Astron. Astrophys. 364, 816-828 (2000)
5. The sensitivity function
The planned GOLF signal would have involved the ratio
. In this case the normalization
factor would have cancelled out. Due
to the poor operation of the rotating polarization mechanisms, the
GOLF instrument now operates in a single wing and the normalization
factor is found by comparison to a temporal average of the returned
integrated-sunlight signal. For the purpose of the simulation of the
GOLF signal this average can also be calculated by integrating
or
over the visible solar disk since we use line profile functions which
represent an average of the time-variable profiles. To avoid
duplication of formulae which are essentially identical, we replace
the subscript b or r with w as a generalized wing
designation where w can take on the values b and
r. The average intensity is then:
![[EQUATION]](img93.gif)
The apparent velocity signal detected by GOLF is then the change in
intensity due to a mode distributed over the surface according to
relative to the average intensity
multiplied by a conversion factor :
![[EQUATION]](img96.gif)
We define a sensitivity S to be a function of x and
y which when multiplied by the surface velocity
and integrated over the visible disk
yields the observed change in velocity. Consequently, the integral in
Eq. (32) shows that the appropriate definition of the sensitivity
function is:
![[EQUATION]](img97.gif)
Due to the presence of three scattering components, the character
of the sensitivity functions depends on the resonance cell temperature
through the functions. If a single
scattering component were present, the response function would simply
be . Consequently, it is useful to
examine these three functions independently to help anticipate the
character of a change which could be caused by a change in the balance
between the three scattering strengths. These functions are shown in
Fig. 4 in a format similar to that used for Fig. 3. The
range of velocity shown in these figures is slightly larger than is
seen by the GOLF instrument including the effects of orbital velocity
variation and solar rotation. The solar disk center curves for
have a restricted range since they
do not involve solar rotation. However, the significant non-linearity
shown for the 60o case and which is present at
75o as well, indicates that the representation of the solar
line profiles as triangles or trapezoids is not a good approximation.
Due to the fact that the signal comes from all three components, some
of the slope variation seen in this figure in fact cancels out and the
net non-linearity is not as extreme as is shown in this figure.
![[FIGURE]](img101.gif) |
Fig. 4. The sensitivity functions for each of the scattering components. Each of these curves is the local line slope normalized by the local bisector intensity. The velocity is relative to the wavelength of the local line bisector.
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The velocity conversion factor can be estimated in two ways. The
variation in the orbital velocity corresponds to a uniform shift of
the whole solar surface, i.e. it is equivalent to picking
to be a constant which may
arbitrarily be taken as unity. Eq. (32) then yields:
![[EQUATION]](img103.gif)
The second method is by tracking the observed GOLF output as a
function of and applying the
analysis of Ulrich et al. (1998). The comparison is shown in
Fig. 5 for two values of cell stem temperature. There are four
points of comparison relevant on this figure: the value of
, the slope of
as a function of
, the separation between the values
of and
parameterized as
) and the curvature of
as a function of
. The excellent agreement between all
these parameters represents a strong validation of the model. Of these
four points of comparison, only the curvature is not well reproduced
from the ground-based profile model.
![[FIGURE]](img111.gif) |
Fig. 5. The conversion factor derived from the GOLF measurements on SOHO shown as the solid lines to the same parameter derived from the ground-based line profiles for two stem temperatures: 146oK (short-dashed lines) and 155oK (long-dashed lines).
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While values for many parameters go into this model, these
parameters are all determined from data other than that shown in
Fig. 5. Furthermore, we are primarily interested in using
spatially resolved data to reproduce the GOLF signal which means that
we do not need separately but rather
use to convert the GOLF signal to a
velocity and at the same time use
to convert the spatially resolved data to an equivalent GOLF velocity.
As long as the model is consistent between these two applications,
most uncertainties cancel. The largest uncertainty in the model
concerns the treatment of the spectral resolution of the Mt. Wilson
system and the effect of line smearing due to spatially unresolved
line-of-sight velocities. Either of these effects produce changes in
the functions at the 5% level and we
believe they cancel so that it is best to adopt the directly observed
profiles as we have done here. The scattered light corrections to both
GOLF and the Mt. Wilson profiles are constrained respectively by GOLF
data taken during cool cell periods and the fit of the core intensity
of the Mt. Wilson profiles to those measured by the double-pass system
of Delbouille et al. (1973). The values of
are changed by 2% when this
correction is dropped. The amplitude of magnetic modulation almost
exclusively governs the separation between the
curves for the two states of
modulation. Note that the amplitude of magnetic modulation was
adjusted in the paper describing the instrument sensitivity
Ulrich et al. (2000) in order to account for the two wing data.
The results here also depend on the value adopted in that paper but no
further adjustment was made to achieve the agreement shown here.
© European Southern Observatory (ESO) 2000
Online publication: January 29, 2001
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