As described above, the UVIS channel uses two 4096×2051 CCDs, butted together to yield a 4096
×4102 array with a ~31 pixel (1.2 arcsec) gap. Because the detector is tilted along its diagonal axis 21
° with respect to the incident beam, the field of view projected onto the sky is rhombus-shaped, 162 arcsec on a side, with an angle of 86.1
° between the sides at amplifiers B and C (
Figure 6.1). The pixels projected onto the sky are also rhomboidal, ~0.04 arcsec on a side.
Distortion must be taken into account when exposures are flat-fielded, photometrically calibrated, used for astrometric measurements, or combined with other dithered exposures. The AstroDrizzle software appropriately carries out those operations; a combination of software packages in
DrizzlePac can be used to optimize the combination of dithered exposures. (See the
DrizzlePac documentation.)
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HST-based system (V2, V3 or U2, U3; units of arcsec)
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The image-based coordinate system (Axis1, Axis2, as shown in
Figure 6.1) is an orthogonal system of detector pixel readouts. Axis1 is aligned with the detector data rows and Axis2 with the columns. It is used by the calibration pipeline and other data-analysis software and is sometimes also referred to as the user frame. When a detector image is displayed on a computer screen, this system has the X-axis (Axis1) increasing to the right and the Y-axis (Axis2) increasing to the top of the screen, with 1 being the conventional index of the first pixel in both axes. For WFC3/UVIS, each chip has its own origin and Axis1, Axis2 system. The image-based coordinate system is used in most figures in this handbook, as well as in the aperture definitions available in the Science Instrument Aperture File.
The POS TARG reference frame, sometimes referred to as the spacecraft system, is used for specifying the placement of an astronomical target relative to the aperture reference point (sometimes called the fiducial point) in the instrument field of view. Its units are arcseconds. For the UVIS channel, the POS TARG system is defined such that the POS TARG Y axis is parallel to Axis2 at the reference point of the aperture in use. The POS TARG X axis is orthogonal to the POS TARG Y axis; it is not parallel to Axis1 due to geometric distortion.
As is the case for other HST instruments, the POS TARG origin is defined to be at the reference point (fiducial point) of the user-selected UVIS aperture (such as the geometric center of a particular chip, or the optimum center of a quadrant, etc.; see
Table 6.1 below for the names of the various UVIS channel apertures).
Figure 6.1 illustrates the POS TARG reference frame for the “UVIS” aperture, whose center is near the middle of the WFC3 UVIS field of view; the POS TARG directions are indicated by arrows labeled Xpos and Ypos.
The HST-based, or vehicle (V2, V3), system is an orthogonal reference frame tied to the telescope and is used operationally for alignment, pointing, and slewing purposes. The V1 axis lies along the optical axis while V2,V3 run parallel and perpendicular, respectively, to the solar-array rotation axis (see
Figure 2.2). Note that the (undistorted) diagonals of the WFC3 CCD detector run along the V2,V3 directions. Because WFC3 is on-axis, the origin of the V2,V3 system lies near the center of the WFC3 field of view. However, the V2,V3 (and U2, U3) coordinate axes have been shifted for clarity in
Figure 6.1.
HST observers may be more familiar with the U2,U3 coordinate system than V2,V3; for example, the specification of the ORIENT angle Special Requirement in APT uses the position angle of the U3 axis. The U2,U3 coordinates are defined as U2 = –V2 and U3 = –V3, and are marked in
Figure 6.1. Observations of an astrometric field are made to locate the detector in the (V2, V3) system (
WFC3 ISR 2009-35).
A fourth coordinate system (the detector-based reference frame in pixel units) is described here for completeness, but observers are unlikely to encounter this system other than in technical documents created during the development and ground-testing of WFC3. The detector-based system (Xdet, Ydet) is used by the flight software for commanding the detectors. It is a right-handed system based upon the orientation of the CCD serial registers, with its origin at Amplifier A (the four amplifiers are in the outer corners of the detectors, as shown in
Figure 6.1). The +Xdet and +Ydet axes map to the –Axis2 and +Axis1 axes, respectively. Unlike the image-based Axis1, Axis2 system, the detector system is 0-indexed. Parallel shifting is performed along constant Xdet, and serial shifting is done along the constant Ydet direction (
Section 6.7.2).
Beginning in Cycle 18, a wider range of subarray sizes was provided: 512×512, 1k
×1k, and 2k
×2k. User-defined subarrays, and subarrays that span quadrant boundaries, are no longer supported. Subarrays are invoked via the appropriate Aperture parameter in the Phase II observing proposal; these apertures contain the string “SUB” in their names.
Figure 6.2 shows the supported subarrays. See
Section 6.4.5 and
Table 6.1 for the reference points (default target positions) of these apertures.
For the special case of quad filters (which are optical elements that include four different bandpasses simultaneously, one bandpass per WFC3 UVIS quadrant), the observer must select one of the “QUAD” Aperture values in the Phase II proposal, in conjunction with the desired quad filter via the filter parameter. This combination of quad aperture and quad filter ensures that the target is automatically placed in the correct quadrant for imaging with the requested quad bandpass. Furthermore, specification of the subarray quad aperture (UVIS-QUAD-SUB) instructs the ground system to read out only the 2k×2k quadrant of interest. If “-SUB” is omitted from the quad aperture name (i.e., UVIS-QUAD, UVIS-QUAD-FIX), the target is positioned in the proper quadrant for the bandpass requested in the filter parameter, but the entire frame, both CCDs, is still read out.
Table 6.1 indicates which apertures place the target at the geometric center of the subarray, and which apertures place it at a substantial offset from the center. See the
Phase II Proposal Instructions for updates in aperture definitions at the beginning of a new cycle.
The APERTURE parameter in the Phase II observing proposal defines two quantities: the active
region of the detector to be read out (full frame or subarray), as well as the positioning of the target within the region (
reference point). The default is to place the target at the reference point (also called the fiducial point) of the chosen aperture, but a
POS TARG Special Requirement may be added to offset the target from this position.
With regard to pointing HST, there are two types of apertures: “
fixed” and “
optimum.” The fixed positions have reference points near the geometric center of the aperture in question, and, as the name implies, their locations will remain fixed in image-based coordinates for the life of the instrument. The “optimum” apertures have reference points that are offset from the geometric center so as to avoid any known CCD features (e.g., bad column, quad filter edge effects) that might compromise the observation of a target at that position. The locations of the “optimum” aperture reference points—in both the image-based coordinate system and the spacecraft V2,V3 coordinate system—may change over time as the characteristics and the characterization of the CCD evolve.
There are also fixed and optimum apertures for use with the quad filters. Because the filter wheel assembly is necessarily offset from the focal plane, the edges between quad filters are blurred at the focal plane, producing regions with contributions from multiple quad filter passbands (Figure 6.8). The UVIS-QUAD-SUB apertures (redefined for cycle 20) and UVIS-QUAD apertures have reference points centered within the useful single-passband regions, while the UVIS-QUAD-FIX apertures have reference points at the geometric centers of the quadrants (closer to the filter edge effects). In programs where targets are placed in different quadrants, the choice of quad aperture will affect the size of offsets and may require new guide star acquisition, as described in
Section 10.2.
Subarray apertures pictured in Figure 6.2 are all “optimum”; no “fixed” apertures are available for these subapertures. The reference points for these apertures have initially been defined near the geometric center of the subarray, except for the 2K2 apertures, where the reference points match those of the UVIS-QUAD apertures.
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2048×2050, quadrant corresponding to selected quadrant filter
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512×512, quadrant C near detector center
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