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  • SBI-1: September 2003
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For additional information about this web page and for feedback please contact
Pietro Bernasconi
Phone: 443 778 8970

Camera


space Detector Characteristics

The key component of the SBI is the bolometric imager, which has the unique capability to record images (320×240 pixels in size) in total light, i.e. with a flat photometric response from the UV to the NIR. The detector characteristics are described in more detail in Foukal and Libonate (2001).

The detector is composed of an array of 320×240 barium strontium titanate (BST) ferroelectric elements, each element 50×50 μm in size. BST exhibits a strong temperature dependence of capacitance around its Curie point (at about +30 °C). If exposed to IR radiation the elements produce a change in output current that is proportional to the radiation intensity. For the SBI we used a modified IR detector array based on this effect (Hanson, 1997), commercially available for night vision cameras. For our 30 cm aperture F/12 telescope the image scale is 0.0573 arcsec/μm. Given the detector size, the image field of view is about 917×687 arcsec. Thus, a full disc image of the Sun can be obtained with a mosaic of 10 single tiles, with the pattern 2-3-3-2, and with a considerable overlap between individual tiles.

To transform such a camera into a detector with flat response over the UV to NIR range we deposited a thin (~30 μm) layer of gold black on the monolithic light-receiving surface of the array. Gold-black films have a spectral absorptance that varies less than ±1% from 0.2 μm to beyond 3 μm (Advena et al., 1993). Therefore, such a film will uniformly redistribute the absorbed radiation in the above mentioned spectral range in the form of thermal emission and it will be detected by the under lying thermal IR BST imaging array. This link shows that the measured hemispherical reflectance of a gold-blackened BST array is extremely flat over the spectral range between 300 and 1600 nm. This indicates that approximately 99% of the incident light in that range is absorbed. An image of a gold-blackened Raytheon BST detector array with fused quartz window used as a prototype for the SBI is shown here.


space Camera Operation

The detector elements are sensitive to temperature change but do not provide a DC response (the temperature signal is AC coupled). A chopper (with the shape of an Archimedes spiral) modulates the scene energy onto an AC carrier, normally at 30 Hz. Abrupt sensor output changes occur when the chopper blade exposes or blocks the source image energy. If the scene temperature is higher than the chopper blade temperature, the pixel element will heat up when exposed and cool down when blocked. The opposite will occur if the scene temperature is colder than the chopper blade temperature, producing an apparent 180° phase shift in the signal, however this is a perfectly acceptable mode of operation for this imager chip.

The output from each pixel amplifier goes to a sample-and-hold circuit, and the output from the pixel multiplexer is the difference between the current pixel amplifier and the last held value. When the next adjacent pixel is read out, the previous pixel output is sampled and stored in its sample/hold circuit. This means that the output frames from the detector have alternating polarity. For example, if we define Os the output signal when a pixel element is looking at the scene, and Oc the output signal when the chopper blade is in front of the same element, then the output signal S(i) for that pixel for frame i (the ith cycle of the chopper blade) is given by:
2 spaceS(i) = Os − Oc + Z + noise,
where Z is an arbitrary signal offset. The output signal S(i+1) from the next frame would then be:
2 spaceS(i+1) = Oc − Os + Z + noise.
By computing the difference between consecutive frames we obtain:
2 spaceS(i) − S(i+1) = 2(Os − Oc) + √2 noise,
thus eliminating the offset and reducing the noise.

grn ball Another image of the camera, with a chopper blade made of a transparent material (used only for testing).


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