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        VISIR USER MANUAL
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1.                 3 0  Calibration Units  db ra ea kee se be A ew ee en  A a NN  3 8  Data dcquisilon  system  2 aa ze rd A ih    4 Observing with VISIR at the VLT    Al  Proposa prepaid Okee 228  ALLA EEE ee ee A  4 2 Telescope observing parameters                                  4 2 1 Instrument orientation on the sky                            4 2 2 Chopping parameters   2 286 6 4424 u BA a ds asie EH  4 2 3 Nodding parameters za    2  04 same MN Las t  s  BD FON CL aOQUISILOA ee y e A A ee DE ea Ro E E  Aw   Guide stars a Ed AE ws  Alo  Brichtness Imitat  ons  ee 3   ns aa a anA a a EE a  ALO ONCE eS ee re een ee ade Ge  Ar  Calnbrabion observations oa s auie ada ta MN de A Re  4 8  ARONA Problems  AA as a e Dis  4 8 1 Decreased image quality ar 4 ac 34 hod ica BA a A do e  4 82 kLow levelsttipes  ss mmm dr BS Gus ee Oh A Kb a ne  4S3   Bad tesiduals roer a a da A o ee dd  4 8 4 Residuals of sky emission lines    a 4 4   24 iia a id  AS  SEID  yc Sag ae ely oy at As oe Ge He A ES BS he A G  5 VISIR data  O a fee acne ae ee ei Eee ee ee See nie  Ds PpO as cries oe mn ne ah rede Be ke ee ec SS et e ea    9 3  VISIR spectrometer data a LEE he aa Fe hee eda OPS SEES be eee eS  6 VISIR templates description  Dal  Ze OED    dt ea  oe  tae ee eet    ee ee A ek a  GS ee eee ade ee ee E  6 2  Observing with the imager   22     425 ei da seu ESE FEES S S34 TOE oe ws  6 3 Observing with the spectrometer     a  aooo m nn  Ode  Cal  br sl on  a2 at oS  2 ann a ee ee ee ee a ee a    7 C
2.   A checklist  to help the preparation of OBs is available in 37  Acquisition  observing and calibration templates  are explained in 8 6     This manual reflects knowledge gathered during early phases of operations and is in some aspects to  be considered to be preliminary  Therefore we strongly recommend to consult   http   www eso org instruments visir  for additional information and updates  For support  during proposal preparation and OB submission  please contact ESO   s User Support Department   usd help eso org         2 Observing in the MIR from the ground    2 1 The Earth   s atmosphere    Our atmosphere absorbs the majority of the MIR radiation from astronomical sources  The main  absorbing molecules are H20  CH4  CO2  CO  O2  O3  However  the atmosphere is quite transparent  in the two atmospheric windows  the N and Q band  They are centered around 10 and 20 um   respectively     The transmission in the N band is fairly good at a dry site and becomes particular  transparent in the wavelength range 10 5 12 ym   However  the transmission of the Q band is rapidly  decreasing with wavelength and can be viewed as the superposition of many sub bands having a  typical spectral coverage of AA   lum at an average transmission of 60   Observations in this band  require low water vapor content in the atmosphere  The atmospheric transmission in the N and Q  bands is displayed on Fig  1        2 2 The spatial resolution    The spatial resolution of an instrument is ultimately l
3.   To avoid chopping inside the object it is recommended to use a chopping and nodding  throw which is   1 5 times larger than the estimated MIR diameter of the object  In the case of point  sources  the throw is usually set around  10    to ensure proper separation of the different beams  The  maximum chopping throw at the VLT is 30    and the minimum is 8     For good image quality  and  good background cancelation  chopping and nodding throws below 15    are recommended  see    4 8 1    Note that for chopping throws larger than the field of view  the negative beams will not be seen on the  detector  and the integration times have to be adjusted accordingly    The chopper position angle  TEL CHOP POSANG  is the angle of chopping counted East of North  see  Fig  16   This parameter can be set by the observer  In order to keep the same distribution of  beams on the detector for a different rotator angle  TEL ROT OFFANGLE  as in the default rotator  position  then TEL CHOP POSANG must be equal to TEL ROT OFFANGLE  In particular  this is the case  in spectroscopy if the observer wishes to have the 3 beams along the slit    As stated in Sect 3 5  the chopping frequency is not a parameter accessible to the observer  it is fixed  internally to ensure the best data quality        Figure 16  Definition of chopping parameters from the telescope point of view  If the position an   gle  PA  is measured counter clockwise from North to East with PA between 0 and 360    then  TEL CHOP POSA
