SlideShare ist ein Scribd-Unternehmen logo
1 von 30
Rita Castro 1 , Antonio Gutiérrez 1 , José Barbosa 1 ,  Nuno Catarino 1 , Sofia Freitas 1 , Bruno Lucas 1 , Henrique Candeias 1 ,  José Freitas 2 , Marco Ventura 2 , Michele Zundo 3 1 DEIMOS Engenharia, Portugal 2 Critical Software 3 ESA/ESTEC, Noordwijk, Netherlands SMOS L1 Algorithms
L1PP Overview
L1PP Overview ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
L1PP processed the first data available at ESAC on 17-Dec-2009
L1PP continued processing data with all calibration parameters, as soon as they became available (March 2010 data)
Level   1a Processing
First Calibrated Images ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Calibration Remarks Important algorithms and corrections have been validated using L1PP and are now included in L1OP PMS Linearity Correction   Correction on the the PMS voltages using the deflection parameter ( C ) Visibilities Offsets Correction Can be applied to all baselines or only to baselines covered by a common Local Oscillator Differences between Using the C-parameter or not performing any 2nd order correction. Final decision is to apply Deflection Method. Differences between both applications can go up to 2K. Final decision is to apply correction only to baselines sharing LO.
Calibration Remarks Local Oscillator Offset Calibration The correction in phase is crucial to retrieve properly the features of the targets observed The sampling of Local Oscillator phase  must be carried out optimally in order to provide high quality data while reducing the number of measurement losses due to the calibration activities L1PP has an algorithm to decimate the LO Calibration and study the influence of different LO calibration intervals Results obtained by decimating data with 2 mins. frequency Credits: R.Oliva, “Local Oscillator Decimation Study”  A trade-off of  10 minutes  sampling period was made between SOIL MOISTURE and OCEAN SALINITY teams
Level   1b Processing
Foreign Sources Removal ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Applying this algorithm on a Sky target allows: a) Assess on the quality of one Auxiliary File for SMOS – the Galaxy Map b) Assess on the Instrument Accuracy Sky image for 02-Mar-2010 Without Sky Removal (H-pol) <Tb> = 4.59±2.09 K in the Hexagon Remove Correct With Sky Removal (H-pol) <Tb> = 0.27±1.04 K in the Hexagon
Sun Direct Algorithm ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Based on Camps et al.,  Sun Effects In 2D Aperture Synthesis Radiometry Imaging And Their Cancellation  (2004)
Flat Target Transformation ,[object Object],[object Object],[object Object],[object Object],After applying the FTT on the Sky Image of 23-Dec-2009, the Galaxy is observed, as well as other features... Without applying the FTT <Tb> = 3.43±8.25 K in the Hexagon <Tb> = 7.66±7.03 K in the AF-FOV Applying the FTT <Tb> = 3.43±0.97 K in the Hexagon <Tb> = 3.52±0.51 K in the AF-FOV Moon Position Sun Alias Radio Source ξ ξ
Instrument Accuracy  & Radiometric Sensitivity
Instrument Accuracy Defining  Accuracy   as  and using L1PP v3.3.0 and the Sky Removal algorithm, the Accuracy of MIRAS has been estimated for both polarimetric modes SO-TN-DME-L1PP-0237 ,[object Object],[object Object],Two FTRs: 1) Sky Image (19-Jan-2010);  2) FTTs (21-Jan-2010) Pol. Accuracy Hexagon AF-FOV Circle r = 0.3 Circle r = 0.2 H 0.580 0.335 0.337 0.298 V 0.694 0.273 0.279 0.276 H 0.749 0.328 0.316 0.291 V 0.777 0.286 0.291 0.285 Re(HV) 0.435 0.319 0.312 0.285 Im(HV) 0.367 0.256 0.251 0.222
