Retrieval Coefficient Assessment for TexAQS 2000
MJ Mahoney, July 24, 2002
Background
The TexAQS 2000 campaign was the first time that a Microwave Temperature
Profiler (MTP) flew extensively in the planetary boundary layer (PBL).
Because of the short time available to prepare for this field deployment,
the existing DC-8 MTP was flow "as is." There wasn't time to consider what
the optimum instrument configuration might be, such a frequency of operation,
scan angles, etc. Since the DC-8 normally flies at an altitude of 10-12
km, much more optically-thick oxygen lines are observed than might be optimal
at the typical TexAQS flight altitude of 0.61 km (2000 feet). As it turns
out, this is both good and bad.
A particular concern before performing the MTP retrievals for TexAQS
2000 was the impact of ground emission on the observed brightness temperatures.
Initially, it was hoped that infrared surface temperatures measured on
the NCAR Electra could be used as an additional "observable" in the MTP retrievals
to constrain the downward-looking observables. This might have been possible
over water, but over land the emissivity is simply too variable. In addition,
there is no obvious relationship between the infrared and microwave emissivities,
so it is not clear where this approach might have lead. (see
Investigation of Heimann Probe Data
)
Given the limited resources for this work, the decision was made to weight-down
the downward-looking MTP brightness temperature measurements so that they
would not impact the retrievals. This was done by requiring five optical-depths
(one optical depth is the e-folding distance) between the aircraft and the
ground in the viewing direction at the most optically-thin measurement frequency
(55.51 GHz). Using this criterium, it was found that for flight at 2000 feet,
the rms difference between 206 coastal RAOBs and simulated retrievals was
<0.4 K at a distance of 1000 feet (0.305 km) below the aircraft, and this
was deemed acceptable. (The rms difference between RAOBs and the simulated
retrieved temperature at flight level was 0.25 K.)
Because it was (erroneously) believed that the NCAR Electra never flew
when ground inversions existed, the retrieval accuracy assessment did not
include any RAOBs with ground inversions. This was an oversight, because ground
inversions did exist over the downtown Houston RAOB launch site on August
30, 2000, and was apparent in RAOBs launched at 1400 (50.4 ks) and 1700 (61.2
ks) UT on August 30, 2000. The NCAR Electra took off at ~55 ks on August
30 and flew over downtown Houston at 56.7 ks and 58.4 ks. The first overpass
was at 11,000 feet and the second at 2000 feet. Examination of the MTP data
shows no evidence for the inversion when at 11,000 feet because it does not
have the vertical resolution necessary to do so, but the measurements clearly
show the inversion when flying at 2000 feet.
The August 30, 2000, Ozone Event
On August 30, 2000, during the TexAQS 2000 campaign, atmospheric conditions
were such that the larger-scale geostrophic flow was offshore and opposed
the local sea breeze near Houston, Texas. This situation is especially conducive
to pollution events, because air originating from the emission sources near
Houston become stagnant over Galveston Bay, leading to very high ozone levels
when the sea breeze front finally penetrates inland. A question which we
wish to pursue is whether or not the Jet Propulsion Laboratory (JPL) Microwave
Temperature Profiler (MTP) data taken aboard the NCAR Electra can be used
by Texas A&M University (TAMU) to validate and improve the MM5 model
simulations of boundary layer depth, boundary layer variability, and sea
breeze structure on August 30 and other days during the TexAQS 2000 field
program.
While the MTP measurements clearly map the horizontal temperature gradients
over the Houston area, this is not the most important driver for the MM5
model’s ability to forecast a pollution episode. What matters most is the
surface forcing as characterized by the temperature field below the NCAR
Electra’s flight altitude. Since the NCAR Electra nominally flew at 2000
feet, or near the top of the PBL, relaxing the weight given to the downward-looking
MTP measurements could have a negative impact on the usefulness of the MTP
data for the MM5 modeling activity.
For the purpose of evaluating the effectiveness of the MTP retrievals to
capture the surface forcing, seven Airsonde radiosondes from downtown Houston
(HOU) and LaMarque (HSE) were chosen for case studies: from HSE – 2002.08.28
2033UT and 2002.08.31 2300UT, and from HOU - 2002.08.29 2301UT, and 2002.08.30
1400UT, 1700UT, 2000UT, 2259UT. Simulated MTP retrievals were performed
to understand the limitations of the downward looking retrievals, and hence
the ability of the MTP to characterize the surface forcing.
The figure above shows the accuracy of the simulated retrievals for four
differently weighted sets of rectrieval coefficients (RCs) as a function
of the distance below the aircraft. Only the five radiosondes without inversions
were used; all the radiosondes were used in the next figure. Since the radionsondes
used to calculate the retrieval coefficients did not include any inversions,
all of the RC sets did quite well, with the most heavily weight RCs being
best. The average error has no bias, and its rms error is <0.25 K within
1000 feet of the aircraft.
The figure above shows the
results when test radiosondes with inversions are included. As expected,
the retrievals deteriorate significantly. However, since the raw MTP measurements
clearly show brightness temperatures expected for inversions, it is expected
that with proper retrieval coefficients that these errors will drop significantly.
MTP Home Page:
http://mtp.jpl.nasa.gov