1 st post launch SCIAMACHY calibration & Verification Meeting L1b Astrium Friedrichshafen –...
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Transcript of 1 st post launch SCIAMACHY calibration & Verification Meeting L1b Astrium Friedrichshafen –...
1st post launchSCIAMACHY calibration & Verification
MeetingL1b
Astrium Friedrichshafen – Germany24 July 2002
First Level 1b Spectral Calibration analysis
2
Level 1b Spectral Calibration analysis: content
The Spectral Calibration philosophy The Iecf Spectral Calibration Algorithm Related Verification Tasks: orbit behaviour Analysis specifics First results Other Spectral Calibration Verification Tasks Recommendations
3
The Spectral Calibration Philosophy
Objective: to assign a wavelength to each individual SCIA detector pixel during the flight.
Method: the relation between pixel index and wavelength is described by a 4th order polynomial:
To derive a set of calibration coefficients two calibration sources, the SLS and the sun, are analysed.
Stability: due to ageing of the instrument, the wavelength parameters needs to be updated on a regular basis. Iecf, Instrument Engineering and Calibration Facility, guarantees long term stability of scientific measurements.
44
33
2210 iiiii papapapaa
4
The Iecf Spectral Calibration Algorithm
Task: to determine coefficients of the 4th order polynomial for each channel as function of the orbital regions.
Input: Level 1b Newly Calculated Spectral ADS
Method: for each polynomial coefficient, given by the Spectral ADS as a function of orbital phase, a harmonic fit has to be performed in order to parameterise the orbital dependence.
The coefficients values are then computedfor a set of 12 fixed orbital phases:
)_( ORSPcoeff
i ii iicoeffcoeff 2cos2sin)( 0
5
Related verification Task: orbit behaviour
L1.01.02: Number of orbital regions for spectral calibration
L1.09.03: Orbit region dependency
Due to the instrument’s thermal environment along the orbit, the spectral calibration can be expected to show orbital dependency. Therefore SLS measurements shall be executed along the entire orbit to investigate whether the number of measurements and the number of orbital regions are sufficient and the orbit phase boundaries are chosen properly.
6
Analysis specifics and overview
Level 1b product: SCI_NL__0PNPDK20020621_182502_000062172007_00056_01613_0129.N1
Orbits: 1613States: 10 SLS States (predefined State_ID 59), on 87 total States
Channel 1: variation long the orbit is close or less to 1/100 of a pixel
Channel 2: not analysed due to erroneous key-data set used by the Level 0 to 1b processor
Channels 3, 4, 5 and 6: variation long the orbit is close or less to 1/100 of a pixel
Channel 7 and 8: not analysed for no in-flight dark current correction of the the raw lamp spectrum
First Results: Orbit dependency for Channel 1
The algorithm performs correctly the harmonic fit of the coefficients.
… but is this the best approach to the Spectral Calibration?
-3.20E-05
-3.00E-05
-2.80E-05
-2.60E-05
-2.40E-05
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
Coeff
a1 [nm
]
ADS GADS
1.10E-10
1.20E-10
1.30E-10
1.40E-10
1.50E-10
1.60E-10
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
Coeff
a3 [nm
]
ADS GADS
5.00E-08
6.00E-08
7.00E-08
8.00E-08
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
Coeff
a2 [nm
]
ADS GADS
-1.46E-13
-1.44E-13
-1.42E-13
-1.40E-13
-1.38E-13
-1.36E-13
-1.34E-13
-1.32E-13
-1.30E-13
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
Coeff
a4 [nm
]
ADS GADS
Spectral Calibration - Channel 1
1.8E-02
1.9E-02
2.0E-02
2.1E-02
2.2E-02
2.3E-02
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
Coeff
a0 [nm
]ADS GADS
First Results: Orbit dependency for Channel 3
The algorithm performs correctly the harmonic fit of the coefficients.
… but is this the best approach to the Spectral Calibration?
