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There is one file in this section:
SWAA SWS Auto-Analysis Results
The AAR files contain primary headers described in Table
9.11. In this table example information is used to fill the
header.
Most keywords are self explanatory, or have been described above. Those that
are not include:
- INSTRA
- This, along with INSTDEC and INSTROLL, are described in the ISO
DUM .
Header keyword | Contents | Comment |
SIMPLE = | T | / |
BITPIX = | 8 | / |
NAXIS = | 0 | / |
EXTEND = | T | / |
ORIGIN = | 'ESA ' | / European Space Agency |
TELESCOP = | 'ISO ' | / Infrared Space Observatory |
INSTRUME = | 'SWS ' | / Instrument used |
COMMENT | | SWS Auto Analysis Results |
FILENAME = | 'SWAA26400248' | / File name in ISO archive |
DATE = | '17/10/95' | / Creation date 95/290 |
FILEVERS = | '0399 ' | / Version ID in ISO archive |
OLPVERS = | 'LATEST ' | / SOC OLP system version |
USERNAME = | 'JSTERNBE' | / Unofficial data product |
OBJECT = | 'TEST_OBJ' | / Target ID as given by proposer |
OBSERVER = | 'KLEECH' | / Proposer ID in ISO Mission DB |
EQUINOX = | 2000.0 | / Equinox |
TMRATE = | 32 | / Telemetry rate in Kbps (Kbits/sec) |
EOHAUTCS = | '96166223020' | / Approx. UTC of start of observation |
EOHAUTCE = | '96166223818' | / Approx. UTC of end of observation |
EOHAAOTN = | 'S07 ' | / AOT name |
EOHAPLID = | 'KL_TEST' | / Proposal ID |
EOHAOSN = | '48 ' | / Observation sequence number |
EOHAPSN = | '0 ' | / Pointing sequence number |
EOHAPCAT = | '1 ' | / Proposal category |
EOHACIND = | ' ' | / Calibration indicator |
EOHATTYP = | '2 ' | / Target type |
ATTUTCSL = | '96166222532' | / UTC of start time of slew to intended target |
ATTUTCS = | '96166222627' | / UTC of time of first arrival at intended target |
ATTOTFTH = | 10.0 | / On-target flag threshold (arc secs) |
ATTRA = | 102.66 | / Intended Right Ascension of instrument viewing |
ATTDEC = | 27.8 | / Intended DEClination (with ATTRA) |
ATTTYPE = | 'P ' | / Type of attitude operation (P/R/T) |
ATTGUIDE = | 150002 | / Guide star reference number |
ATTSAANG = | 115.9 | / Solar aspect angle (degrees) |
ATTERROR = | 2 | / CONTINGEncy flag(0=success; 1=target not acq'd) |
TREFUTC1 = | 235175420 | / UTC (whole seconds since 01-01-1989) |
TREFUTC2 = | 8505250 | / UTC (remaining fraction of second) |
TREFUTK = | 1857816480 | / ISO Uniform Time Key (UTK) |
TREFITK = | 1857816480 | / ISO INSTRUMENT Time Key (ITK) |
TREFITKU = | 0.04166666666667 | / ITK unit length in seconds |
TREFCOR1 = | 235175420 | /UTC of 1st reference time |
TREFHEL1 = | -253.41 | /Heliocentric correction +(s) at TREFCOR1 |
TREFDOP1 = | -13.92 | /ISO velocity towards target (km/s) at TREFCOR1 |
TREFCOR2 = | 235175659 | /UTC of 2nd reference time |
TREFHEL2 = | -253.40 | /Heliocentric correction +(s) at TREFCOR2 |
TREFDOP2 = | -13.93 | /ISO velocity towards target (km/s) at TREFCOR2 |
TREFCOR3 = | 235175898 | /UTC of 3rd reference time |
TREFHEL3 = | -253.39 | /Heliocentric correction +(s) at TREFCOR3 |
TREFDOP3 = | -13.94 | /ISO velocity towards target (km/s) at TREFCOR3 |
INSTRA = | 102.66474 | /Reference instrument J2000 right ascension (deg) |
INSTDEC = | +27.81240 | /Reference instrument J2000 declination (deg) |
INSTROLL = | 318.89 | /Reference instrument J2000 roll angle (deg) |
VERS1 = | '0399/SWSP26400248' | / Version ID of each input file |
VERS2 = | '0388/SC03' | / Version ID of each input file |
VERS3 = | '0388/SC21_1' | / Version ID of each input file |
VERS4 = | '0388/SC21_2' | / Version ID of each input file |
VERS5 = | '0388/SC21_4' | / Version ID of each input file |
VERS6 = | '0388/SC21_8' | / Version ID of each input file |
VERS7 = | '0388/SC13' | / Version ID of each input file |
VERS8 = | '0388/SC25_1A' | / Version ID of each input file |
VERS9 = | '0388/SC25_3A' | / Version ID of each input file |
VERS10 = | '0388/SC25_5B' | / Version ID of each input file |
Table 9.11: AAR primary headers
The AAR file contains records with the fields described in Table 9.12.