Radiometric Sensitivity The Radiometric Sensitivity is defined as the  minimum detectable brightness temperature signal . It has been computed using data acquired by MIRAS, for all polarisations, in the two polarimetric modes Time Averaged Scene ,[object Object],[object Object],[object Object],Radiometric Sensitivity for 150 Scenes in  Dual Polarisation  (H-pol) Radiometric Sensitivity for 150 Scenes in  Full Polarisation  (H-pol) Pol. Radiometric Sensitivity Average  Hexagon AF-FOV Circle r = 0.3 H 1.474 2.257 1.576 1.535 V 1.436 2.254 1.571 1.527 H 1.833 3.066 2.158 2.110 V 1.887 3.052 2.113 2.051 Re(HV) 1.926 2.977 2.087 2.037 Im(HV) 1.961 2.996 2.101 2.047
From Radiometric Sensitivity
Integration Times L1PP results revealed an error in the theoretical value for the integration time of Full Pol Scenes  It was expected that But using the average values for the Radiometric Sensitivity inside the Circle r = 0.3  These differences lead to the computation of  Empirical Integration Times ,  τ eff , for Mixed and HV Scenes of Full Pol. Mode After the correction of the theoretical integration time…. Theoretical Ratios Experimental Ratios  (Circle r = 0.3) 1.41 1.36 1.73 1.59
Instrument Stability ,[object Object],[object Object],Differences  between polarisations range  0.08 K Analyzing the seven FTRs in Full Polarisation mode acquired during the Commissioning Phase… The Radiometric Sensitivity is a good parameter to characterize the Stability of MIRAS
Baseline Weights Algorithm
Processing Steps Generate Baseline Weights ADF Weights on the J+ matrix must be the same as the ones applied to the visibilities to be reconstructed L1PP v3.4 used to process the same orbit with Sea-Weighted J +  Matrix and Nominal J +  Matrix 10-Mar-2010 Full Pol. Orbit with NIR & Long Calibration from 09-Feb-2010 Compute Radiometric Noise Levels for Mixed and LICEF-LICEF Baselines from Dual-Pol Scenes over 4 months of data over the Pacific Ocean Based on Anterrieu et al.,  Estimating and accounting for the covariance matrix of the MIRAS instrument onboard SMOS  (2009) Weighted J +  Matrix
Impact on Sensitivity H-pol On average, there is an improvement of ~0.24 K inside the Circle r = 0.3 No Weights [1] Sea Weights [2] Δ  ([2] – [1]) V-pol On average, there is an improvement of ~0.21 K inside the Circle r = 0.3
More on Instrument Stability The Instrument Stability can also be assessed using the ratio between between M- and L- Baselines,  Descending (Des) orbits show some variability wrt the Ascending (Asc) ones    L1OP was not stable at beggining of IOCP ,[object Object],[object Object]
Conclusions
Conclusions ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Future Work – Radio Frequency Interference (RFI)
RFI during Commissioning RFI has been a presence since the begining of the SMOS Commissioning Phase... Strong sources in the Iberian Peninsula were switched off by authorities during the Commissioning Phase Algorithms to mitigate the effect of RFIs are being developed by the scientists from the Experts Support Laboratories and will be tested in L1PP Probability Map for RFI – generated before March-2010 Credits: P. Richaume,  http://www.cesbio.ups-tlse.fr/SMOS_blog/   Images from March-2010 Credits: R. Oliva,  http://www.cesbio.ups-tlse.fr/SMOS_blog/
First Steps in RFI Mitigation Based on the Sun Direct removal algorithm, Deimos has prototyped a RFI Mitigation Technique, however, sources have different behaviours Original Snapshot RFI Corrected Snapshot ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
More results on RFI Detection and Mitigation techniques for SMOS have been presented in Session  WE3.L07 :  Frequency Allocation for Remote Sensing and RFI Mitigation for Microwave Radiometry Original Browse “ RFI Corrected“ Browse Images generated by R.Oliva with data processed by L1PP
Thank you for your kind attention [email_address] [email_address] [email_address] http://www.smos.com.pt/ L1PP Homepage http://www.deimos.com.pt/en/ Deimos Engenharia Homepage