4.  PERPENDICU   LAR  PARALLEL    0  10  0    180  3600  NODEFAULT   0  359  0    8  30  8     Imager pixel scale  Observation Category    Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_img_obs_GenericChopNod tsf    To be specified   Range  Default    INS FILT1 NAME    INS PFOV  SEQ CATG    SEQ  JITTER WIDTH  SEQ NOFF  SEQ OFFSET COORDS    SEQ OFFSET1 LIST  SEQ OFFSET2 LIST  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    SIC PAH  ARII SIV_1 SIV  SIV2 PAH2 PAH22 NEIL1  NEII NEII_2 Q1 Q2 Q3  NODE   FAULT    0 075 0 127  0 127   PRE IMAGE SCIENCE  SCI   ENCE    0  10  0    1  100  NODEFAULT    SKY DETECTOR  NODE   FAULT     NODEFAULT    NODEFAULT    180  3600  NODEFAULT   0  359  0    8  30  10     Imager Filter    Imager pixel scale  Observation Category    Random Jitter Width  arcsec   Number of offset positions  Offset coordinates    List of offsets in RA or X   List of offsets in DEC or Y  Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_obs_LRAutoChopNod tsf    To be specified     Range  Default    INS GRAT1 WLEN  SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    8 5 8 8 9 8 11 4 12 2 12 4  NODE   FAULT     PARALLEL PERPENDICU     LAR  PARALLEL    0  10  0    180  3600  NODEFAULT   0  359  0    8  30  8     Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    R
5.  This limit is particularly constraining for VISIR spectroscopic observations  All acquisition  images are recorded and archived     As part of the execution of the VISIR_spec_acq_MoveToSlit template  an image used to measure  the slit location is always taken and archived  In service mode  through slit images are also taken  and archived so that the user can assess the correct centering of her his object  The slit location  image and the through slit images are automatic procedures that cannot be modified by a  service mode observer  Their execution time is included in the advertised execution time of the  spectroscopic acquisition template        e If the target coordinates are well known  VISIR imaging modes allow to perform blind preset  observations with the VISIR_img_acg Preset template  In this case  no acquisition images are  taken  The target will be located at the center of the detector with an accuracy limited by the  accuracy of the guide star  typically 1     RMS   If both the target coordinates and the guide  star ones are within the same astrometric systems  the pointing accuracy is limited by the rel   ative accuracy between the coordinates of the two objects  In particular  the pointing accuracy  maybe affected by significant  usually unknown  proper motion of the guide star  Note that the  observatory does not guarantee the accuracy of the world coordinate systems  WCS  keywords  in the FITS headers     For a successful completion of an OB  the observer has 
6.  a  y    sign e     Re     yR   x           9   9     and along the dispersion     fs v y     x  sign A     Ra     yR     y   y     A 40   10     Finally  the origin of the coordinate system is moved back from the fix point to  1 1      VISIR User Manual 26    fole  y       Ey E   11        Spectral extraction is similar to the TIMMI2 pipeline and described by Siebenmorgen et al  2004  AA  414  123     Wavelength calibration   A first order wavelength calibration is given by the optical model of the instrument  Its precision  is about  10 pixels for the low and medium resolution mode and  15 pixels for the high resolution  mode  The wavelength calibration can be refined by using Fabry Perot Etalons plates or atmospheric  lines  In the VISIR FITS file  chopper half cycle frames  which are dominated by sky emission lines   are stored  85 1   They can be used to fine tune the wavelength calibration to sub pixel precision  by comparison with a model of the atmospheric lines  This method is used by the pipeline  More  specifically  the zero point of the wavelength calibration is obtained by cross   correlating the observed  sky spectrum with a HITRAN model of the sky emission lines    The chopped frames cannot be used for calibration with atmospheric lines because the chopping pro   cess results in a near perfect cancelation of sky lines        Atmosphere absorption correction   The atmosphere does not uniformly absorb the MIR radiation  3 2 1   At some wavelengths it is com   ple
