The code that we used for the determination of the best orbital parameters was first published by Bertiau & Grobben (1969). It is based on the Lehmann-Filhés method and allows that weights are given to each of the data points. The period can be fixed as well as variable.
The star Per is the primary of an eccentric binary with a period
of approximately two weeks. The star is also known for its strong and
complicated line-profile variations (Smith et al. 1987;
Gies &
Kullavanijaya 1988) on a time-scale of hours. It is not yet clear how many and
what kind of pulsation modes are active in the star, but
high-degree modes are surely involved.
De Cat et al. (in
preparation) have recently obtained an extensive set of high-resolution profiles
that span the complete orbital period with the aim to study the orbital motion,
the pulsation of the primary, and also the coupling between the two. We refer to
their study for further details but use their radial-velocity data of the
Å line of
Per to determine the orbital periods with our method.
The data consist of 11 nights for which the pulsational behaviour is well-covered and 3 additional nights during which the weather conditions were poor and only a few spectra were obtained. We determined the standard error (s.e.) of these latter spectra by means of the method outlined above, i.e. by application of formula (12). To achieve this, each of the radial-velocity curves for the fully covered nights was fitted with a sine after having determined the best frequency per night for such a fit with a period-search algorithm (PDM, Stellingwerf 1978). From these fits we derived the average radial velocity of that night with its s.e. and the amplitude. The latter is used in the determination of the s.e. of the data of the uncovered nights.
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This example shows that adding
points of poorly covered nights to well-determined nightly averages over a
pulsation cycle leads to
the same accuracy of the orbital parameters if
one assigns a proper weight to the scattered data points.
In the example of Per there is no problem to determine the
solution without assigning weights because the data nicely cover
the complete orbital cycle and a couple of additional nights provide little
extra information. When the latter is not the case our method becomes
particularly helpful (see the last example).
The Cep star
Sco was monitored as part of
a systematic spectroscopic study of pulsating stars in multiple systems (see
De
Mey 1997; Aerts et al. 1998b). It
consists of a
Cep-type primary and a yet unknown secondary. This object
has a pulsational behaviour that is similar to the one of the
multiple
Cep star
Sco and was
observed during the same observing runs that were devoted to both stars
(see De Mey et al. 1997, for the results on
Sco).
The data set consists of 9 fully covered nights and 78 scattered data
points. We refer to De Mey (1997) for a full description of the data set.
Two pulsational frequencies are known in the literature for Sco and we
fitted the fully covered nights with a sine fit for the main frequency
5.004 c/d (Lomb & Shobbrook 1975). We do not find different results than the
ones listed below by considering the second frequency given by Lomb &
Shobbrook, nor when we first search for the best frequency per night and make a
fit with this frequency.
De Mey (1997) determined the orbital period from the complete radial-velocity
data set with the PDM and CLEAN methods and found 195.77 days. She used
this fixed period to search for the other orbital parameters. We refer to her
work for the results.
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At first, we used the same data set as De Mey (1997)
to search for the orbital parameters in the traditional way without fixing
the orbital period. This leads to a period of 195.870.01 days and slightly
different orbital parameters as found by De Mey (1997). We refer to the second
column of Table4 for
the values of the other orbital parameters. The rms of this
solution is 2.38 km s-1 while the orbit given by
De Mey (1997) corresponds to an rms of
2.44 km s-1. We therefore take our solution given in Table4 and compare
it with the results obtained with the approach outlined in Sect. 2.
The results
of this comparison are given in Table4 and are shown in Fig. 2.
It can be noted from the figure that the solution found by means
of our new approach gives a slightly better fit to the data and results in
orbital parameters with substantially smaller standard errors.
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Figure 2:
The orbital radial velocity of the ![]() ![]() ![]() ![]() |
For this example, the introduction of weights is less crucial for the point estimates than for the standard errors. The reason is that we were able to extend our initial data set with many scattered follow-up data that were obtained to determine the orbit. If the number of scattered points is sufficiently high and well-spread, they will not so much change the average, but may affect precision estimation. Moreover, this star has an orbital velocity amplitude much larger than the amplitude of the pulsation velocity. The last example shows that, when these two conditions do not hold, it can be essential to include weights in a proper way.
The application of our method to the data presented by Aerts
et al. (1998a) illustrates that assigning weights as we propose here can make the
difference between succeeding and failing to determine the orbital parameters in
the case that the time spread of the data is very limited with respect
to the orbital period.
Indeed, Aerts et al. (1998a) failed to find a suitable orbital solution for
Cru before the application of our method. The reason is that
the few follow-up measurements that were gathered with the specific aim to study
the orbital motion were almost neglected in the calculation of the orbit
compared to the more than 1000 spectra
obtained for the study of the pulsational behaviour. Moreover,
Cru is
an example in which the amplitude of the orbital motion is comparable to the one
of the pulsational velocity. In such a situation, it is crucial to substitute
fully covered nights by a single data point and add this measurement to the
follow-up data, each of them with a proper weight.
In fact, the development of
our method originates from the purpose to determine an orbital solution for the
complicated case of
Cru from the data presented by
Aerts et al. (1998a). We list the solution for the orbit of
Cru in
Table5 and refer to Aerts et al. (1998a) for
further details of this application.
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