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The SWS calibration is carried out in two phases: ground calibration
and in-flight calibration .
Due to the viewing constraints of the ISO satellite and for scheduling
reasons, it is not possible for the observer
to directly tie a science observation to
an immediately following observation of an astronomical calibrator.
Instead, internal calibration sources provide both flux and wavelength
references for science observations, and these internal references are
tied to astronomical standards by means of a dedicated calibration
programme planned and executed by the Science Operation Team and the SWS
consortium.
In particular, the internal calibrators will be used to monitor the
responsitivity variations of the detectors. They bridge the gap between
on-ground and in-flight calibration .
The calibrations include:
- Determination of focal plane geometry, array geometry and
alignment. The relative positions of the various entrance apertures and
detectors need to be known to ensure that one grating wavelength
calibration can be applied to all combinations of entrance slit and
detector. The respective offsets have been calibrated in instrument level
tests on the ground. Beam profile measurements and wavelength calibrations on astronomical sources were used for
in-orbit checks - it was such calibrations that found the need for the virtual
aperture 4.
- Determination of wavelength scales .
In ground-based instrument level tests,
the relation between grating position readout and physical grating angle
has been determined by measurement of wavelength references in the form of
vapour absorption lines (H O, NH , HCl). The spectral features provided
by the internal
grating wavelength calibrator have been tied to that scale. For the
Fabry-Pérot, the position-gap relation has been determined from the
spectrum of the internal F-P wavelength calibrator, which is known to high
accuracy from fourier transform spectroscopy. H O and NH vapour
absorption lines have
been used for additional checks and for determination of the variation of
effective F-P gap with wavelength. In orbit, the grating
position-angle relation and the F-P position-gap relation will be
re-established first using the internal calibrators and then astronomical
sources.
- Determination of photometric sensitivity .
The photometric sensitivity has been determined on ground by scanning the
spectrum of a calibrated blackbody source within the test cryostat. These
tests resulted both in detailed spectral response functions for
the various AOT bands and in a first calibration of the signal created
by the internal stimulators. The signal from the stimulators will be used
to monitor variations in the broad band sensitivity of the detectors, e.g.
due to memory effects. In orbit, an extensive program will be executed to
determine the photometric sensitivity on astronomical sources.
The dark current measurements needed both on ground and
in orbit are done with SWS shutter closed.
The procedures for SWS calibration are developed in more detail in the
ISO In Orbit Calibration Requirements Document (IOCRD), Ref. ISO-SSD-9003.
Next: Astronomical Calibration Sources
Up: Calibration
Previous: Calibration
SWS Consortium
Wed Aug 7 17:20:29 MET DST 1996