Weitere ähnliche Inhalte

Was ist angesagt?

Accuracy improvement of gnss and real time kinematic using egyptian network a...
Accuracy improvement of gnss and real time kinematic using egyptian network a...Accuracy improvement of gnss and real time kinematic using egyptian network a...
Accuracy improvement of gnss and real time kinematic using egyptian network a...Alexander Decker
 
GPS cycle slips detection and repair through various signal combinations
GPS cycle slips detection and repair through various signal combinationsGPS cycle slips detection and repair through various signal combinations
GPS cycle slips detection and repair through various signal combinationsIJMER
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
Towards the identification of the primary particle nature by the radiodetecti...
Towards the identification of the primary particle nature by the radiodetecti...Towards the identification of the primary particle nature by the radiodetecti...
Towards the identification of the primary particle nature by the radiodetecti...Ahmed Ammar Rebai PhD
 
Assessment of the Accuracy of Processing GPS Static Baselines Up To 40 Km Us...
Assessment of the Accuracy of Processing GPS Static Baselines  Up To 40 Km Us...Assessment of the Accuracy of Processing GPS Static Baselines  Up To 40 Km Us...
Assessment of the Accuracy of Processing GPS Static Baselines Up To 40 Km Us...IJMER
 
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...umairali255
 
Gps ins odometer data fusion
Gps ins odometer data fusionGps ins odometer data fusion
Gps ins odometer data fusionRappy Saha
 
IGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxIGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxgrssieee
 
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...grssieee
 
FR4.T05.1.ppt
FR4.T05.1.pptFR4.T05.1.ppt
FR4.T05.1.pptgrssieee
 
Integral field spectroscopy
Integral field spectroscopyIntegral field spectroscopy
Integral field spectroscopyFernando Reche
 
IGARSS11_takaku_dsm_report.ppt
IGARSS11_takaku_dsm_report.pptIGARSS11_takaku_dsm_report.ppt
IGARSS11_takaku_dsm_report.pptgrssieee
 
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform Domain
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform DomainAtmospheric Correction of Remotely Sensed Images in Spatial and Transform Domain
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform DomainCSCJournals
 
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias Codes
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias CodesFast Sparse 2-D DFT Computation using Sparse-Graph Alias Codes
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias CodesFrank Ong
 
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BAND
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BANDTH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BAND
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BANDgrssieee
 
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATA
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATAFR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATA
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATAgrssieee
 

Was ist angesagt? (19)

Accuracy improvement of gnss and real time kinematic using egyptian network a...
Accuracy improvement of gnss and real time kinematic using egyptian network a...Accuracy improvement of gnss and real time kinematic using egyptian network a...
Accuracy improvement of gnss and real time kinematic using egyptian network a...
 
Gps2
Gps2Gps2
Gps2
 
GPS cycle slips detection and repair through various signal combinations
GPS cycle slips detection and repair through various signal combinationsGPS cycle slips detection and repair through various signal combinations
GPS cycle slips detection and repair through various signal combinations
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
Towards the identification of the primary particle nature by the radiodetecti...
Towards the identification of the primary particle nature by the radiodetecti...Towards the identification of the primary particle nature by the radiodetecti...
Towards the identification of the primary particle nature by the radiodetecti...
 
Assessment of the Accuracy of Processing GPS Static Baselines Up To 40 Km Us...
Assessment of the Accuracy of Processing GPS Static Baselines  Up To 40 Km Us...Assessment of the Accuracy of Processing GPS Static Baselines  Up To 40 Km Us...
Assessment of the Accuracy of Processing GPS Static Baselines Up To 40 Km Us...
 
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...
Novel Terrain Integrated Navigation System using Neural Network aided Kalman ...
 