Spectral Calibration - Channel 3
6.00E-02
6.04E-02
6.08E-02
6.12E-02
6.16E-02
6.20E-02
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a0 [nm
]ADS GADS
0.00E+00
1.00E-05
2.00E-05
3.00E-05
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a1 [nm
]
ADS GADS-5.50E-07
-5.10E-07
-4.70E-07
-4.30E-07
-3.90E-07
-3.50E-07
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a2 [nm
]
ADS GADS
1.00E-09
1.10E-09
1.20E-09
1.30E-09
1.40E-09
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a3 [nm
]
ADS GADS
-9.00E-13
-8.50E-13
-8.00E-13
-7.50E-13
-7.00E-13
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a4 [nm
]
ADS GADS
First Results: Orbit dependency for Channel 4
The algorithm performs correctly the harmonic fit of the coefficients.
… but is this the best approach to the Spectral Calibration?
Spectral Calibration - Channel 4
2.00E-02
2.20E-02
2.40E-02
2.60E-02
2.80E-02
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a0 [nm
]
ADS GADS
2.60E-04
2.70E-04
2.80E-04
2.90E-04
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a1 [nm
]
ADS GADS-1.60E-06
-1.58E-06
-1.56E-06
-1.54E-06
-1.52E-06
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a2 [nm
]
ADS GADS
2.67E-09
2.69E-09
2.71E-09
2.73E-09
2.75E-09
2.77E-09
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a3 [nm
]
ADS GADS
-1.42E-12
-1.41E-12
-1.40E-12
-1.39E-12
-1.38E-12
-1.37E-12
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a4 [nm
]
ADS GADS
First Results: Orbit dependency for Channel 5
The algorithm performs correctly the harmonic fit of the coefficients.
… but is this the best approach to the Spectral Calibration?
Spectral Calibration - Channel 5
1.65E-01
1.66E-01
1.67E-01
1.68E-01
1.69E-01
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a0 [nm
]
ADS GADS
1.50E-05
3.50E-05
5.50E-05
7.50E-05
9.50E-05
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a1 [nm
]
ADS GADS-1.38E-06
-1.34E-06
-1.30E-06
-1.26E-06
-1.22E-06
-1.18E-06
-1.14E-06
-1.10E-06
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a2 [nm
]
ADS GADS
2.10E-09
2.15E-09
2.20E-09
2.25E-09
2.30E-09
2.35E-09
2.40E-09
2.45E-09
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a3 [nm
]
ADS GADS
-1.30E-12
-1.25E-12
-1.20E-12
-1.15E-12
-1.10E-12
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a4 [nm
]
ADS GADS
First Results: Orbit dependency for Channel 6
The algorithm performs correctly the harmonic fit of the coefficients.
… but is this the best approach to the Spectral Calibration?
Spectral Calibration - Channel 6
1.20E-01
1.30E-01
1.40E-01
1.50E-01
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a0 [nm
]
ADS GADS
5.80E-05
7.80E-05
9.80E-05
1.18E-04
1.38E-04
1.58E-04
1.78E-04
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a1 [nm
]
ADS GADS-2.00E-06
-1.90E-06
-1.80E-06
-1.70E-06
-1.60E-06
-1.50E-06
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a2 [nm
]
ADS GADS
2.40E-09
2.50E-09
2.60E-09
2.70E-09
2.80E-09
2.90E-09
3.00E-09
3.10E-09
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a3 [nm
]
ADS GADS
-1.35E-12
-1.30E-12
-1.25E-12
-1.20E-12
-1.15E-12
-1.10E-12
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Orbit phase
a4 [nm
]
ADS GADS
First Analysis: the harmonic fit approach for Channel 1
Orbit 1613
Maximum variation long the orbit: 1.1509E-03 nm or 0.01 of a pixel
