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3. Relative calibration

In Sect. 2 we have shown that, in the absence of an accurate a-priori knowledge of the Galactic emission, absolute calibration can be done on time scales of several days. It is important then to address the question of the relative calibration, i.e., to estimate at what level one can control the radiometer gain stability over a time scale of hours or days.

For relative calibration, the accurate knowledge of the observed signals is not critical, as long as it is highly stable within the time scale of interest. By repeatedly observing a stable signal difference tex2html_wrap_inline1808 one can monitor long-term gain changes. If a gain drift tex2html_wrap_inline1810 in a time scale tex2html_wrap_inline1812 is occurring, the instrument will measure at time tex2html_wrap_inline1814 a signal difference tex2html_wrap_inline1816, and at time tex2html_wrap_inline1818 a signal difference tex2html_wrap_inline1820. Assuming a well balanced differential system, the measured change in the signal difference is related to the gain change by
equation523
From Eq. (5), the accuracy with which one can account for variations in the gain is:
equation527
where tex2html_wrap_inline1822 is the rms noise associated with the measurement of tex2html_wrap_inline1824, according to Eq. (6). So we obtain:
equation536
Equation (8), as expected, reduces to Eq. (20) when tex2html_wrap_inline1826, since in this case the accuracy of the calibration load temperatures is not relevant.

The time scale of the expected gain drifts depends on the source of instability. Gain variations can be due to thermal changes or can be intrinsic of the detectors. The differential receiver minimizes the effect of intrinsic 1/f noise. In addition, residual effects on time scales < 2 hours are averaged out by the large number (typically tex2html_wrap_inline1832) of successive measurements of the same sky pixel (observed by different radiometers at a given frequency), with the net effect of a small increase of the nominal white noise level of the receivers (e.g. Janssen et al. 1996). Our main concern here is then our ability of tracing slow drifts due to residual 1/f noise on time-scales >2 hours. Laboratory measurements suggest that one may expect gain variations of order tex2html_wrap_inline1838 in few hours, or tex2html_wrap_inline1840 in tex2html_wrap_inline1842 hours (Weinreb 1996).

Possible thermal effects on the gain are quite small, thanks to the choice of the L2 orbit and scanning technique. Thermal variations can only arise due to re-pointing maneuvers away from the anti-sun direction. A thermal study (Bersanelli et al. 1996) shows that any temperature drifts at the focal plane will be dominated by a slowly varying component with a time-scale of tex2html_wrap_inline1844 hours, so that for time scales tex2html_wrap_inline1846 hours thermal effects can be considered linear. Thermal effects on the gain are expected only at a level tex2html_wrap_inline1848 in the 100 hours period.

We have simulated the presence of a linear drift in the noise-added data stream with a rate of tex2html_wrap_inline1850 per hour. As shown in Sect. 1, in order to disentangle a gain drift from a baseline drift in the internal load (which will be discussed in the next section), we need to monitor signal differences rather than the signal intensity in a fixed pixel. We follow the circle described by the beam in two hours. The voltage associated to each pixel is
equation544
where G is the gain at an arbitrary time t=0, tex2html_wrap_inline1856 min, k=1,2,...120, and tex2html_wrap_inline1860 is the temperature relative to the internal load of the i-th pixel at time tex2html_wrap_inline1864 due to the Galaxy and the CMB dipole. We then evaluate tex2html_wrap_inline1866, the difference between tex2html_wrap_inline1868 and the signal of that pixel in the circle where the dipole is expected to provide the minimum contribution. We assume that the instrument response is stable during each spin period (1 minute). Since tex2html_wrap_inline1870, we can write:
equation551
Note that the load temperature (and its possible drift occurring on time scales tex2html_wrap_inline1872 min) has been eliminated. Now we can average the previous expression over a circle obtaining
equation556
where the notation tex2html_wrap_inline1874, N being the number of elements in a given circle. Note that in this case the Galactic emission provides additional modulation to the signal observed in each circle, thus contributing to the detection of gain drifts. We have then a set tex2html_wrap_inline1878 (and associated noise) with k=1,120, that we can fit to a linear law tex2html_wrap_inline1882. The ratio between the angular coefficient b and the zero-value a provides the estimate of the gain drift. Due to the slow gradient of the dipole, the time scale can be expanded up to tex2html_wrap_inline1888 successive circles with basically no additional uncertainty on the result. This allows to further averaging the values of tex2html_wrap_inline1890 already evaluated for each circle.

  figure563
Figure 6: Reconstruction of long-term gain drifts (relative calibration) from the closure pattern of the scanning technique. A drift tex2html_wrap_inline1892hour was added to the data. Here the results are presented for the drift as reconstructed in each 2-hour circle, corresponding to tex2html_wrap_inline1894 (dashed horizontal lines). Each point represents the simulation results based on 6 hours of observation. The regions of increased spread correspond to the periods when the scan geometry is such to have minimum sky signal modulation within the observed circle

The results of our calculations are presented in Fig. 6 (click here) for the four LFI frequencies. Each point in the plot represents the algorithm reconstruction of a drift of 0.25% per hour (or 0.5% per circle) based on 6 consecutive circles (corresponding to 12 hours of data). Again, the accuracy of the results is degraded significantly in the two periods of the year when tex2html_wrap_inline1896 is smaller due to the geometry of the CMB dipole, which dominates in general over the Galaxy. On average, however, it is apparent that the relative calibration allows to recover the gain drift with high accuracy at all frequencies, with a typical uncertainty of less than tex2html_wrap_inline1898 on G for the assumed 12 hours time scale. Our simulations show that this result is nearly independent of the amplitude of the assumed drift.

This demonstrates that even in the absence of frequent absolute calibration, relative calibration can provide an accurate monitor of the long-term gain stability.


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