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Airborne imaging DOAS measurements (iDOAS)Introduction Instrument Observation Geometry Viewing Angles Imaging Quality First Results References Links Contact
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Figures: (Left) Polar-5 aircraft at the
hangar in Bremerhaven. (Right) iDOAS installed inside the Polar-5 aircraft in
Jun 2011.
The special setup allows gap-free measurements (due to frame transfer CCD) and flexible positioning in aircraft (due to sorted fibre bundle).
Spectrometer type: | Czerny-Turner with 300 mm focal length |
Spectral window/resolution: | 420 - 460nm / 0.7-1.0nm |
Grating: | 600 l/mm |
CCD Detector size: | 512x512 pixels, 8.2x8.2 mm² |
Detector type: | Frame transfer (FT) technique |
Entrance optics: | Wide angle objective + fibre bundle |
Fibre bundle: | 35 sorted fibres imaged onto CCD |
Power consumption: | < 550 W (variable, typically < 400 W) |
Power Supply: |
230 VAC via UPS or 28 VDC via Inverter and UPS |
Length x width x height: |
915 x 565 x
402 (given in mm; rack only!) |
Mass | ~ 120 kg + ~ 10 kg base plate |
Temperature of spectrometer |
35°C
(stabilized, spectrometer unit only) |
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Field of view: ~48° across track (g),
<3° along track (q)
Swath width: on the order of flight altitude H
Spectrometer viewing directions: max. 35 LOS (line of sight)
from 35 fibres
LOS after averaging across track: fibres combined to e.g. 9 LOS (qi)
Exposure time texp: typ. 0.5s
Measurement sequence: no gaps between exposures
Spatial resolution: ~100 m (at H=1km flight altitude, 9 viewing directions)
The realized spatial resolution depends on flight altitude and required SNR
Two nadir ports are used: the spectrometer objective and a picture camera
Sketch showing the influence of the aircraft angles (pitch, roll and yaw) on the ground geolocation
Calculation of correct ground geolocation from the field of view is important
Geolocation information of the aircraft is received from GPS sensor and
gyrometer
Consideration of the aircraft angles (pitch, roll and yaw) is required in
addition to GPS position
Influence of aircraft angles on geolocation:
Aircraft movement changes the ground pixel geolocation significantly.
In addition, the magnitude of the displacement of the observed pixel on
ground depends on flight altitude and LOS.
Displacements of the ground pixel at a flight altitude ~1km:
During straight tracks: on the order of a few tens of metres
During turns: typically on the order of 500 m, max. displacements larger than
1km
Average for central flight pattern on 04.06.11: around 160m
The imaging quality of the iDOAS instrument is very good and allows recording of small scale sources. In the figure above, the left figure shows the CCD intensity image (in absolute Counts). Spatial information is distributed along the vertical axis, spectral information along the horizontal axis. The stripes are generated by the individual fibres. The right image shows the photograph of the nadir picture camera above a brightly reflecting motorway in between darker fields to the sides. The blue box marks the field of view corresponding to the instant when the CCD image on the left was recorded. The high radiation intensity on the CCD image is nicely visible in one of the fibres only.
During a flight on June 4th in 2011, a power plant exhaust
plume has been observed emerging from a black coal power plant. The recorded
spectra have been analysed for the absorption signal of NO2. The settings for
the DOAS retrieval are listed below. The enhanced NO2 amounts above the power
plant are clearly visible in the NO2 map. Large variations of the NO2 amounts
across and along track are observed
Figure: Preliminary result of NO2 slant columns above a black coal
power plant. The exhaust plume is clearly visible with enhanced NO2
amounts downwind of the power plant stack. From the slant columns, the vertical
columns and respective volume mixing ratios are computed by taking into account
the radiative transfer conditions as well as an NO2 altitude profile.
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