-8.0E-04
-4.0E-04
0.0E+00
4.0E-04
8.0E-04
1.2E-03
1.6E-03
0 128 256 384 512 640 768 896 1024
Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 2 Rec 6 Rec 7 Rec 8 Rec 9 Rec 10 Rec 11 Rec 12
Channel 1: Pixel 950
-0.003
-0.0025
-0.002
-0.0015
-0.001
-0.0005
0
0.0005
0.001
0.0015
0.002
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
Channel 1: Pixel 325
-0.003
-0.0025
-0.002
-0.0015
-0.001
-0.0005
0
0.0005
0.001
0.0015
0.002
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
First Analysis: the harmonic fit approach for Channel 3
Orbit 1613
Maximum variation long the orbit: 2.1606E-02 nm or 0.090 of a pixel
-2.4E-02
-1.6E-02
-8.0E-03
0.0E+00
8.0E-03
1.6E-02
2.4E-02
0 128 256 384 512 640 768 896 1024
Pixel ID
Diff
eren
ce in W
vlen
[nm
]
Rec 2 Rec 6 Rec 7 Rec 8 Rec 9 Rec 10 Rec 11 Rec 12
Channel 3: pixel 950
-0.035
-0.03
-0.025
-0.02
-0.015
-0.01
-0.005
0
0.005
0.01
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
Channel 3: pixel 300
-0.035
-0.03
-0.025
-0.02
-0.015
-0.01
-0.005
0
0.005
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
First Analysis: the harmonic fit approach for Channel 4
Orbit 1613
Maximum variation long the orbit: 1.5229E-03 nm or 0.007 of a pixel
-2.0E-03
-1.6E-03
-1.2E-03
-8.0E-04
-4.0E-04
0.0E+00
4.0E-04
8.0E-04
1.2E-03
1.6E-03
0 128 256 384 512 640 768 896 1024Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 2 Rec 6 Rec 7 Rec 8 Rec 9 Rec 10 Rec 11 Rec 12
Channel 4: pixel 950
-0.003
-0.002
-0.001
0
0.001
0.002
0.003
0.004
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
Channel 4: pixel 340
-0.003
-0.002
-0.001
0
0.001
0.002
0.003
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
First Analysis: the harmonic fit approach for Channel 5
Orbit 1613
Maximum variation long the orbit: 2.0408E-02 nm or 0.07 of a pixel
-1.6E-02-1.2E-02-8.0E-03-4.0E-030.0E+004.0E-038.0E-031.2E-021.6E-022.0E-022.4E-02
0 128 256 384 512 640 768 896 1024Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 2 Rec 6 Rec 7 Rec 8 Rec 9 Rec 10 Rec 11 Rec 12
Channel 5: pixel 950
-0.015
-0.01
-0.005
0
0.005
0.01
0.015
0.02
0.025
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
Channel 5: pixel 340
-0.015
-0.01
-0.005
0
0.005
0.01
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
First Analysis: the harmonic fit approach for Channel 6
Orbit 1613
Maximum variation long the orbit: 3.2390E-02nm or 0.041 of a pixel
-2.0E-02
-1.0E-02
0.0E+00
1.0E-02
2.0E-02
3.0E-02
4.0E-02
0 128 256 384 512 640 768 896 1024Pixel ID
Diff
eren
ce in W
vlen
[nm
]
Rec 2 Rec 6 Rec 7 Rec 8 Rec 9 Rec 10 Rec 11 Rec 12
Channel 6: pixel 950
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
Channel 6: pixel 330
-0.03
-0.025
-0.02
-0.015
-0.01
-0.005
0
0.005
0.01
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
Orbit Phase
Diff
eren
ce in
Wvl
en [n
m]
First analysis: variation on the input for Channel 1
Coefficient average long the orbit as reference
Maximum variation long the orbit from average: 1.5786E-03 nm or 0.013 of a pixel
-1.50E-03
-1.00E-03
-5.00E-04
0.00E+00
5.00E-04
1.00E-03
1.50E-03
2.00E-03
0 128 256 384 512 640 768 896 1024Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 1 Rec 2 Rec 3 Rec 4 Rec 5 Rec 6 Rec 7 Rec 8
Maximum variation long the orbit from fit: 1.1509E-03 nm or 0.01 of a pixel
