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Subsections


7.4 In-band power calibration  

Detailed description: section 5, 4.5.4

The steps described in this section are applied to all astronomical measurements except those collected with PHT-S. The PHT-S SPD processing finishes without this last step.

The detector responsivity varies along a revolution, in particular the long wavelength detectors P3, C100, and C200 show significant variations. To guard against such drifts, all PHT AOTs except P40 contain at least one FCS measurement per detector that has been used during an AOT. The FCS measurement determines the responsivity of the detector at approximately the same time as the sky is observed.

The derivation of the target's in-band power using the FCS calibration requires important instrumental corrections to ensure the best photometric calibration. The related processing steps are described in the following sections.

7.4.1 Determination in-band power from FCS  

Detailed description: section 5

The electrical heating power p applied to the FCS directly corresponds to an FCS power on the detector PFCS. The conversion is obtained from dedicated in-orbit FCS calibration observations where the signal of a calibration source is directly compared with the signal of the FCS for a given heating power p. However, the calibration observations could only cover a limited range in p due to limited availability of suitable calibration targets. FCS measurements with values for p outside the calibratable range will get unreliable PFCS based on extrapolations.

In Derive_SPD the value for p is checked. In case the value is outside the valid range an extrapolated value for PFCS will be retrieved, and a warning will be issued in the SPD file header.

Ancillary data required:

The valid heating power ranges are included in the FCS power calibration Cal G files PPxFCSPOW (x=1,2,3) for the P detectors, and PCxFCSPOW (x=1,2) for the C100 and C200 detectors, see section 13.10.

7.4.2 Signal to in-band power conversion for P detectors  

Detailed description:5.2.3

From the electrical power (in mW) applied to the FCS, an in-band power on the detector PFCS normalized to the aperture area (in ${\rm W/mm^2}$)is obtained using FCS calibration tables, see Chapter 5. The FCS measurement provides the detector responsivity R:

 
 \begin{displaymath}
R = \frac{{\langle s_{FCS} \rangle}\cdot{C_{det}}}
 {P_{FCS}{\cdot}A_{FCS}}~~~~~~~~~~A/W,\end{displaymath} (7.14)

where

The in-band power Ptarget is obtained by:

 
 \begin{displaymath}
P_{target} = \frac{\langle s_{target} \rangle C_{int}^{det}}{R}~~~~~~~~~W,\end{displaymath} (7.15)

and

 
 \begin{displaymath}
{\Delta}P_{target} = \frac{{\Delta}\langle s_{target} \rangle}
 {\langle s_{target} \rangle}
 P_{target}~~~~~~~~~W,\end{displaymath} (7.16)

where Ptarget and $\langle s_{target} \rangle$ can refer to any filter in a multi-filter sequence taken with detector P1, P2, or P3. Cintdet is the capacitance of the detector.

Caveat:  In principle, inhomogeneous illumination by the FCS (see section 7.4.3) affects the calibration involving apertures. The FCS power on the detector is not proportional with aperture area for a given electical power applied to the FCS. Although the correction method has been implemented in OLP Version 7, the present version of the Cal G files provide no correction. The investigations are ongoing, and non-unity correction factors are expected in a future version of the calibration files. 

Ancillary data required:

7.4.3 Signal to-in band power conversion for C detectors  

Detailed description: section 5.2.3

The detector flat-field or pixel-to-pixel variation in the PHT-C responsivity is found to be filter dependent. Correction for the pixel-to-pixel variation is in principle taken care of by the FCS measurement which determines the responsivity for each individual pixel. However, for a multi-filter observation the FCS measurement is done in only one filter. Therefore a correction is necessary that relate the flat field obtained from the FCS measurement with those in the other filter bands.

Firstly, the FCS measurement is used to determine the responsivity of each pixel R(i) for the filter in which the FCS measurement is taken:

 
 \begin{displaymath}
R(i) = \frac {\langle s_{FCS}(i,f) \rangle \cdot C_{int}^{det}}
 {P_{FCS}(p,f) \cdot {\Gamma}(i,f) \cdot {\chi}(i,f)}~~~A/W,\end{displaymath} (7.17)

where

The illumination matrix ${\Gamma}(i,f)$ is needed to correct for the fact that the FCS illumination is not flat but varies from pixel to pixel in the C100 and C200 arrays. This correction is applied to each pixel in the array with respect to a reference pixel for which the FCS calibration tables apply (section 4.5.4).

Secondly, the power on each pixel for any filter f' can be derived from the mean signal per chopper plateau $\langle s_{target}(i,f') \rangle$:

 
 \begin{displaymath}
P_{target}(i,f')\,=\,\frac {\langle s_{target}(i,f') \rangle \cdot
 C_{int}^{det}}{R(i) \cdot \chi(i,f')}~~~~~W,\end{displaymath} (7.18)

and

 
 \begin{displaymath}
{\Delta}P_{target}(i,f') = \frac {{\Delta}\langle s_{target}...
 ...e}
 {\langle s_{target}(i,f') \rangle}
 P_{target}(i,f')~~~~~W.\end{displaymath} (7.19)

Ancillary data required:

7.4.4 In-band power for raster maps

Detailed description: None

In case of a raster map, two FCS measurements are collected: one at the beginning and one at the end of the map. It is assumed that differences between the derived responsivities of the two FCS measurements can be attributed to a detector responsivity drift which is linear in time. In order to compute the detector responsivity at the mean time of the plateau signal a linear interpolation in time between the two FCS signals is performed for the P detectors, and a linear interpolation in time between the two responsivities R(i) is performed for the C detectors (cf. eqn. 7.18).

Ancillary data required:

None

7.4.5 Default responsivities  

Detailed description: None

It can happen that one or more FCS measurements are of insufficient quality for the derivation of a reliable detector responsivities. Such an event occurs e.g. in case all ramps/signals during the FCS measurement were rejected due to saturation or glitches.

For all chopped observations using the PHT03, PHT04 and PHT22 AOTs, the detector responsivity that can be derived from the chopped FCS measurement is assumed to be too unreliable for further use. In the current version of PHT-OLP the default responsivity is used for the in-band power calibration.

The default responsivity is time dependent and depends on the orbital phase of an measurement. For each measurement the orbital phase is read from ERD keyword TREFCOR2 which gives the orbital phase corresponding to the mid point of an AOT, and the default responsivity is determined by linear interpolation in the Cal G file which gives the default responsivity versus orbital position for a given detector.

Derive_SPD will also compute the FCS1 responsivity from the FCS measurement and the results are stored in the designated Cal A file. To give the observer some information on the discrepancies, the ratio:

\begin{displaymath}
r(i) = \frac {R_{FCS}(i)}{R_{default}(i)},\end{displaymath} (7.20)

is stored for each pixel i in the SPD header with keyword RESPRi.

Ancillary data required:

Default detector responsivities are stored in Cal G files PPRESP, PC1RESP, and PC2RESP for the P, C100 and C200 subsystems, respectively, see section 13.11.

7.4.6 Dependencies on mission dates  

Detailed description: None

During the mission two main events took place which seriously impacted on the ISOPHOT calibration:

As a consequence, the following calibration files have different entries depending on the revolution date:

Ancillary data required:

Information on the time dependence of ISOPHOT Cal G files is stored in Cal G file PTIMEDEP, a detailed description is given in section 13.2.


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Next: 7.5 Quality flags for Up: 7 Data Processing Level: Previous: 7.3 Signal Processing

ISOPHOT Data Users Manual, Version 4.1, SAI/95-220/Dc