboratory   •Sensing
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     The Soil Moisture & Ocean Salinity Earth Explorer Mission (ESA)
                                                                      Aperture Synthesis
                                                                  Interferometric Radiometer
                                                               • MIRAS instrument concept
                                                                     - Y-shaped array (arm length ~ 4.5 m)
                                                                     - 21 dual-pol. L-band antennas / arm
                                                                     - spacing 0.875 λ (~1400 MHz)
                                                                     -no scanning mechanisms,
                                                                            2D imaging by Fourier synthesis
                                                                     -(u,v) antenna separation in wavelengths

                                                              2D images formed by Fourier Synthesis
                                                             (ideal case). Cross correlation of the signals
                                                             collected by each antenna pair gives the so-
                                                             called: Visibility samples V(u,v):

   Launched November 2009
                                                                                        TB (ξ, η) − Tph        2
                                                                                                                  
                                                           V(u, v) =< b1 (t)b (t) >= F 
                                                                             *
                                                                             2                           F(ξ, η) 
(SMOS artist’s view, by EADS-CASA Space Division, Spain)
                                                                                        1−ξ −η
                                                                                       
                                                                                                 2    2
                                                                                                                  
                                                                                                                  
                                                      IGARSS 2011 Vancouver                                    2
•Remote
      Remote Sensing Laboratory   •Sensing
      Universitat Politècnica de Catalunya
                                  •Laboratory


 Simplified block diagram of a single baseline
                                                                      MIRAS measures
                                                                   normalized correlations:


                               antenna 1

                                                                                             Mkj
                                antenna 2



                                                 antenna planes

                                          System temperatures measured by a power detector in each receiver




Visibility sample at A                           TsysAk TsysAj
                    V = M kj
the antenna plane kj                                        jφkj
                                                               A
                                                                      Fringe Wash function at the origin (τ=0):
                                                Gkj (0) e              • Modulus (≈1)
                                           IGARSS 2011 Vancouver       • FWF Phase at antenna plane       3
•Remote
      Remote Sensing Laboratory   •Sensing
      Universitat Politècnica de Catalunya
                                  •Laboratory


                              Framework of the activity
SMOS is producing images within expected performance. However, there is
some degree of image distortion (spatial errors) due to a number of causes.

This research activity is devoted to assess the different contributions of
spatial errors, with two objectives in mind:
         • SMOS Improved performance
         • SMOS follow-on specifications

The RSC method is devoted to assess the peformance of phase calibration.

For calibration purposes, the phase calibration term (antenna plane) is modeled as:



                  φkj = (φkant − φ jant ) + (φkrec − φ jrec ) + φkj
                    A                                            FWF




             Antenna phase terms                Receiver phases    Fringe-wash term

                                           IGARSS 2011 Vancouver                      4
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                                    •Laboratory



                            SMOS phase calibration strategy

             • Receiver phase drift is calibrated by periodic (2-10 min) correlated noise
               injection (LO phase track)

             • Antenna phase term (manufacturing tolerances): Measured on ground

             • Fringe washing term due to filter response differences (negligible)
Antenna                     Receiver
 plane             φkant     plane       φkrec                    Antenna phase test set-up


                   A L                           receiver " k "
         η
                   C                                     M kj
 Noise injection
                                       Correlator
                   Switch


Front end phase model                            receiver " j "

                                                     IGARSS 2011 Vancouver                    5
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       Remote Sensing Laboratory   •Sensing
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                                   •Laboratory


                        Redundant Space Calibration (RSC)
Redundant baselines measure the same visibility using a different pair of antennas




                                                                        Redundant baselines




    Visibility phase measured by a baseline:           φVkj = φk − φj + φscene,kj
   RSC phase differences are independent of the phase of the scene

     Baseline phase differences:            φVkj − φVji =k − 2φj + φi
                                                         φ
                                            IGARSS 2011 Vancouver                             6
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          Remote Sensing Laboratory   •Sensing
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                                      •Laboratory



                                   RSC system of equations
     A system of equations can be built using independent RSC equations


