space title
green bullet Home
green bullet Scientific objectives
green bullet Instrument description
green bullet Flights
  • SBI-1: September 2003
  • SBI-2: Antarctica 2006
  • SBI-3: September 2007
green bullet Scientific results
  • Data reduction
  • SBI-1 Science
  • SBI-3 Science
green bullet Publications
green bullet Presentations
green bullet Team
green bullet Useful links
green bullet Site Map

For additional information about this web page and for feedback please contact
Pietro Bernasconi
Phone: 443 778 8970

Data Reduction


During the five hours of observation the camera performed flawlessly, recording images in a continuous mode at a rate of 30 frames per second, for a total of more than half a million broad-band images. Table 1 summarizes the most relevant observations made during the flight. The table does not include the calibration measurements, like the flat fields for the different filters. The actual dataset is more extensive, since the camera was also continuously recording while optimizing the telescope focus, movin the field-of-view from one position to another across the Sun, and while waiting for the pointing and the camera temperature to stabilize. For example, most of the time needed to record a single full-disk mosaic of 10 tiles is actually spent waiting for the system to optimally stabilize itself before taking the actual science images.


Data Reduction Steps

The main steps of the data reduction are: 1) Construction of a flat field; 2) Individually flat field the single frames; 3) Co-align the frames to be averaged, then co-add them to obtain mosaic tiles; 4) Stitch together the averaged tiles to form a full-disk mosaic; and 5) Determine the limb-darkening function and remove it from the full disk mosaic to obtain a map of the photospheric contrast. Dark current corrections are not required because of the particular way the camera operates and delivers the raw images. The raw frames are basically the difference between images recorded with the detector looking at the actual scene (the Sun) and looking at the chopper blade (used as baseline reference), thus having the detector offsets already automatically removed. Foukal and Libonate (2001) or Bernasconi et al. (2004) provide more details on the camera operation.


green ball Step 1: Preparation of a Flat field

Probably this is the most critical step of the entire process. During the flight we recorded several hundred images at Sun center with the telescope far from focus. These images are used to create the flat field. Defocusing the telescope has the effect to remove all the solar surface features from an averaged image. However, because of the relatively large field-of-view of the detector, the limb darkening is still present causing a considerable intensity variation from the center to the edges of the frame. This residual limb darkening effect is not straightforward to remove, but we have developed an iterative procedure that allows us to exactly determine the amount of limb-darkening still present in the averaged flat field.

The procedure takes the advantage of the fact that the mosaic tiles have a fairly large overlap with each other. If the flat field is correct then the regions where tiles overlap, which actually correspond to completely different parts of the frame, should have the same intensity: First, we compute a preliminary flat field without limb-darkening correction, by averaging 300 frames taken at disk center with the telescope out of focus. Then we proceed with Steps 2 and 3 of the data reduction procedure: flat fielding of all the individual frames composing a mosaic; co-alignment and averaging of the frames of the same mosaic tile. Finally, after determining the exact tile positions in the mosaic (Step 4), we compute the difference of all the overlaps, pixel by pixel, and add them up to obtain the sum of all the residuals ΔO. Ideally, the resulting value of ΔO should be zero. Values different from zero are due to detector noise, differences in the actual image because the overlapping tiles have been recorded at different times, and finally by the incorrect estimation of the flat field residual limb darkening. We minimize ΔO with an iterative minimization algorithm. The flat field image is divided by a mathematical model of the limb darkening described by a third degree polynomial with three free parameters (it is an expansion of the two degrees polynomial from Allen, 2000):

(1)spaceLD(μ) = 1 + (μ − 1) ⋅ u + (μ2 − 1) ⋅ v + (μ3 − 1) ⋅ z ,

where μ = cos(θ) is the distance from the Sun center and u, v, and z are free parameters. Three additional free parameters are necessary: the coordinates x and y of the center of LD function with respect to the flat field image, and the radius r of the Sun. Then we proceed to re-compute ΔO by repeating the Steps 2, 3, and 4. The entire process is repeated with different parameters u, v, z, x, y, and r until the smallest value for ΔO is reached.


green ball Step 2: Flat field correction

Each single frame needs to be individually corrected for pixel-to-pixel gain differences before co-adding them together. Dark current corrections are not necessary since each image delivered by the camera is already the difference between two consecutive frames (scene minus chopper blade).


green ball Step 3: Frame co-alignment and averaging

To reduce the noise level, each individual tile is obtained by averaging of 60 individual frames taken at the same location. Each image needs to be co-registered with respect to each other, before co-adding them. We achieved co-registration of the order of 0.1 pixels or better by cross correlating edge-enhanced individual frames.


green ball Step 4: Construction of the mosaic

To cover the entire solar disk it is necessary to record images (tiles) at 10 different locations. The mosaic is built by finding the exact overlap between tiles. The pointing information recorded by the on board-computer when each tile was taken is used as first guess. However this can be off by up to 15 arcsec (about 5 pixels). For a precise overlapping of the tiles we use the same method as in Step 2. Here is a finished mosaic. This represents the first image of the Sun ever obtained with an instrument with flat sensitivity from 0.28 to 2.6 μm. The image spatial resolution is about 5.6 arcsec, limited by the pixel size of 2.8 arcsec.


green ball Step 5: Removal of limb darkening from mosaic

To determine the actual irradiance contrast of the features in the solar photosphere, the limb darkening function (LD) needs to be removed from the mosaic. This is done by fitting the same model of the limb-darkening as in Equation (1) to the actual fill-disk mosaic. Here you can see the same mosaic as above but with the disk intensity divided by the limb darkening function with parameters:
spaceu = 0.718, spacev = − 0.106, spacez = 0.019.
The actual shape of LD can be seen here. Some large-scale artifacts and some seams between tiles can be still seen, but this is because the image has been heavily contrast enhanced to better highlight the faculae and enhanced network. The contrast amplitude of these artifacts is smaller than 0.3%, which is well below our sensitivity requirement of 1% for faculae and enhanced network.


space Back to TOP