tes characterization for carbon cycle science ppt overview factors that affect co 2 source and sink...
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Characterization of Tropospheric Emission Spectrometer (TES) CO2for carbon cycle science
Susan Kulawik, Kevin Bowman, Dylan Jones, Ray Nassar, John Worden, F.W. Irion, Annmarie Eldering, and the TES team
Kevin Bowman – ASSFTS 14
Copyright YEAR California Institute of Technology. Government sponsorship acknowledged.
Talk overview
Factors that affect CO2 source and sink estimates
TES CO2 results and characterization
OSSE to estimate TES CO2 impact on source and sink estimates
Conclusions
Kevin Bowman – ASSFTS 14
Quality of CO2 source/sink estimates depends on:
Radiance
680 700 720 740 760
Frequency (cm-1)
456789
10
-6 W/cm
2/sr/cm
-1
-1
3
-0.2 0.0 0.2 0.4 0.6
0
10
20
30
40
50
Altitude (km)
100
10
DOFS 1.0
908 hPa511 hPa133 hPa10 hPa0.1 hPa
Retrieval Result for CO2
Volume Mixing Ratio [ppmv]
0
5
10
15
20
25
30
35
Altitude [km] Result
A priori
1000
100
10
Pressure [mb]
1122
)( −− −+− am SaS xxxFy
radiances radiative transfer assimilation and source / sinkretrieval algorithms modeling scheme estimates
• instrument characteristics• radiative transfer algorithm• retrieval algorithms• assimilation method• chemistry and transport model• atmospheric conditions (affects retrieval sensitivity)
Region BiosphTg c/yr
CombustTg c/yr
USA-48 205 5220
Alaska 160 75
Russia -1220 1800
Kevin Bowman – ASSFTS 14
Instrument characteristics- AIRS, IASI, GOSAT, and TES instruments at mid-infrared (700 cm-1):
Native resolution
S/N @native
S/N @ 0.5 cm-1
AIRS 0.5 cm-1 ~525 ~525*
IASI 0.5 cm-1 ~225 ~225**
GOSAT 0.2 cm-1 >300*** >475
TES 0.1 cm-1 ~80 ~200****
* http://airs.jpl.nasa.gov/technology/specifications/ with 0.35K @ 250K; 9 footprint ave** Crevoisier et al., 2009 0.22K error at 700 cm-1*** http://www.jaxa.jp/press/2009/02/20090209_ibuki_e.html, infrared band average**** Shephard et al., 2008 table 2, with 0.3K @250K at AIRS resolution
Kevin Bowman – ASSFTS 14
Retrieval approach- Based on the optimal estimation framework (Rodgers, 2000), temperature,
H2O, CO2, cloud and surface parameters are jointly retrieved
- Optimal estimation framework provides a characterization of CO2 estimates in terms of the accuracy, precision (Bowman, 2006; Worden, 2004):
• Joint temperature, H2O, CO2 retrievals– Minimizes temperature, water bias
• Choice of windows– Choose broad set of windows in ν2 and laser bands– Remove spectral areas that are not well fit
• Constraints based on altitude-dependent Tikhonov (Kulawik et al. 2006)– Use 6% variability near surface and 2% higher
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Kevin Bowman – ASSFTS 14
Radiance
680 700 720 740 760
Frequency (cm-1)
456789
10
-6 W/cm
2/sr/cm
-1
970 975 980 985 990
Frequency (cm-1)
5.86.06.26.46.66.8
10
-6 W/cm
2/sr/cm
-1
1070 1080 1090 1100 1110
Frequency (cm-1)
3.5
4.0
4.5
5.0
10
-6 W/cm
2/sr/cm
-1
Information at infrared wavelengthsradiances and Jacobians
680 700 720 740 760
0
5
10
15
20
Height (km) Jacobians
970 975 980 985 990
0
5
10
15
20
Height (km)
1070 1080 1090 1100 1110
0
5
10
15
20
Height (km)
Jacobians show the sensitivity of radiances to changes in CO2. This location shows the change in radiance at 715 cm-1
when CO2 at 5 km is changed
10
15
20
0.00
0.25
0.50
0.75
1.00
Sensitivity
----
ν2 band is mainly sensitive to CO2 in the middle Troposphere through the lower Stratosphere
Laser bands are sensitive to middle Troposphere and below
Jacobian[ν,z] = d(Radiance[ν]) / dln(CO2[z]) / radiance_noise[ν]
1070 1080 1090 1100 1110
Frequency (cm-1)
Kevin Bowman – ASSFTS 14
Change in TES calculated radiance when boundary layer values (0-2 km) or mid-Troposphere (4-8 km) are changed for optimal boundary layer viewing conditions (e.g. high thermal contrast):
We find that 1K temperature bias propagates into a 25 ppm CO2 bias
Errors in CO2 estimates strongly depend on the accuracy of temperature and water vapor
970 975 980 985 990
Frequency (cm-1)
0
1
2
3
4
dRadiance*1e-8
Radiance noise
970 975 980 985 990
Frequency (cm-1)
02
4
6
8
1012
dRadiance*1e-8
Radiance noise
Water +10%
Temp. -1K
CO2 +10 ppm
Boundary layer (0-2 km) changes Mid-trop. (4-8 km) changes
Kevin Bowman – ASSFTS 14
TES CO2 Errors
0 2 4 6 8 10 12
1000
100
10
Pressure (hPa) Prior
SmoothTempH2OCLOUDMeas. ErrorPred. Error
Typical TES single target errors
• Estimated TES single target error in the middle troposphere is ~8 ppm.
