The central overlap technique was first proposed by Eichhorn & Jefferys (1971). It intends to determine the plate-to-plate transformation parameters, the stars motions and the errors simultaneously, using all the data at the same time. This method has rigorous mathematical foundations (Eichhorn 1988), but its computational requirements are so huge that, in practice, it cannot be implemented in its strict formulation. The usual approach to the method is generally known as iterative central-overlap algorithm (ICOA), and implies the separation of the determination of plate and star parameters in consecutive steps that are iterated until convergence is achieved. This procedure is known to be equivalent, in practice, to the one-step block-adjustment approach (Tucholke 1992), and has been extensively used during the last decades (for instance, Cudworth et al. 1993; Van Altena et al. 1988; Tucholke et al. 1994).
Given the diversity of the plate material used in this study, we decided to use an ICOA for our astrometric analysis. Our implementation, similar to that by Jones & Walker (1988), is summarized in the flow chart of Fig. 3. One plate is selected as reference ("master'' plate). All the other plates ("source'' plates) are tied into the master reference system. Proper motions are computed from different positions at different epochs, and they are fed-back to improve the transformations of source plates to the master plate reference system. The whole process is iterated until the computed proper motions converge. The best modern epoch plate, OCA 3305, was selected as master.
To begin the process, an initial input list with a number of stars cross-identified with the master plate is needed for each source plate. These initial cross-identification files were generated by matching the equatorial coordinates contained in the preliminary astrometric catalogue of each plate (Sect. 2.8).
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Figure 3: Flow chart of the iterative central overlap algorithm (ICOA) used for the determination of proper motions |
The code calculates the transformation coefficients by a least
squares fit, with 3 clipping: the fit is performed iteratively,
discarding at each step those stars whose residual is larger than
3
, until no more stars are eliminated.
The program admits a general plate model of the following form:
x' = Pn,x(x,y) + Qx(x,y,m); | (4) |
y' = Pn,y(x,y) + Qy(x,y,m). | (5) |
P2,x(x,y) = a0 + a1 x + a2 y + a3 x2 + a4 xy + a5 y2.
Qx(x,y,m) and Qy(x,y,m) are polynomial functions containing some magnitude-dependent terms.So, the general model has a purely geometrical part, beside a mixed geometrical-photometric dependence. The specific plate models used in the calculations will be discussed in Sects. 5 and 6.
The cross-identification routine applies the just computed transformation equations to all stars in the source plate and performs a complete cross-identification with the master plate. The cross-identification takes into account a double position-brightness criterion:
The search radius and magnitude tolerance are parameters set up for each plate. The search radius is a function of the epoch difference with the master plate. For contemporary plates, a search radius of 5'' was selected. The search radius grows linearly with time in such a way that for an epoch difference of 90 years, it becomes 9''.
The magnitude difference tolerance was set to , where
and
are the
dispersions of the fit performed on the master and source plates for
cross-identification purposes (Sect. 3.3), respectively.
The resulting list of cross-identifications was re-introduced into the first element of the loop, in order to compute an improved plate-to-plate transformation. The loop was iterated until the number of cross-identifications in the output list stabilized. This resulted in one file for each source plate, containing the positions of all matched objects for the epoch of the source plate in the reference system of the master plate.
The programs used in the transformation-crossing loop were adapted from C-codes kindly provided by C. Alard, and originally designed for the DUO (Disk Unseen Objects) project (Alard & Guibert 1997).
After the automated recovery of unmatched bright stars, proper
motions were computed in the master plate reference system by means of
least squares fits of position as a function of epoch:
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(6) |
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(7) |
The index p run over the whole plate set, including the master
plate. The fits were performed including a weighting system that took
into account the plate scale (Sect. 7.1). The proper
motions fits included a 3 clipping. For a given star, after
performing a proper motion calculation in both coordinates, the largest
residual in x and y was checked. If one or both of them were larger
than 3
, the plate was removed from both fits for this star and
the fit parameters re-computed. The checking and rejection was repeated
until all the residuals were smaller than 3
. The resulting
parameters and standard errors were recorded.
High proper motion stars can distort the reference frame, if their motion is not taken into account in the plate-to-plate transformations. At the end of the first iteration, a search for high proper motion stars was performed through the output list. The stars with modulus of proper motion larger than 6 mas yr-1 were labelled. All proper motions were set again to zero, and the whole process was repeated. But now, in the second iteration, high proper motion stars were not used for computing the plate-to-plate transformations. However, they were included in the last cross-identification performed in the transformation-crossing loop, and they continued the rest of this and further iterations as any other star.
From the third iteration on, positions of all stars in the master
plate were converted to the epoch of each source plate, by applying the
parameters () and (
), before
entering into the transformation-crossing loop. At this stage, the
reference frame is no longer linked only to the physical positions
measured on the master plate, but depends on the whole set of
astrometric data.
At the end of the third and following iterations, the mean change of the proper motions from the previous to the last iterations was computed, using the formal proper motion errors as a weight. When the average change was well below the mean error, the iterations stopped.
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