4 Final Report - Emits - ESA
4 Final Report - Emits - ESA
4 Final Report - Emits - ESA
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4 <strong>Final</strong><br />
<strong>Report</strong><br />
If the LoS motion during the summation of the successive images is large (typically > 1 pixel), the<br />
motion must be compensated for by shifting the pixels. The simplest correction is the so-called<br />
"nearest pixel motion compensation", where the shift is limited to an integer number of pixels, simply<br />
achieved by a shift in memory and an accumulation. The average MTF loss at the Nyquist frequency is<br />
0.64 on the accumulated image, i.e. equivalent to a shift of one pixel over the whole accumulation. To<br />
reduce this significant degradation of the MTF, refined offset correction methods based on pixel<br />
interpolation are possible, but not retained for Geo-Oculus for their low maturity and the required large<br />
on-board computation and storage capabilities.<br />
The first step is however to measure the LoS motion between two integration phases, with an<br />
accuracy significantly better than half a pixel (0.2 pixel i.e. ~0.1 µrad).<br />
4.4.3.2 LoS drift measurement<br />
The LoS motion information can be extracted from gyroscope measurements, provided they are<br />
mounted close to the focal plane. The following figure shows the LoS drift estimation error for two high<br />
accuracy gyros (Pleiades Astrix 200 FOG and SIRU HRG): Over the maximum image acquisition time<br />
(5 sec), the error is 0.3-0.5 µrad, well above the 0.1 µrad requirement. Gyros are therefore not<br />
adequate for LoS drift estimation.<br />
Gyro drift (µrad)<br />
0,5<br />
0,4<br />
0,3<br />
0,2<br />
0,1<br />
0,0<br />
0 1 2 3 4 5<br />
Time (secs)<br />
Figure 4.4-3: LoS drift estimation accuracy using gyroscopes<br />
ASTRIX200<br />
In the case of GEO-observation with a staring instrument, the motion information can also be<br />
extracted from the image itself, which removes the need for additional motion sensor. The principle is<br />
to correlate in real-time on board the spacecraft the incoming image with the accumulated image, so<br />
as to determine the relative image to be corrected. Either the full image or vignettes of interest are<br />
used. In the first case, the processing load is high, but the algorithm is simple (correlation over a small<br />
moving window) and repetitive, which is well adapted to FPGA or ASIC implementation. In the latter<br />
case, the system shall identify vignettes of interest within the first image using an algorithm detecting<br />
areas with contrasted variations. Then the correlation is performed between the selected vignettes<br />
extracted from the accumulated & current image.<br />
Such techniques are actively investigated at Astrium, primarily for on-ground processing to improve<br />
image quality without relying on pre-defined landmarks. The resulting accuracy of image correlation is<br />
in the order of 10% to 20% of a pixel, that is to say below 0.03 to 0.06 µrad, well with in the 0.1 µrad<br />
requirement. Image correlation is therefore the selected approach for LoS drift measurement.<br />
Doc. No: GOC-ASG-RP-002 Page 4-47<br />
Issue: 2<br />
Date: 13.05.2009 Astrium GmbH<br />
SIRU