7.  crossing should be avoided  because of fast  tracking speeds that do not allow proper background cancelation after nodding    Questions related to the VISIR Phasel and Phase 2 observing preparation should be directed to the  User Support Department  usd help eso org      4 2    Telescope observing parameters  4 2 1 Instrument orientation on the sky    By default  the imager orientation is such that North is at the top and East is to the left  For the  spectrometer  the default orientation is rotated by 90   respective to the imager  so that the North is  to the left and the East to the bottom  with the slit orientation along the North South direction    Since VISIR is mounted on a rotator at the Cassegrain focus of Melipal  it is possible to change the  default orientation of VISIR on the sky  for example  to obtain the spectra of two objects at once   The parameter TEL ROT OFFANGLE  defaulted to 0    is used for this purpose  If PA represents the    VISIR User Manual 18    required position angle on the sky east of north  i e   counted positively from north to east  within  the range O to 360    then  TEL ROT OFFANGLE   360     PA    4 2 2 Chopping parameters    The chopping technique  as described in 32  is based on beam switching using the moving secondary  mirror of the telescope  It allows to alternatively observe a field  then another field offset from the  first by a chopping distance or throw  called TEL CHOP THROW  see Fig  16  This parameter can be set  by the user
8.  during the night  84 7   Flux and noise levels  are extracted by multi aperture photometry using the curve of growth method  the aperture used for  all 4 beams in a given frame is the one for which the flux to noise ratio is the largest  By combining  all 4 beams  the sensitivity in a given set up  filter  field of view  is defined as the limiting flux of a  point source detected with a S N of 10 in one hour of on source integration    The growing calibration database allows a statistical analysis of the sensitivity with respect to instru   mental and atmospherical conditions  The values for each filter given in Table 2 refer to the median of  more than 600 different observations during September and December 2004  A graphical compilation  is presented in Fig  4 for the N band and Q band imaging filters  Some of the best measurements  approach theoretical expectations  i e  they are close to background limited performance  BLIP    Sensitivity estimates for the VISIR spectroscopy observing modes are obtained in a similar way   However  in this case  chopping and nodding are executed in parallel  Consequently  only 3 beams are       VISIR User Manual 4    Staring images Staring images  n    chopper position    Chopped images    subircaction    subtraction    Han     B chopper position    Sketch of mid infrared    chopping and nodding    technique of observation    Chopped nodded image Final Image  zoomed    He2 16 blue compact galaxy        Figure 3  Illustration of the choppi
9.  offsets  and allows the user to specify them  in a list of relative offset positions  In the most simple application  only one offset position is specified   This allows to record nodding pairs  i e  cycle of on   off observations  using a flexible offset position   Additional jitter offsets can be specified  More than one entry in the offset list results in a freely  programmable pattern of nodding pairs  Note that the integration time  SEQ TIME  specified refers  to only one nodding pair  The total observing time is given by the product of SEQ NOFFbySEQ TIME   The offset positions are calculated as the cumulative sum of offsets  i e  are defined relative to the  previous offset positions  Note that the telescope always returns to the first  reference  position  when  specifying a list of offsets  This mode can be exploited to perform mosaic or raster imaging  The  first reference position can then be considered as a sky observation while the offsets refer to object  positions  It is recommended to offset to positions that result in observations of overlapping fields   which enhances the redundancy after image reconstruction                  Nodding Position B1    Nodding Position B2    Nodding Position B3    Preset Reference Position A    Figure 20  Illustration of generating raster maps with VISIR_img_obs_GenericChopNod     An illustration of generating an raster map can be found in Fig  20  The following parameters  correspond to this setting     SEQ   NOFF 3  SEQ OFFSET
10.  tt  Ne H 7 att 4  amp  wt     7 a we 9 6 2 a  X     i att   NE DX E   at      Lasa i ve     1 5x10 ae  7 7 a D 1 35x100 2   5x10 AE  gt  ra  x H r   4  e    S  7 O Z  E         10x10 E uo   EEn o Ka    TS L 7 al  gt  a           a  x B a      x   e   a E a           va  be 6   a   5    y ORO   ae E o 5 0x10  j va    NY H Pal A Sen 2  oO E pe A D a  En F eo 7 rid  O L at J O    at Cc  7  E O   po O E AA AP AI A fen E E  0 2 4 6 8 0 0 0 2 0 4 0 6 0 8 1 0  integration time  s  integration time  s     Figure 11  Linearity curve of the detector in the large  left  and small  right  capacity modes  The  break in the response at   2 3 at 1 8  10    e    of the large and at 1 9   10  e    of the small capacity are  indicated by full lines  The top lines indicate the well capacities        Figure 12  Bad pixel maps of the imager  left  and spectrometer  right  detectors  The large grey  rectangular areas correspond to electronically masked pixels in order to decrease detector striping        VISIR User Manual 15       Figure 13  The DRS detector shows stripes and repeating ghosts for very bright sources  left   The  ghosts are distributed every 16 columns  For other sources striping is not apparent  right         Figure 14  Sequence of chop nod  reduced spectra obtained in the Medium Resolution mode with a  central wavelength   8 8um   The TEL CHOP THROW   8  11  13 and 14    from left to right  Note  the presence of significant striping when the    left    beam hits some hot pixels 