First analysis: variation on the input for Channel 3
Coefficient average long the orbit as reference
-3.00E-03
-2.00E-03
-1.00E-03
0.00E+00
1.00E-03
2.00E-03
3.00E-03
0 128 256 384 512 640 768 896 1024Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 1 Rec 2 Rec 3 Rec 4 Rec 5 Rec 6 Rec 7 Rec 8
Maximum variation long the orbit from average: 2.2911E-03 nm or 0.010 of a pixel
Maximum variation long the orbit from fit: 2.1606E-02 nm or 0.090 of a pixel
First analysis: variation on the input for Channel 4
Coefficient average long the orbit as reference
Maximum variation long the orbit from average: 1.8100E-03 nm or 0.008 of a pixel
Maximum variation long the orbit from fit: 1.5229E-03 nm or 0.007 of a pixel
-2.00E-03
-1.50E-03
-1.00E-03
-5.00E-04
0.00E+00
5.00E-04
1.00E-03
1.50E-03
2.00E-03
0 128 256 384 512 640 768 896 1024
Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 1 Rec 2 Rec 3 Rec 4 Rec 5 Rec 6 Rec 7 Rec 8
First analysis: variation on the input for Channel 5
Coefficient average long the orbit as reference
Maximum variation long the orbit from average: 3.2879E-03 nm or 0.012 of a pixel
Maximum variation long the orbit: 2.0408E-02 nm or 0.07 of a pixel
-0.0040
-0.0030
-0.0020
-0.0010
0.0000
0.0010
0.0020
0.0030
0 128 256 384 512 640 768 896 1024
Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 1 Rec 2 Rec 3 Rec 4 Rec 5 Rec 6 Rec 7 Rec 8
First analysis: variation on the input for Channel 6
Coefficient average long the orbit as reference
Maximum variation long the orbit from average: 4.2989E-03 nm or 0.006 of a pixel
Maximum variation long the orbit: 3.2390E-02nm or 0.041 of a pixel
-6.00E-03
-4.00E-03
-2.00E-03
0.00E+00
2.00E-03
4.00E-03
6.00E-03
0 128 256 384 512 640 768 896 1024
Pixel ID
Diff
eren
ce in
Wvl
en [n
m]
Rec 1 Rec 2 Rec 3 Rec 4 Rec 5 Rec 6 Rec 7 Rec 8
22
First Analysis: Summary
Level 1b: variation long the
orbit [nm]
Iecf output: variation long
the orbit [nm] Minumum variation
Ch 1 1.5786E-03 1.1509E-03 Iecf output
Ch 3 -2.7120E-03 -2.1606E-02 Average Level 1b
Ch 4 1.8100E-03 -1.5229E-03 Iecf output
Ch 5 -3.2879E-03 2.0408E-02 Average Level 1b
Ch 6 -4.9289E-03 3.2390E-02 Average Level 1b
Reference average coeffs
Level 1b: variation long the
orbit [pixel]
Iecf output: variation long
the orbit [pixel] Pixel spacing
Ch 1 0.0133 0.0097 1.1901E-01
Ch 3 0.0113 0.0904 2.3902E-01
Ch 4 0.0085 0.0072 2.1192E-01
Ch 5 0.0116 0.0722 2.8276E-01
Ch 6 0.0063 0.0414 7.8224E-01
Reference average coeffs Ref. corresponding Level 1b
Ref. corresponding Level 1b
23
All Spectral Cal Related Verification Tasks
L1.01.02 Number of orbital regions for spectral calibration
• L1.02.03 Wavelength calibration - selected line list not changes
• L1.02.04 Slit function parameters unchanged
• L1.09.01 Verification of precise basis for spectral calibration
• L1.09.02 Verification of selected lines for calibration L1.09.03 Verify orbit region dependency
• L1.09.04 Verify whether SLS or Fraunhofer calibration shall be the baseline
L1.14.01: Wavelength calibration differences monitoring
24
Level 1b Spectral Calibration analysis: Recommendations
The approach averaging the coefficients from the Level 1b seems to give better results
Fit based on a lower order polynomial shall be investigated …