• Uncertainties in temperature and retrieval sensitivity (smoothing) are the dominant errors for CO2 estimates using the IR bands TES maximum
sensitivity
statecrossmeassmoothtotal −++= SSSS
Kevin Bowman – ASSFTS 14
Averaging targets
• Averaging more targets (over a larger spatial area) decreases error vs. Mauna Loa
• Progression agrees with 1/sqrt(N) reduction in error for averages
S. Kulawik – March, 2009
CO2 Errors vs. spatial averaging
50 100 150 200
Number of targets
0.0
0.5
1.0
1.5
2.0
Error (ppm)
Error vs. Mauna Loa1/sqrt(n) progression
Tropospheric Emission Spectrometer CO2Observed yearly and seasonal variations are consistent within situ datau
Monthly averages of ~200 targetsMonthly mean error is 0.9 ppm with 5.6 ppm biasBias close to estimated spectroscopic error of ~4 ppm (Devi, 2003)Greatest sensitivity in middle Troposphere (500 mb)Validated for low O.D. cloud, ocean, 40S to 40N
TES CO2 at 511 hPa, 15-30N
2006 2007 2008 2009
Year
365
370
375
380
385
390
395
CO2 VMR (ppm)
TES monthly TES monthly aveave
CONTRAIL aircraft dataCONTRAIL aircraft data Mauna LoaMauna Loa
prior
Highly correlated with Mauna Loa CO2
370 375 380 385 390
TES
370
375
380
385
390
Mauna Loa
corr 0.94
slope 1.02bias -5.6 ppm
Kevin Bowman – ASSFTS 14
Global (40S-40N) TES results
• Comparison of monthly mean TES gridded values (small circles and interpolated values at 511 hPa) and ground station data (large circles)
• A low bias correction of 5.6 ppm is added to TES CO2
Kevin Bowman – ASSFTS 14
-150 -120 -90 -60 -30 0 30 60 90 120 150
-150 -120 -90 -60 -30 0 30 60 90 120 150
-30
030
-30
030
Oct, ’06: TES 511hPa +5.6ppm, Flasks
370
376
382
389
395
VMR (PPM)
-150 -120 -90 -60 -30 0 30 60 90 120 150
-150 -120 -90 -60 -30 0 30 60 90 120 150
-30
030
-30
030
370
376
382
389
395
VMR (PPM)
-150 -120 -90 -60 -30 0 30 60 90 120 150
-150 -120 -90 -60 -30 0 30 60 90 120 150
-30
030
-30
030
370
376
382
389
395
VMR (PPM)
Approach for estimating CO2 sources & sinksObserving System Simulation Experiment (OSSE) by Nassar et al., 2009
TES: 20 x 30 degree x 1 month averages Errors are driven by number of clear sky
profiles per bin
GLOBALVIEW: 76 surface stations
MODEL: GEOS-Chem with NASA GMAO met . fields, specialized CO2 source/sink inputs
FLUXES• 14 regions of combustion and terrestrial
exchange + “rest of world” (29 elements)• A priori flux uncertainty:
– 100% for terrestrial biosphere
– 30% for combustion
Err
or (
ppm
)
Kevin Bowman – ASSFTS 14
Estimates of biosphere & ocean fluxes
TES alone:improves flux uncertainty from 100% initial uncertainty to 15-30%
76 surface stations alone (with 0.1 ppm errors assumed): improves flux uncertainty from 100% initial uncertainty to 15-30%
Based on this analysis, the information content of TES is comparable to surface sites
TES (free troposphere) and surface station (boundary layer) sensitivities are complementary
Nassar et al., 2009
Kevin Bowman – ASSFTS 14
Conclusions
TES observed yearly and seasonal variations are consistent with in situ data
TES CO2 with error characterization can be used to improve estimates of CO2sources and sinks
Next steps
Using real TES data for source and sink estimates
Examine the use of other sensors for measuring CO2 profiles to improve source and sink estimates
Validation versus aircraft data over land in progress
Kevin Bowman – ASSFTS 14
AcknowledgementsWork at JPL was carried out under contract to NASA with funds from ROSES 2007. Work by
Nassar et al. funded by Natural Sciences and Engineering Research Council (NSERC) of Canada. We acknowledge use of GLOBALVIEW-CO2 and Mauna Loa from NOAA-ESRL and CONTRAIL data from World Data Centre for Greenhouse Gases (WDCGG).