11.  type   standard star in the Low Resolution mode  based on the same catalog as for imaging with an  airmass difference no larger than 0 2 AM  Such a calibration measurement will be performed at  least once per night  per instrument configuration  More precisely the following settings of the  VISIR_spec_cal_LRAutoChopNod template    6  will be used        SEQ  TIME 180 sec  TEL   CHOP   POSANG 0    TEL   CHOP   THROW 8       SEQ CHOPNOD DIR PARALLEL    The wavelength setting INS GRAT1 WLEN and INS SLIT1 WIDTH will be adjusted to the science obser   vation     Important note    The observatory does not provide standard calibrations for VISIR medium and high resolution spec   troscopy  Thus for medium and high resolution mode the observer has to supply his own calibration by  supplying a calibration OB to each science OB  The observing time needed to execute this calibration  is charged to the observer  Ideally  early type stars should be chosen     For both imaing and spectroscopy  day calibrations of VISIR are performed with an extended source  that mimics a black body with adjustable flux  by regulating its temperature   For each instrument  mode  a corresponding flat field is recorded  which consists of a series of images with different back   ground levels  Bad pixels  gain maps and fringing patterns can  in principle  be derived from these  flat fields  However  at the moment  the scientific value of the application of these corrections is not  established  Day calibration
12. 1 LIST 30 10 10  SEQ OFFSET2 LIST 30  10  10  SEQ   OFFSET  COORDS SKY    VISIR User Manual 29    Note that depending on choice of the integration time SEQ  TIME  several nodding cycles might result   e g  pattern like ABIBIAABIBI1A  AB2B2A AB2B2A  AB3B3A AB3B3A    Pre imaging observations  As of Period 76  the observatory supports a fast data release for VISIR pre   imaging observations  Pre imaging images must be obtained either with the VISIR_img_obs_AutoChopNod  or VISIR_img_obs_GenericChopNod templates  The SEQ CATG keyword must be set to PRE IMAGE    In addition  the name of the OB must start with the prefix PRE     6 3 Observing with the spectrometer    Conceptually the same observing techniques applies for spectroscopy as well as for imaging  The  default slit orientation is in North South direction  The length of the slit is selected by the keyword  INS SLIT1 TYPE  only for cross dispersed  high resolution  observations SHORT must be used  otherwise  LONG is the default setting    A preferred observing strategy is called    nodding on the slit     where the chopping and nodding  amplitudes are small  SEQ CHOPNOD DIR   PARALLEL   Note that    nodding on the slit    requires to  set the telescope rotator offset angle and the M2 chopping position angle to the same value  which is   in general  different from 0   This is useful to acquire two targets simultaneously in the slit    The keyword SEQ  JITTER WIDTH allows to apply random offsets along the slit    More complex 
13. AA line order spect  resol  dispersion sensitivity   um    um    theoretical   pixels um   Jy 100 1h  HR 7 970     8 270 0 02420  H254  17B 32000 10544 3  HR 12 738     12 882 0 03571  Ne I  11A 17000 1145 0 9  HR 16 800     17 200 0 05156  H2 Sl  8B 14000 4950  lt 10  HRX 9 360   9 690 0 02325  H253  15A 25000 10974 av   HRX 12 210   12 760 0 03864  H2 S2  11B 20000 6604 1 5    Table 6  VISIR high resolution long slit  HR  and cross dispersed  HRX  modes  The second column  gives the minimum and maximum allowed values for the central wavelength  Ac  in the given setting   The wavelength range per setting in given in the 3rd column  AA   Offered slits have widths of 0 40   0 75 and 1 00        VISIR User Manual 12       Figure 8  Schematic drawing of the warm calibration unit on top of the VISIR vessel     3 7 Detectors    The VISIR imager and spectrometer are each equipped with a DRS  former Boeing  256 x 256 BIB  detector  The quantum efficiency of the detectors is greater than 50  and reaches 65  or more at 12  um  Fig  9     The detector noise has to be compared with the photon noise of the background  As shown in Fig  10   the measured noise in an observation consists of read   out noise and fixed pattern noise  which are  both independent of the detector integration time  DIT   At the operating temperature of the detector     7K   the dark current  which is the signal obtained when the detector receives no photons  is  negligible compared to the background generated by 