0    0     1     −2     1     0    … …         0   
                                                   
0    0 0 1 −2 1 0 … 0                                                                 Applied on calibrated
…    … … … … … … … …                                                                  visibilities the RSC
                                                                                      method retrieves the
0    … … … … 0                     1    −2 1       ·φreceivers = φphase differences
…                                                                                     residual phase error
      … −1 1 … −1                   1    .. …
                                                   
…    −1 … 1 … …                    1    −1 …       
…    … … … … … … … …                               
                                                   
     A matrix: 66 x 69                                             Underdetermined system
     Receivers vector: 69 x 1                                  (three unknown phases, rank = 66)
     Phase differences vector: 66 x 1
                                                              Moore-Penrose pseudoinverse matrix
      66 equations, 69 unknowns

      Averaging is required to reduce uncertainty due to thermal noise
                                               IGARSS 2011 Vancouver                                       7
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                                   •Laboratory



   Averaging: visibility measurements must be carefully selected
   • Low visibility amplitude: produces unwanted variations and jumps
   • Fast scene changes: phase bias in land-ocean transitions
   • RFI: interferences that spoils the phase values

                                                        Land-ocean transition




Low visibility
  amplitude




                                                                                RFI



                                            IGARSS 2011 Vancouver                     8
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                            •Laboratory



      RSC: examples of good quality visibility samples



             Averaging
               area                            Averaging
                                                 area
                                                                         Averaging
                                                                           area


      Arm A                               Arm B                     Arm C




                                                     Red line: Average snap-shots




                                     IGARSS 2011 Vancouver                          9
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                                •Laboratory



                       RSC: Impact of undetermination
The 3 unknown phases have a physical meaning:




                    Tilt angle
                                                                 Steering angle




                                                                    Pointing error


   Common path delay                             Irrelevant
                                         IGARSS 2011 Vancouver                       10
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                               •Laboratory



             RSC: Pointing error in the phase retrievals
Simulations show that a pointing error yields a linear phase error directly
related to the antenna position in the arms.


                                                           φerror,bslN = a·u bslN + b·v bslN


                                                                                        a      b 
                                                    TBcalibrated (ξ, η) = TBideal  ξ −    ,η−    
                                                                                       2π     2π 
                                                                                  a
                                                                    ξps ' = ξps −
                                                                                 2π
                                                                                  b
                                                                    ηps ' = ps −
                                                                           η
                                                                                 2π

     Retrieval error linear in each arm
 The pointing error can be corrected, if required, using a point source (e.g, an
 interference at a known position ξps , ηps)

                                        IGARSS 2011 Vancouver                                    11
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                                •Laboratory



       Assessment on the pointing error in RSC retrievals
Simulation: SMOS point source retrieval by the RSC method: random phase error




         Ideal                           Phase corrupted         Corrected

    •Image blurring (example, σphases = 25º)
    • Secondary lobes increase
    • Small pointing error: the maximum has been displaced.
 Once the point source is RSC calibrated, image blurring and secondary lobes are
corrected. However, the pointing error is not compensated.
                                                                                   12
                                         IGARSS 2011 Vancouver
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                               •Laboratory



              RSC implementation (i): Good/bad estimations
Due to pointing error, the difference between two phase retrievals must be
linear. This property is used to discard bad estimations of the RSC phases
           φretrieved = φIVT,error + φpoint ing error
            1                         1


           φretrieved = φIVT,error + φpoint ing error
             2                        2


   φretrieved − φretrieved = φpoint ing error − φpoint ing error
     2           1            2                  1
                                                                                     Linear




                  Bad estimations                                           Good estimations
                                                    IGARSS 2011 Vancouver                      13
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       Remote Sensing Laboratory   •Sensing
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                                   •Laboratory



                                   RSC retrieved phases
Final RSC phases retrieved by averaging RSC phases from 38 orbits over the ocean

          Horizontal Phases                      Vertical Phases
                                                                      RSC Phase Error
                                                                        dispersion

                                                                        σH =5.97º
                                                                        σV =3.17º