The LEISA Atmospheric Corrector (LAC) on Earth Observer 1 (EO1)
The LEISA Atmospheric Corrector (LAC) on Earth Observer 1 (EO1)The LEISA Atmospheric Corrector (LAC) on Earth Observer 1 (EO1)
The LEISA Atmospheric Corrector (LAC) on Earth Observer 1 (EO1)
 
Gps ins odometer data fusion
Gps ins odometer data fusionGps ins odometer data fusion
Gps ins odometer data fusion
 
IGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxIGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptx
 
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...
TU2.L10 - ACCURATE MONITORING OF TERRESTRIAL AEROSOLS AND TOTAL SOLAR IRRADIA...
 
FR4.T05.1.ppt
FR4.T05.1.pptFR4.T05.1.ppt
FR4.T05.1.ppt
 
Integral field spectroscopy
Integral field spectroscopyIntegral field spectroscopy
Integral field spectroscopy
 
IGARSS11_takaku_dsm_report.ppt
IGARSS11_takaku_dsm_report.pptIGARSS11_takaku_dsm_report.ppt
IGARSS11_takaku_dsm_report.ppt
 
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform Domain
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform DomainAtmospheric Correction of Remotely Sensed Images in Spatial and Transform Domain
Atmospheric Correction of Remotely Sensed Images in Spatial and Transform Domain
 
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias Codes
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias CodesFast Sparse 2-D DFT Computation using Sparse-Graph Alias Codes
Fast Sparse 2-D DFT Computation using Sparse-Graph Alias Codes
 
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BAND
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BANDTH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BAND
TH1.L09 - ACCURATE FOCUSING OF SINGLE-PASS AIRBORNE INSAR DATA AT L-BAND
 
Presentation1
Presentation1Presentation1
Presentation1
 
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATA
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATAFR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATA
FR2.L09 - PROCESSING OF MEMPHIS MILLIMETER WAVE MULTI-BASELINE INSAR DATA
 

Ähnlich wie TH2.L10.4: SMOS L1 ALGORITHMS

Flight Dynamics Software Presentation Part I Version 5
Flight Dynamics Software Presentation Part I Version 5Flight Dynamics Software Presentation Part I Version 5
Flight Dynamics Software Presentation Part I Version 5Antonios Arkas
 
Precise Attitude Determination Using a Hexagonal GPS Platform
Precise Attitude Determination Using a Hexagonal GPS PlatformPrecise Attitude Determination Using a Hexagonal GPS Platform
Precise Attitude Determination Using a Hexagonal GPS PlatformCSCJournals
 
Characterisation of neutron meriaty
Characterisation of neutron  meriatyCharacterisation of neutron  meriaty
Characterisation of neutron meriatyLeishman Associates
 
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...Angelo State University
 
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...adrianocamps
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSjantjournal
 
Atmospheric Correction of Remote Sensing Data_RamaRao.pptx
Atmospheric Correction of Remote Sensing Data_RamaRao.pptxAtmospheric Correction of Remote Sensing Data_RamaRao.pptx
Atmospheric Correction of Remote Sensing Data_RamaRao.pptxssusercd49c0
 
IGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxIGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxgrssieee
 
INS/GPS Integrated Navigation Technology for Hypersonic UAV
INS/GPS Integrated Navigation Technology for Hypersonic UAVINS/GPS Integrated Navigation Technology for Hypersonic UAV
INS/GPS Integrated Navigation Technology for Hypersonic UAVNooria Sukmaningtyas
 
GPS Instrumental Biases Estimation Using Continuous Operating Receivers Network
GPS Instrumental Biases Estimation Using Continuous Operating Receivers NetworkGPS Instrumental Biases Estimation Using Continuous Operating Receivers Network
GPS Instrumental Biases Estimation Using Continuous Operating Receivers NetworkCSCJournals
 
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...Muhammad Ushaq
 
FR4.TO5.5.ppt
FR4.TO5.5.pptFR4.TO5.5.ppt
FR4.TO5.5.pptgrssieee
 
Environmentally Corrected RSSI Based Real Time Location Detection System
Environmentally Corrected RSSI Based Real Time Location Detection SystemEnvironmentally Corrected RSSI Based Real Time Location Detection System
Environmentally Corrected RSSI Based Real Time Location Detection SystemAIRCC Publishing Corporation
 
