Lunar data preparation for PROBA-V

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Presentation transcript:

Lunar data preparation for PROBA-V Stefan Adriaensen (VITO) 2nd GSICS/CEOS Lunar Calibration Workshop, Xi’an, China 13/11/20117 – 16/11/20117

PROBA-V instrument No active thermal control No on-board calibration lamp No solar diffuser Design complexity 3 Cameras 2 focal planes: VNIR with 3 bands SWIR with 1 band but staggered strips

Oceans DC Clouds Deserts Absolute Interband Temporal Inter-pixel PROBA-V Calibration OSCAR* (Optical Sensor Calibration with simulated Radiances) Relies on combination of various vicarious calibration methods to reduce uncertainty in the calibration results and to verify the different requirements Absolute Oceans Interband DC Clouds Antarctica Greenland Inter-pixel Yaw steering maneuver Temporal Deserts *Sterckx et al. IJRS, 2014; Sterckx et al. , TGARS, 2013; Govaerts et al., RSL, 2013

Moon Maneuver Only center camera is considered 7 degrees phase before and after full moon 360 degrees pitch at 0.2deg/s every band has different view angle 24.5 seconds between swir and nir lunar scan takes about 2.6 seconds nir moon red blue swir

Processing steps Input L1A Extract band Radiance Masking Geometry Total Irradiance

L1A extraction HDF5 file format : convert to image files (DN) extract platform line data : line time and satellite position,integration time SWIR VNIR

Conversion to Radiance based on vicarious calibration techniques radiometric model : dark current calibrated using nightly ocean scenes every month background radiance observed in the image is close to zero( <0.6% of avg moon pixel)

Masking threshold Center of observation timestamp Satellite position Pixel solid angle 5% of max radiance Radiance image

Number of selected pixels vs moon obs distance

Solid angle the pixel solid angle is calculated directly from the data Pixel along track angle = rotational_speed * (t_max - t_min) / nr_of_lines Pixel across track angle = ( 2 * atan (moon_eq_radius / distance obs_moon) ) / nr_of_columns Solid angle includes oversampling factor Orientation of the moon in the image is currently neglected

Provided to GLOD basic processing is performed per observation : timestamp satellite position total irradiance recently updated +100 observations no imagettes have been included to GLOD

Results : BLUE

Results : RED

Results : NIR

Conclusions PROBA-V data has been processed and compared with GIRO successfully update current PROBA-V GLOD dataset is required better performance might be achieved (cfr. orientation of the moon ) SWIR processing needs full review