                                                                    • RSC gives a conservative
     Horizontal Mean Phases                  Vertical Mean Phases
                                                                     upper bound for SMOS

                                                                     residual phase errors

                                                                    • RSC phase dispersion very

                                                                     much contributed by

                                                                     pointing error


                                            IGARSS 2011 Vancouver                          14
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      Remote Sensing Laboratory   •Sensing
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                                  •Laboratory



                 RSC: phase error impact of pointing error
                                                                   Mean pointing error (H)

                                                              Horizontal Phases
                                                                 Simulation

                         r
                                                              SMOS std




                                                   <r>
                                                               Horizontal Std
                                                                        σphases (°)
Simulation: point source shift for 200 cases
with σph=20º. 95% of points within a radius              σH =5.97º               σV =3.17º
r=2mrayleigh centred at the point source real
position
                                                         rH = 0.00066           rV = 0.00037
                                                    ∆L H = km
                                                         0.76                  ∆L V = km
                                                                                    0.43

             ΔLH and ΔLV below 2% of SMOS resolution (42 km)
                                           IGARSS 2011 Vancouver                               15
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Remote Sensing Laboratory   •Sensing
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                            •Laboratory



RSC peformance assesssment: RFI in the Caribbean Sea
           Interference from a vessel (11/02/2010, 21:23 semi-orbit)




                                   IGARSS 2011 Vancouver

                                                                       16
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RSC peformance assesssment: RFI in the Caribbean Sea
                                          Horizontal




                                IGARSS 2011 Vancouver

                                                        17
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                            •Laboratory



 RSC peformance assessment: RFI in the Caribbean Sea

– Primary to Secondary Lobe Ratio (H):
                        Case              Primary to Secondary Lobe Ratio
                 Real Point Source                   17,40 dB
             Corrected Point Source                  16,50 dB

– Primary to Secondary Lobe Ratio (V):
                        Case              Primary to Secondary Lobe Ratio
                Real Point Source                    17,40 dB
             Corrected Point Source                  16,65 dB

– The uncorrected RFI presents a main-to-secondary lobe ratio very
  close to an ideal point source.
– The RSC method uncertainty above SMOS phase error accuracy!!


                                                                            18
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Remote Sensing Laboratory   •Sensing
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                            •Laboratory



   RSC implementation: Interference in Cáceres (Spain)
                                          Vertical




                                                         19
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    Remote Sensing Laboratory   •Sensing
    Universitat Politècnica de Catalunya
                                •Laboratory



                                        Conclusions
• The RSC method cannot be used to phase calibrate SMOS in a per snap
shot basis due to the need for long averaging and filtering

• SMOS orbital phase drift requires periodic (2-10 min) correlated noise
injection (LO phase track)


• The RSC is used to validate the consistency of SMOS phase calibrated
visibilities:

    •RSC phase retrieval accuracy limited by undetermination (pointing
    error)
    •SMOS phase errors well below σH=5.97 º and σV=3.17º, probably very
    close to the σ =1º target

•Assessment on point sources (RFI) shows that the impact of SMOS
residual phase errors on image distortion is probably negligible
                                         IGARSS 2011 Vancouver        20

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Phase error assessment of MIRASSMOS by means of Redundant Space Calibration.pdf