In the FITS file they are defined in the binary header.
Field name | Number | Format | Unit | Comment |
SWAAWAVE | 1 | R*4 | | Wavelength of data point |
SWAAFLUX | 1 | R*4 | Jy | Flux |
SWAASTDV | 1 | R*4 | Jy | Standard deviation of the flux |
SWAATINT | 1 | I*4 | sec | Total integration time |
SWAADETN | 1 | I*4 | | detector number |
SWAAITK | 1 | I*4 | | SWS instrument time key |
SWAAUTK | 1 | I*4 | | ISO uniform time key |
SWAARPID | 2 | I*1 | | raster point id |
SWAASPAR | 2 | I*1 | | spare |
SWAALINE | 1 | I*4 | | line number |
SWAASDIR | 1 | I*4 | | scan direction |
SWAASCNT | 1 | I*4 | | scan number |
SWAASTAT | 1 | I*4 | | status word |
SWAAFLAG | 1 | I*4 | | flag word |
Table 9.12: AAR file
Notes
- 1
- The total integration time, SWAATINT, is the total time taken into
account to calculate this data point. See section 8.3.8 for a
definition of this.
- 2
- SWAADETN can be used to find which detector observed each point by
referring to table 3.1.
- 3
- SWAARPID, the raster point id, is copied over from the
GPSCRPID in the SPD. It is always (1,1) (unless a Solar System
Object is being tracked) (but see section 2.9, ``Caveats'',
point 6), as SWS has no raster AOTs, but is included so that the format of SWS
AA is compatible with LWS AA.
- 4
- See section 9.4.2 for a discussion of SWAALINE and
SWAASCNT.
- 5
- SWAASDIR is used to identify if the datapoint is from an up-scan (1)
or a down scan (-1). 0 is undefined (and don't use the data). See section
8.3.6 for a definition of up-down scans .
- 6
- SWAASTAT is copied over from SWSPSTAT . For a
description of this see Table 9.7.
- 7
- SWAAFLAG is copied over from SWSPFLAG . For a
description of this see Table 9.8.
SWAALINE and SWAASCNT are both counts of the valid data present in an AAR.
SWAALINE is a count of the valid ranges in a dataset. For AOT 1 ,
it is filled with the AOT band number. For an AOT 2 observing
X lines it will count from 1 to X, with 0 reserved for any
datapoints not associated with a line. Note that the datapoints associated with
SWAALINE set to, e.g. 1, may not correspond to the first entered line number
in your AOT as the logic may re-arrange them to increase efficiency. For AOT
6 it counts the number of scans, for an example see table
9.13.
Operation | line number for detector band |
| 1 | 2 | 3 | 4 |
REF | 1 | 2 | 3 | 4 |
SCAN UP | 5 | 6 | 7 | 8 |
REF | 9 | 10 | 11 | 12 |
SCAN DOWN | 13 | 14 | 15 | 16 |
REF | 17 | 18 | 19 | 20 |
. | . | . | . | . |
Table 9.13: Line number against detector band
Note that the scans may be different for a different AOT 6 operation.
SWAASCNT has nothing to do with the number of scans required for an AOT. It is
a count of the number of lines/bands containing requested (i.e. what was
requested in the AOT) data, starting with 1. Any data outside the requested
ranges will have SWAASCNT set to 0. Note that even if SWAASCNT is greater than
0, the flag and status word should be checked to ensure the data is okay. For
AOT 1 SWAASCNT is filled with 1.
The decision whether to increment SWAALINE or SWAASCNT depends on whether
a scan starts and ends at the same grating position as the preceeding scan.
Initially both are set to one. If a scan starts and ends at the same grating
position as the preceeding scan the line counter is not incremented but the
scan counter is. If the wavelength range is different the line counter is
incremented and the scan counter is (re-)set to one.
A slight problem exists in the counting of SWAALINE in that the counter can
count up too much, resulting in a higher count than the number of lines. This
will be fixed in a later release of OLP.
Next: 9.5 Calibration-G files
Up: 9 Product Description
Previous: 9.3 Standard processed (SPD)
K. Leech with contributions from
the SWS Instrument Dedicated Team (SIDT)
and the SWS Instrument Support Team (SIST)