Ravasi_etal_EAGE2015b
Ravasi_etal_EAGE2015bRavasi_etal_EAGE2015b
Ravasi_etal_EAGE2015bMatteo Ravasi
 

Ähnlich wie TH2.L10.4: SMOS L1 ALGORITHMS (20)

Flight Dynamics Software Presentation Part I Version 5
Flight Dynamics Software Presentation Part I Version 5Flight Dynamics Software Presentation Part I Version 5
Flight Dynamics Software Presentation Part I Version 5
 
Basics of dip
Basics of dipBasics of dip
Basics of dip
 
Precise Attitude Determination Using a Hexagonal GPS Platform
Precise Attitude Determination Using a Hexagonal GPS PlatformPrecise Attitude Determination Using a Hexagonal GPS Platform
Precise Attitude Determination Using a Hexagonal GPS Platform
 
Characterisation of neutron meriaty
Characterisation of neutron  meriatyCharacterisation of neutron  meriaty
Characterisation of neutron meriaty
 
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...
Design and First Results of an UAV-Borne L-Band Radiometer for Multiple Monit...
 
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...
ESA SMOS (Soil Moisture and Ocean Salinity) Mission: Principles of Operation ...
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONSDUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
DUAL BAND GNSS ANTENNA PHASE CENTER CHARACTERIZATION FOR AUTOMOTIVE APPLICATIONS
 
Atmospheric Correction of Remote Sensing Data_RamaRao.pptx
Atmospheric Correction of Remote Sensing Data_RamaRao.pptxAtmospheric Correction of Remote Sensing Data_RamaRao.pptx
Atmospheric Correction of Remote Sensing Data_RamaRao.pptx
 
IGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptxIGARSS_2011_XB_v007.pptx
IGARSS_2011_XB_v007.pptx
 
INS/GPS Integrated Navigation Technology for Hypersonic UAV
INS/GPS Integrated Navigation Technology for Hypersonic UAVINS/GPS Integrated Navigation Technology for Hypersonic UAV
INS/GPS Integrated Navigation Technology for Hypersonic UAV
 
GPS Instrumental Biases Estimation Using Continuous Operating Receivers Network
GPS Instrumental Biases Estimation Using Continuous Operating Receivers NetworkGPS Instrumental Biases Estimation Using Continuous Operating Receivers Network
GPS Instrumental Biases Estimation Using Continuous Operating Receivers Network
 
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...
1-A Fault Tolerant Integrated Navigation Scheme Realized through Online Tunin...
 
FR4.TO5.5.ppt
FR4.TO5.5.pptFR4.TO5.5.ppt
FR4.TO5.5.ppt
 
Environmentally Corrected RSSI Based Real Time Location Detection System
Environmentally Corrected RSSI Based Real Time Location Detection SystemEnvironmentally Corrected RSSI Based Real Time Location Detection System
Environmentally Corrected RSSI Based Real Time Location Detection System
 
Ravasi_etal_EAGE2015b
Ravasi_etal_EAGE2015bRavasi_etal_EAGE2015b
Ravasi_etal_EAGE2015b
 

Mehr von grssieee

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
 
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
 
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
 
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
 
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
 

Mehr von grssieee (20)

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...
 
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
 
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...
 