14. EL  CHOP   THROW  along a  position angle equal to       e PA   90     360     TEL CHOP POSANG   90    if SEQ  CHOPNOD DIR   PERPENDICULAR   e PA   180     180     TEL CHOP POSANG  if SEQ  CHOPNOD DIR   PARALLEL     The resulting distribution of images on a frame is illustrated in Fig 19  In imaging  more flexibility  on the nodding offsets are possible with the VISIR_img_obs_GenericChopNod template     4 3 Target acquisition    Observing blocks must start with an acquisition template  Pointing to a target can only be performed  through an acquisition template  Target coordinate  name and proper motion are all set in the  acquisition templates    The execution of the acquisition templates presets the telescope to the target coordinate given by  TEL TARG  ALPHA and TEL TARG DELTA  Offsets with respect to the target coordinates can be specified  by TEL TARG OFFSETALPHA and TEL TARG OFFSETDELTA and allow  for example  to use a bright offset  star for precise acquisition  To guarantee proper centering within the slit when using an offset star  the  angular separation between the offset star and the target should not be larger than 60     Acquisition  with an offset star has not been tested with the narrow  0 4    slit and should be avoided in P76  Note  that the convention          TEL TARG ALPHA   TEL TARG OFFSETALPHA   RA  offsetstar     TEL TARG DELTA   TEL TARG OFFSETADELTA   DEC offsetstar     is used   The target can be further offset to a particular position on the detecto
15. EST FLAT      MSW    FOCUS  DETECTOR MECHANISM       Figure 7  Schematic layout of the design of the VISIR spectrometer     The long slits have a length of 32 5   and therefore cover the whole width of the detector  The short  slits  only used in high resolution  cross dispersed mode  have a length of 4 1     The all reflective  optical design of the spectrometer uses two TMA systems in double pass  pass 1  collimator  pass 2   camera   A schematic layout of the VISIR spectrometer design is shown in Fig  7  The 3 mirror system  of the low  and medium resolution arm gives a 53mm  diameter  collimated beam  the collimated  beam diameter in the high resolution arm is 125mm  Both subsystems image the spectrum onto  the same detector  selection between the two spectrometer arms is done by two pairs of folding flat  mirrors  In front of the actual spectrometer subsystems is a reflective re imager consisting of two  off axis paraboloids and three folding flats  The re imager provides a 16 mm diameter cold stop pupil  in parallel light and transforms the incoming VLT Cassegrain beam of F 13 4 to an F 10 beam at  the spectrometer entrance  The spectrometer slit wheel is also equipped with a very wide slit  15 3      named OPEN in P2PP  It gives the possibility to make imaging with the spectrometer detector and  is used for object acquisition and centering on the detector    The list of available filters for spectroscopic acquisition offered is given in Table 3  together with their  me
16. EUROPEAN SOUTHERN OBSERVATOR Y    Organisation Europ  enne pour des Recherches Astronomiques dans 1 H  misphere Austral  Europaische Organisation f  r astronomische Forschung in der s  dlichen Hemisphare       VERY LARGE TELESCOPE    VISIR USER MANUAL    Doc  No  VLT MAN ESO 14300 3514  Version 76 4    14 Jul 05    VISIR User Manual    Issue  Rev     04 09 04  10 12 04    01 02 05    06 07 05    14 07 05    14 07 05    Change Record    Section Parag  affected   Reason  Tnitiation Documents Remarks    creation First release for science verification  in P74 and OT proposals in P75    2 4  3 2  6 2  6 3  7  8 update for P75 Phase2   all update for P76 CfP    all update for P76 Phase 2       4 8 1 Corrected Legend Fig 17    Cover pages Corrected typos    v1 0  v1 1  v76 1  edited by R  Siebenmorgen  E  Pantin  M  Sterzik  v76 2 4  updated by A  Smette  Send comments to asmette eso org       11    VISIR User Manual    Contents  1 Introduction    2 Observing in the MIR from the ground    21 e arts at mosphere see a Ls ti d en A Re ee are  22   Thespalialiresolution o 5 8 AE Sr DREI as la de  23 MIR Pace oro Ud  a an  u e ee Bee OME RA a as de  22  Chopping and nodding e 3 Lames Lis a 80er RT Eee  2 D IN re ee A ee ee ees cee ne  3 Instrument description and offered observing modes  DL MAR  ES III  3222 SO PECLTOMCLOS  y ue SRE LAA RUN LAND AUS A ERR AA  39  com Midis    a A A ds  32 I Ol O A II E Sh SA era N open kit es S  3 5 Low resolution  offered central wavelengths            