  • 1. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Phase error assessment of MIRAS/SMOS by means of Redundant Space Calibration Rubén Dávila(1), Francesc Torres(1), Nuria Duffo(1), Ignasi Corbella(1), Miriam Pablos(1) and Manuel Martín-Neira (2) (1) Remote Sensing Laboratory. Universitat Politècnica de Catalunya, Barcelona.SMOS Barcelona Expert Centre (2) European Space Agency (ESA-ESTEC). Noordwijk. The Netherlands 1/20
  • 2. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory The Soil Moisture & Ocean Salinity Earth Explorer Mission (ESA) Aperture Synthesis Interferometric Radiometer • MIRAS instrument concept - Y-shaped array (arm length ~ 4.5 m) - 21 dual-pol. L-band antennas / arm - spacing 0.875 λ (~1400 MHz) -no scanning mechanisms, 2D imaging by Fourier synthesis -(u,v) antenna separation in wavelengths 2D images formed by Fourier Synthesis (ideal case). Cross correlation of the signals collected by each antenna pair gives the so- called: Visibility samples V(u,v): Launched November 2009  TB (ξ, η) − Tph 2  V(u, v) =< b1 (t)b (t) >= F  * 2 F(ξ, η)  (SMOS artist’s view, by EADS-CASA Space Division, Spain)  1−ξ −η  2 2   IGARSS 2011 Vancouver 2
  • 3. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Simplified block diagram of a single baseline MIRAS measures normalized correlations: antenna 1 Mkj antenna 2 antenna planes System temperatures measured by a power detector in each receiver Visibility sample at A TsysAk TsysAj V = M kj the antenna plane kj jφkj A Fringe Wash function at the origin (τ=0): Gkj (0) e • Modulus (≈1) IGARSS 2011 Vancouver • FWF Phase at antenna plane 3
  • 4. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Framework of the activity SMOS is producing images within expected performance. However, there is some degree of image distortion (spatial errors) due to a number of causes. This research activity is devoted to assess the different contributions of spatial errors, with two objectives in mind: • SMOS Improved performance • SMOS follow-on specifications The RSC method is devoted to assess the peformance of phase calibration. For calibration purposes, the phase calibration term (antenna plane) is modeled as: φkj = (φkant − φ jant ) + (φkrec − φ jrec ) + φkj A FWF Antenna phase terms Receiver phases Fringe-wash term IGARSS 2011 Vancouver 4
  • 5. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory SMOS phase calibration strategy • Receiver phase drift is calibrated by periodic (2-10 min) correlated noise injection (LO phase track) • Antenna phase term (manufacturing tolerances): Measured on ground • Fringe washing term due to filter response differences (negligible) Antenna Receiver plane φkant plane φkrec Antenna phase test set-up A L receiver " k " η C M kj Noise injection Correlator Switch Front end phase model receiver " j " IGARSS 2011 Vancouver 5
  • 6. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Redundant Space Calibration (RSC) Redundant baselines measure the same visibility using a different pair of antennas Redundant baselines Visibility phase measured by a baseline: φVkj = φk − φj + φscene,kj RSC phase differences are independent of the phase of the scene Baseline phase differences: φVkj − φVji =k − 2φj + φi φ IGARSS 2011 Vancouver 6
  • 7. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC system of equations A system of equations can be built using independent RSC equations 0 0 1 −2 1 0 … … 0    0 0 0 1 −2 1 0 … 0  Applied on calibrated … … … … … … … … …  visibilities the RSC   method retrieves the 0 … … … … 0 1 −2 1 ·φreceivers = φphase differences …  residual phase error … −1 1 … −1 1 .. …   … −1 … 1 … … 1 −1 …  … … … … … … … … …    A matrix: 66 x 69 Underdetermined system Receivers vector: 69 x 1 (three unknown phases, rank = 66) Phase differences vector: 66 x 1 Moore-Penrose pseudoinverse matrix 66 equations, 69 unknowns Averaging is required to reduce uncertainty due to thermal noise IGARSS 2011 Vancouver 7
  • 8. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Averaging: visibility measurements must be carefully selected • Low visibility amplitude: produces unwanted variations and jumps • Fast scene changes: phase bias in land-ocean transitions • RFI: interferences that spoils the phase values Land-ocean transition Low visibility amplitude RFI IGARSS 2011 Vancouver 8
  • 9. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC: examples of good quality visibility samples Averaging area Averaging area Averaging area Arm A Arm B Arm C Red line: Average snap-shots IGARSS 2011 Vancouver 9