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
 
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
 

TH2.L10.4: SMOS L1 ALGORITHMS

  • 1. Rita Castro 1 , Antonio Gutiérrez 1 , José Barbosa 1 , Nuno Catarino 1 , Sofia Freitas 1 , Bruno Lucas 1 , Henrique Candeias 1 , José Freitas 2 , Marco Ventura 2 , Michele Zundo 3 1 DEIMOS Engenharia, Portugal 2 Critical Software 3 ESA/ESTEC, Noordwijk, Netherlands SMOS L1 Algorithms
  • 3.
  • 4. L1PP processed the first data available at ESAC on 17-Dec-2009
  • 5. L1PP continued processing data with all calibration parameters, as soon as they became available (March 2010 data)
  • 6. Level 1a Processing
  • 7.
  • 8. Calibration Remarks Important algorithms and corrections have been validated using L1PP and are now included in L1OP PMS Linearity Correction Correction on the the PMS voltages using the deflection parameter ( C ) Visibilities Offsets Correction Can be applied to all baselines or only to baselines covered by a common Local Oscillator Differences between Using the C-parameter or not performing any 2nd order correction. Final decision is to apply Deflection Method. Differences between both applications can go up to 2K. Final decision is to apply correction only to baselines sharing LO.
  • 9. Calibration Remarks Local Oscillator Offset Calibration The correction in phase is crucial to retrieve properly the features of the targets observed The sampling of Local Oscillator phase must be carried out optimally in order to provide high quality data while reducing the number of measurement losses due to the calibration activities L1PP has an algorithm to decimate the LO Calibration and study the influence of different LO calibration intervals Results obtained by decimating data with 2 mins. frequency Credits: R.Oliva, “Local Oscillator Decimation Study” A trade-off of 10 minutes sampling period was made between SOIL MOISTURE and OCEAN SALINITY teams
  • 10. Level 1b Processing
  • 11.
  • 12.
  • 13.
  • 14. Instrument Accuracy & Radiometric Sensitivity
  • 15.
  • 16.
  • 18. Integration Times L1PP results revealed an error in the theoretical value for the integration time of Full Pol Scenes It was expected that But using the average values for the Radiometric Sensitivity inside the Circle r = 0.3  These differences lead to the computation of Empirical Integration Times , τ eff , for Mixed and HV Scenes of Full Pol. Mode After the correction of the theoretical integration time…. Theoretical Ratios Experimental Ratios (Circle r = 0.3) 1.41 1.36 1.73 1.59
  • 19.
  • 21. Processing Steps Generate Baseline Weights ADF Weights on the J+ matrix must be the same as the ones applied to the visibilities to be reconstructed L1PP v3.4 used to process the same orbit with Sea-Weighted J + Matrix and Nominal J + Matrix 10-Mar-2010 Full Pol. Orbit with NIR & Long Calibration from 09-Feb-2010 Compute Radiometric Noise Levels for Mixed and LICEF-LICEF Baselines from Dual-Pol Scenes over 4 months of data over the Pacific Ocean Based on Anterrieu et al., Estimating and accounting for the covariance matrix of the MIRAS instrument onboard SMOS (2009) Weighted J + Matrix
  • 22. Impact on Sensitivity H-pol On average, there is an improvement of ~0.24 K inside the Circle r = 0.3 No Weights [1] Sea Weights [2] Δ ([2] – [1]) V-pol On average, there is an improvement of ~0.21 K inside the Circle r = 0.3
  • 23.
  • 25.
  • 26. Future Work – Radio Frequency Interference (RFI)
  • 27. RFI during Commissioning RFI has been a presence since the begining of the SMOS Commissioning Phase... Strong sources in the Iberian Peninsula were switched off by authorities during the Commissioning Phase Algorithms to mitigate the effect of RFIs are being developed by the scientists from the Experts Support Laboratories and will be tested in L1PP Probability Map for RFI – generated before March-2010 Credits: P. Richaume, http://www.cesbio.ups-tlse.fr/SMOS_blog/ Images from March-2010 Credits: R. Oliva, http://www.cesbio.ups-tlse.fr/SMOS_blog/
  • 28.
  • 29. More results on RFI Detection and Mitigation techniques for SMOS have been presented in Session WE3.L07 : Frequency Allocation for Remote Sensing and RFI Mitigation for Microwave Radiometry Original Browse “ RFI Corrected“ Browse Images generated by R.Oliva with data processed by L1PP
  • 30. Thank you for your kind attention [email_address] [email_address] [email_address] http://www.smos.com.pt/ L1PP Homepage http://www.deimos.com.pt/en/ Deimos Engenharia Homepage