17. NG is 360       PA  The positive beam     is obtained when the M2 is at Chopping  Position A and corresponds to the pointing position of the telescope as given in the FITS header  The  negative beam     is obtained by moving the M2 so that it points to a position angle on the sky given  by PA and a throw of TEL CHOP THROW from the telescope pointing position  Chopping Position  B   If TEL  CHOP POSANG   TEL ROT OFFANGLE   360     PA  the resulting image on the detector will  appear as in one of the nodding position images illustrated in Fig  19     2In practice  the telescope is actually given an offset equal to TEL CHOP THROW 2 along the angle given by PA   Relative to its idle position and looking from the M1 to the sky  the M2 oscillates along PA between two positions given  by   TEL CHOP THROW 2  This is completely transparent to the user     VISIR User Manual 19    4 2 3 Nodding parameters    The nodding technique allows to switch from one field to another by offsetting the telescope by several  tens of arc seconds  It allows to correct for optical path residuals that remain after chopping  8 2    The nodding period is 90s for exposure time equal or longer than 180s  or is half this value for shorter  exposure times  This parameter can only be modified by the instrument operator    In all the    AutoChopNod    templates  the nodding offset is equal to TEL   CHOP   THROW and cannot be  modified    In order to reach Nodding Position B  the telescope executes an offset of T
18. THROW    8 8 11 4  NODEFAULT     PARALLEL  PERPENDICU   LAR  PARALLEL    0  10  0    30  3600  NODEFAULT    0  359  0    8  30  8     Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_cal_HRAutoChopNod tsf    To be specified   Range Default    INS FILT2 NAME  INS GRAT1 WLEN    SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    NEIL2 H2S_1 H254  NELLA   7 80  19 18  12 810     PARALLEL PERPENDICU     LAR  PARALLEL   0  10  0    30  3600  NODEFAULT   0  359  0    8  30  8     Spectrometer Filter  Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR User Manual 36    VISIR spec_cal HRXAutoChopNod tsf    To be specified   Range Default    INS GRAT1 WLEN 7 60  28 08  VODEFA ULT  Spectrometer Wavelength  mi   crons     SEQ CHOPNOD DIR PARALLEL PERPENDICU    Relative Chop Nod Direction    LAR  PARALLEL   SEQ JITTER WIDTH 0  10  0  Random Jitter Width  arcsec   SEQ TIME 30  3600  NODEFAULT  Total integration time  sec   TEL CHOP POSANG 0  359  0  Chopping Position Angle  deg   TEL CHOP THROW 8  30  8  Chopping Amplitude  arcsec        VISIR User Manual 37    9 Appendix  Filter transmission curves    The filter transmission has been measured using a Four
19. andom Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR User Manual    34    VISIR spec_obs MRAutoChopNod tsf    To be specified   Range Default    8 8 11 4  NODEFAULT     INS GRAT1 WLEN  SEQ CHOPNOD DIR PARALLEL   PERPENDICU   LAR  PARALLEL    0  10  0    180  3600  NODEFAULT   0  359  0    8  30  8     SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_obs_HRAutoChopNod tsf    To be specified     Range  Default    INS FILT2 NAME  INS GRAT1 WLEN    NEIL2 H2S_1 H2S 4  NEILA   7 80  19 18  12 810   SEQ CHOPNOD DIR PARALLEL  PERPENDICU   LAR  PARALLEL    0  10  0    180  3600  NODEFAULT   0  359  0    8  30  8     SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    Spectrometer Filter  Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_obs_HRX AutoChopNod tsf    To be specified     Range  Default    INS GRAT1 WLEN 7 60  28 08  NODEFAULT     SEQ CHOPNOD DIR PARALLEL  PERPENDICU   LAR  PARALLEL    0  10  0    180  3600  NODEFAULT   0  359  0    8  30  8     SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    Spectrome
20. asured bandpasses and approximate sensitivities for image acquisition           3 3 Slit widths    Three different slit widths  0 4     0 75   and 1     are offered for all settings  For over sized widths   e g  for the 1   slit with respect to the diffraction limit around 10um   the spectral resolution of a    VISIR User Manual 10    filter Ac half band width sensitivity     um    um    mJy 100  1h   NSW 8 85 1 35 40  NLW 121 1 9 40  ArII 8 94 0 11 200  Nell1 12 35 0 50 80  Nell2 12 81 0 10 50       Table 3  VISIR spectrometer filter characteristics  The filters transmissions have been determined with  a monochromator and the WCU  The last column list the measured median sensitivities which were  obtained using the curve of growth method on data obtained in parallel chopping nodding directions   3 beams      point source spectrum is better than the one of the sky spectrum  in addition  the zero point of the  wavelength calibration will be affected by an incorrect centering of the object within the slit     3 4 Resolution    In the N band  the low resolution and medium resolution modes provide spectral resolving power  of   300  Table 4  and 3000  Table 5   respectively  In high resolution long slit mode  narrow  wavelength ranges around the 8 02  H2_54   12 813  Ne II  and 17 03 um  H2_S1  line are offered  With  the 1   slit the measured spectral resolution is R   15000  Table 6   and a minimum flux in the line  below 10716 W m   arcsec  can be achieved  This value correspo
