ers - envisat symposium gothenburg 16-20 october, 2000 gomos gomos calibration and processor...
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ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
GOMOS Calibration and Processor Verification
• Instrument Principle
• Calibration• Instrument and Engineering Data Checkout
• Instrument Calibration
• Processor Verification• Level 1b/2 processing verification & tuning
• Mission Planning• Verification of Mission Plan and Calibration Plan
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Instrument Measurement Principle
60 Km
40 Km
20 Km
F(z)
Fo
z
Wavelength
Inte
nsity
Wavelength
Inte
nsity
Fo
Wavelength
Inte
nsity
F(zi)F(z1)F(zi)
Wavelength
Tra
nsm
iss
ion
FoT(zi) =
Independent of gain drift
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Instrument Measurement Principle
As far as the star spectrum is concerned, GOMOS is a slit-less spectrometer, meaning that a movement of the point-like star target results in a spectral and spatial shift on the focal plane.To characterise such movements, the instrument star-tracker continuously samples the star image position. This information is then used in the ground processing to accurately align the individual spectra.
Slit/Baffle
Star Tracker Image
x
y
200 400
2
Time [msec]
Dep
oint
ing
[ra
d]
100 300
Wavelength
Inte
nsity
Facilitates Depointing/Spectral Correction
Tracking Data
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
SODAP
Signal level and band setting
Tracking capability
Performance evaluationCALEX Verification
First in-flight calibrationSecond in-flight calibration and Trend Analyis
Definition of routine calibration opeations
Schedule and obs plan for in-flight calibration
Launch
L+ 3.5 month = Instrument Calibrated
Level 1b Processing chain verification (prototype)
Level 1b Processing Tuning (prototype)
Level 1b Processing Tuning (PDS)
Level 1b chain Update (PDS)
Level 1b product coherency
Val of geoloc & atm prods
L1b
Pro
cess
or v
erif
icat
ion C
alib
rati
on
Oct Nov Dec Jan Feb Mar Apr May June
Hea
lth
chec
k
Schedule - Calibration & Processing Verification
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
On-Ground Processing
Datation
Geolocation
Wavelength Assignment
Covariance Processing
Sample corrections
Transmission Processing
Background Processing
Background Removal
Transmission spectra
Spectral Inversion
Smoothing
Vertical Inversion
Cross SectionComputation
Level 2 Products
Level 1b Processing Level 2 Processing
Cal
ibra
tion
Inp
uts
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Calibration NeedsMain parameters to be re-characterised during the commissioning phase:
Correction functions Parameter (for in-orbit calibration) Comment / required accuracyBad pixel processing Dark Signal Non-Uniformity Median filterCosmic ray processing Threshold value Median filterDigital to electron conversion Sensitivity [LSB / radiometric unit] Monitoring of drift
Non-linearity < 0.1 %Electronic chain offset < 1 %
Dark Charge Removal Dark Signal Non-Uniformity < 1%Mirror reflectivity correction SFM Reflectivity Calibrated on-ground; 0.05%/degStar background estimation Pixel-Response Non-Uniformity < 1 %
IR Vignetting < 5%Slit transmission
Star signal estimation Pixel-Response Non-Uniformity < 1 %IR Vignetting < 5 %
Wavelength Assignment Wavelength Assignement 1/3 pixelDispersion [nm/column]
Level 2 processing Line Spread Function 5 %
Only a very limited number of parameters are expected to change (red) and thus requires recalibration
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Instrument Calibration Support Modes
Besides the normal occultation mode, GOMOS has four other operation modes useful for calibration purposes. All modes will be fully exploited for calibration.
SATU= Star Acquisition and Tracking Unit
• The linearity mode is the same as the occultation mode except that the integration time can be programmed from 0.25 to 10 second in steps of 0.25 second.
• The uniformity mode produces pixel images of both spectrometer, photometer and SATU1 sensors. In this mode the instrument operates in open loop (no active tracking of stars, only orbit compensation).
• The Spatial Spread Mode produces, as in uniformity mode, pixel images of spectrometers, photometers and SATU’s. The difference is that the mode operates in closed loop with the tracking chain and hence needs a star target to track..
• The Fictive Star Mode is similar to the occultation mode (same data format) except that there is no active tracking (the star is specified with a specific position and speed)
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Calibration Preparation
The following resources and tools are prepared, to support the GOMOS commissioning activity:
PDS = Payload Data Segment (geophysical processor in ESRIN)
CALEX - GOMOS Calibration Processor. This software is installed and operated within the Instrument Engineering Calibration Processor. The main product is the GOMOS calibration database; used as input to the GOMOS geophysical product processor.
GOSS - GOMOS system simulator. Includes atmospheric and instrument model to generate real GOMOS source packet products (measurement data).
GOPR - GOMOS level 1b (calibration and transmission spectra processing) and level-2 (geophysical processing) prototype. This processor generates exactly the same products as the PDS one and is used as reference processor.
STARSEL - GOMOS star observation mission tool.
Various other analysis tools (specific tools, Excel and IDL routines etc..)
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Level 1b verification and validation
• Level 1b processing chain verification (step by step) : implementation of
calibration and characterisation parameters.• Verification of data coherency (range) : Check the range of each level 1b product
items. Analyse the self coherency of GOMOS products (e.g. level 2 products from
same geolocation but observed with two different stars)• Validation of stellar derived products : Analyse the stellar spectra products and
create a stellar spectra database• Data flagging monitoring and statistics : Monitor the data flagging of level 1b and
limb products (quality flags)• Recommendations for routine observation plan : Provide inputs to the observation
plan derived from level 1b product analysis• Update of level 1b processor
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
• Level 2 processing chain verification (step by step) : Check functionality of the
level 2 processing chain using real measurements • Coherency with model - climatology verification : Verification of the coherency
using forward models (real star spectra, climatology models) • Tuning of Level 2 processing parameters : analyse and validate the level 2
products tuning of the parameters of the level 2 processing chain to identify the new
initial operational configuration (iterative tuning).• Tuning of the Level 2 processor : modify, adjust the algorithms of the level 2
processing chain as appropriate.• Upgrade of the level 2 operational processor : implementation of the level 2
processing chain updates into the PDS operational chain.
Level 2 Processing Verification
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
IECFInstrument Engineering
Calibration Facility
GOMOS Commissioning
Centre
FOSFlight Operation
Segment
PDSProcessing
Data Segment
RGTReference Operation Plan Generation Tool
NILUNorwegian Institute
for Air Research
AO GroupsExternal Scientific
Studies
Processor update
Data / Processing Config
Observation planningProducts
Observation commanding
SODAPSwitch-On & Data
Acquisition Phase Group
Supporting Facilities and Interfaces
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
Spectral Line Spread Function (LSF)
The GOMOS Level-2 algorithm basically consist of correlating a measured spectrum by a synthesised one; generated from the cross sections.
A condition for this correlation is that the two spectra has the same resolution. As the instrument sets the limit, the synthesized one must first be convoluted with the instrument spectral LSF.
The instrument LSF will be assessed in-orbit by observing narrow stellar lines (preferrably emission lines).
The on-ground measurement is not expected to have changed (major contributing effects are defocus) and will be used.
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
SDE
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS
ERS - ENVISAT SYMPOSIUMGothenburg 16-20 October, 2000
GOMOS