Thanks to H. Worden for S/N calculation help
ReferencesMatsueda, H., H. Y. Inoue, and M. Ishii (2002), Aircraft observation of carbon dioxide at 8-13 km altitude over the western Pacific from 1993 to 1999. Tellus, 54B(1), 1- 21, doi: 10.1034/j.1600-0889.2002.00304.x
Nassar et al, R., D.B.A. Jones, S.S. Kulawik, J.M. Chen. (2009), Use of surface and space-based CO2
observations for inverse modeling of CO2 sources and sinks. (Poster) 2nd North American Carbon Program All-Investigators Meeting, 2009 February 17-20, San Diego, CA.
Palmer, P. I., D. J. Jacob, et al. (2003). "Inverting for emissions of carbon monoxide from Asia using aircraft observations over the western Pacific." Journal of Geophysical Research-Atmospheres 108(D21).
Rodgers, C. (2000). Inverse Methods for Atmospheric Sounding: Theory and Practice. Singapore, World Scientific Publishing Co.
Shephard, M. W., H. M. Worden, et al. (2008). "Tropospheric Emission Spectrometer nadir spectral radiance comparisons." J. Geophys. Res. 113.
U.S. Department of Commerce | National Oceanic and Atmospheric Administration Earth System Research Laboratory | Global Monitoring Division http://www.esrl.noaa.gov/gmd/dv/site/SMO.html
Increased sensitivity to boundary layer CO2�improved CO2 source/sink estimates
- how often does TES observe CO2 in the boundary layer?
0-2 km
0.0 0.1 0.2 0.3 0.4 0.5 0.6
Sensitivity (DOF)
40
60
80
100
CDF (%) ~20% have DOF > 0.15*
% cases with less than the specified degrees of freedom (DOF) for boundary layer (0-2 km) and lower Troposphere (0-4 km)
DOF = Trace(A), where A, the averaging kernel, is the sensitivity of the retrieved state to the true state, A = dxret/dxtrue
0-4 km
0.0 0.1 0.2 0.3 0.4 0.5 0.6
Sensitivity (DOF)
20
40
60
80
100
CDF (%)
- highest sensitivity for daytime, summer; ~5% with better than 0.3 DOF- 0.3 DOF: for a 20 ppm enhancement, TES would observe +6 ppm
regional study over U.S. for all seasons
Kevin Bowman – ASSFTS 14
Boundary layer sensitivitySummertime land case ( on previous page)
TES improvements
- TES IR measurements (left) can be sensitive to the boundary layer but cannot distinguish the boundary layer from the free troposphere
- For 3x increased signal to noise and independently obtained temperature, boundary layer CO2 can be discriminated from the free trop. in some cases
3
-0.2 0.0 0.2 0.4 0.6
0
10
20
30
40
50
Altitude (km)
100
10
DOFS 1.0
908 hPa511 hPa133 hPa10 hPa0.1 hPa
3
-0.2 0.0 0.2 0.4 0.6 0.8
0
10
20
30
40
50
100
10
DOFS 2.8
908 hPa511 hPa133 hPa10 hPa0.1 hPa
*
Kevin Bowman – ASSFTS 14