21. at the lower left of the  detector  For the location of the object along the slit  pixel X 123 at row Y   128   this occured  for TEL CHOP THROW between 10 and 13     approximatively  The horizontal lines at the middle of the  images are caused by the lack of detector response at 8 8m         VISIR User Manual 16    image is stored as a plane in a data cube of a FITS file  The number of chopping cycles corresponds to  the time spent in one nodding position  Ta  This nodding period is typically Thoa   90s for science  observations  The chopper frequency  DIT and also Thoq are predefined by the system  The number  of saved A   B frames in one FITS file is           Nro   Till Lass  1     The number of nodding cycles is computed from the total integration time as given by the observer   The total number of stacked images for each secondary position  respectively chopper half cycle  is  NDIT  This parameter is computed according to     NDIT    2  DIT   fenop       NDITSKIP  2     and is given by the system  It depends on DIT  chopping frequency and NDITSKIP  some read outs at  the beginning of each chopper half cycle are rejected during stabilization of the secondary  Typical  stabilization times of the secondary are 25 ms  The number of rejected exposures is given by NDITSKIP   Similar  during stabilization after each telescope movement  respectively nodding position  a number  NCYSKIP of chopping cycles is ignored  The timing organization of data is shown in Fig  15        The 
22. ators  unless provided by the observer  are selected from the MIR spectro   photometric standard  star catalog of the VLT  http   www eso org instruments visir   This catalog is based on the  radiometric all sky network of absolutely calibrated stellar spectra by Cohen et al    This list is  supplemented by MIR standards used by TIMMI2       5 Cohen et al   1999  AJ 117  1864  Chttp   www 1s eso org lasilla sciops 3p6 timmi html stand html    VISIR User Manual 22    At present the standard star catalog contains 425 sources  Zero point fluxes  Jy  have been calculated  for the VISIR filter set by taking into account the measured transmission curves  Fig  21   the detector  efficiency  Fig  9  and an atmosphere model  Fig  1     A PSF can be derived from these photometric standard star observations  However  it is not guaran   teed that the accuracy is sufficient for deconvolution purposes  If the observer requires a specific PSF  measurement   s he has to provide the corresponding PSF OB    Observations of photometric standards provided by the observatory are taken using the  VISIR_img cal _AutoChopNod template  8 6  with the following settings     SEQ   TIME 180 sec for N and 360 sec for Q band  TEL   CHOP   POSANG 0    TEL   CHOP   THROW 10     SEQ   CHOPNOD  DIR PERPENDICULAR    Filter INS FILT1 NAME and pixel scale INS PFOV will be set according to the science observations     In spectroscopy  the observatory will provide spectro   photometric observations of a telluric  K
23. d the Q band between 16 5 and 24 5 um   respectively  In addition  it offers a slit spectrometer with a range of spectral resolutions between 150  and 30000    The MIR provides invaluable information about the warm dust and gas phase of the Universe  Micron  sized particles such as silicates  silicon carbide  carbon  coals  aluminum oxides or polycyclic aromatic  hydrocarbon  PAH  molecules are major contributors to the thermal MIR emission  The gaseous  phase emits through a large number of ionic and atomic lines  Examples are Nell  12 8 um   and the  pure rotation lines of molecular hydrogen at 8 02  9 66  12 27 and 17 03 um     Because of the very high background from the ambient atmosphere and telescope  the sensitivity  of ground   based MIR instruments cannot compete with that of space born ones  However  ground  based instruments mounted on large telescopes offer superior spatial resolution  For example VISIR  at the VLT provides diffraction limited images at   0 3     FWHM  in the N band  This is an order of  magnitude better than what can be reached by the Spitzer Space Telescope  SST     The VISIR user manual is structured as follows  Basic observing techniques of ground   based MIR  instruments are summarized in 3 2  y 3 provides a technical description of VISIR and its offered  observing modes offered  An overview on how to observe with VISIR at the VLT can be found in 8 4   A description of the structure of the imaging and spectroscopic data files is given in y 5