  • 10. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC: Impact of undetermination The 3 unknown phases have a physical meaning: Tilt angle Steering angle Pointing error Common path delay Irrelevant IGARSS 2011 Vancouver 10
  • 11. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC: Pointing error in the phase retrievals Simulations show that a pointing error yields a linear phase error directly related to the antenna position in the arms. φerror,bslN = a·u bslN + b·v bslN  a b  TBcalibrated (ξ, η) = TBideal  ξ − ,η−   2π 2π  a ξps ' = ξps − 2π b ηps ' = ps − η 2π Retrieval error linear in each arm The pointing error can be corrected, if required, using a point source (e.g, an interference at a known position ξps , ηps) IGARSS 2011 Vancouver 11
  • 12. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Assessment on the pointing error in RSC retrievals Simulation: SMOS point source retrieval by the RSC method: random phase error Ideal Phase corrupted Corrected •Image blurring (example, σphases = 25º) • Secondary lobes increase • Small pointing error: the maximum has been displaced. Once the point source is RSC calibrated, image blurring and secondary lobes are corrected. However, the pointing error is not compensated. 12 IGARSS 2011 Vancouver
  • 13. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC implementation (i): Good/bad estimations Due to pointing error, the difference between two phase retrievals must be linear. This property is used to discard bad estimations of the RSC phases φretrieved = φIVT,error + φpoint ing error 1 1 φretrieved = φIVT,error + φpoint ing error 2 2 φretrieved − φretrieved = φpoint ing error − φpoint ing error 2 1 2 1 Linear Bad estimations Good estimations IGARSS 2011 Vancouver 13
  • 14. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC retrieved phases Final RSC phases retrieved by averaging RSC phases from 38 orbits over the ocean Horizontal Phases Vertical Phases RSC Phase Error dispersion σH =5.97º σV =3.17º • RSC gives a conservative Horizontal Mean Phases Vertical Mean Phases upper bound for SMOS residual phase errors • RSC phase dispersion very much contributed by pointing error IGARSS 2011 Vancouver 14
  • 15. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC: phase error impact of pointing error Mean pointing error (H) Horizontal Phases Simulation r SMOS std <r> Horizontal Std σphases (°) Simulation: point source shift for 200 cases with σph=20º. 95% of points within a radius σH =5.97º σV =3.17º r=2mrayleigh centred at the point source real position rH = 0.00066 rV = 0.00037 ∆L H = km 0.76 ∆L V = km 0.43 ΔLH and ΔLV below 2% of SMOS resolution (42 km) IGARSS 2011 Vancouver 15
  • 16. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC peformance assesssment: RFI in the Caribbean Sea Interference from a vessel (11/02/2010, 21:23 semi-orbit) IGARSS 2011 Vancouver 16
  • 17. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC peformance assesssment: RFI in the Caribbean Sea Horizontal IGARSS 2011 Vancouver 17
  • 18. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC peformance assessment: RFI in the Caribbean Sea – Primary to Secondary Lobe Ratio (H): Case Primary to Secondary Lobe Ratio Real Point Source 17,40 dB Corrected Point Source 16,50 dB – Primary to Secondary Lobe Ratio (V): Case Primary to Secondary Lobe Ratio Real Point Source 17,40 dB Corrected Point Source 16,65 dB – The uncorrected RFI presents a main-to-secondary lobe ratio very close to an ideal point source. – The RSC method uncertainty above SMOS phase error accuracy!! 18
  • 19. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory RSC implementation: Interference in Cáceres (Spain) Vertical 19
  • 20. •Remote Remote Sensing Laboratory •Sensing Universitat Politècnica de Catalunya •Laboratory Conclusions • The RSC method cannot be used to phase calibrate SMOS in a per snap shot basis due to the need for long averaging and filtering • SMOS orbital phase drift requires periodic (2-10 min) correlated noise injection (LO phase track) • The RSC is used to validate the consistency of SMOS phase calibrated visibilities: •RSC phase retrieval accuracy limited by undetermination (pointing error) •SMOS phase errors well below σH=5.97 º and σV=3.17º, probably very close to the σ =1º target •Assessment on point sources (RFI) shows that the impact of SMOS residual phase errors on image distortion is probably negligible IGARSS 2011 Vancouver 20