24. e  O     CO   C   lt L  0 1       N   N               5 10 15 20 25 30    Wavelength  um     Figure 2  VLT diffraction limit  full line  versus seeing  The Spitzer Space Telescope diffraction  limits  dashed  are shown for comparison  The Roddier dependence is shown for two optical seeings     dashed dot         The chopping technique cancels most of the background  However  the optical path is not exactly the  same in both chopper positions  Therefore a residual background remains  It is varying at a time   scale which is long compared to that of the sky  This residual is suppressed by nodding  where the  telescope itself is moved off source and the same chopping observations as in the on source position  is repeated    An illustration of the chopping and nodding technique is shown on Fig  3  Depending on the choice  of chopping and nodding amplitudes and directions  up to 4 images of the source can be seen on the  frame and used for scientific analysis  Of course  the free field of view on the chop nod images can  be severely reduced depending on the particular chopping and nodding parameters chosen        2 5 Sensitivity    Measurements of VISIR sensitivities are based on observations of mid infrared calibration standard  stars  Cohen et al  1991  AJ 117  1864   In imaging mode  the stars are recorded in the small  field  0 075     and intermediate field  0 127     by perpendicular chopping and nodding patterns with  amplitudes of 10     Calibrators are frequently observed
25. e 18 5  Wavelenght  um      ikter  0   120     100  E    80  09   5  2  601  0   o 20  09   c      20     O   J  18 5 19 0 19 5 20 0  Wavelenght  um   Filter  SIV  120     100     DRE  09   5   gt  60  0  E AO  09   C  2 20     O f  10 1 10 3 10 5 LOT    Wavelenght  um            190    10 9    Transmissions  in       Transmissions  in          Filter  QZ       ee  Wavelenght  um     18 9    Filter  Sic  120    100  SO    60    40  20    3 10 2 14 16  Wavelenght  um     Figure 18      continued     38    VISIR User Manual 39                         Filter  Nell_ref 1 Filter  PAH  ref    c 1 2 c  22   O cure     z   v 0 8 v 0 8   G E   O O   os   0 6           N 0 4 N 0 4   O O   E 0 2 E 0 2   O O      00   ZOO we   11 8 120 1 272 12 4 12 6 1038 1122 11 8 1222 12 8   Wavelenght  um  Wavelenght  um   Filter  SIV ref 1 Filter  SIV_ref2   a A c      Q    Q       Be             v 0 8 n   E C   o 5     076     O O   D D   N 0 4    N   O O   E 0 2 E   O O   Ze   i   9 5 9 7 9 9 10 1 10 5 10 4 1026 10 5 1140 11 2   Wavelenght  um  Wavelenght  um     Figure 19  Transmission curves of VISIR imager filters  manufactured by OCLI  Overplotted  dashed   is the atmospheric transmission at low resolution  Only relative transmissions have been determined   their values are normalized so that their peak transmission is equal to 1        
26. e is imaged on a cold stop mask to avoid  straylight and excessive background emission  The collimator mirror  M1  is a concave aspherical  mirror  It is followed by a folding flat mirror  M2  which eases the mechanical implementation     e A set of three objectives mounted on a wheel  Each objective is based on a three mirror  anastigmatic  TMA  system  Each of the TMA   s is made of three conic mirrors     The 0 075     small field  SF  and 0 127     intermediated field  IF  pixel scale are offered  Table 1    These offered pixel fields of view  pfov  ensure a proper sampling of the images in the N and Q band        pfov fov diffraction  diffraction   um pixels   0 127 32 5  32 5  94 1 88   0 075    19 2    x 19 2    159 3 18        Radius of first Airy ring at    7 7um  Table 1  VISIR imager pixel scales offered  The pixel size of the DRS 256x256 detector is 50 um    The first airy ring at    7 7um corresponds to a radius of 0 24   on the sky   The filter wheel is located just behind the cold stop pupil mask  The list of filters offered is given in  Table 2  The transmission curves of the filters measured at 35 K are plotted in the Appendix     Note that ETC v3 0 5 does not properly account for the background behavior as a function of airmass  Also  it  does not take into account the airmass dependence of the seeing        VISIR User Manual T       IA oe 1 I IT bafe tel T I E A D OT AT AT TI N NA 1   PT OT TT TO TT En          theoretical limit                     sensitiv
27. ected on the sky is straight  There  is an additional linear distortion in both dispersion and cross   dispersion direction of the detector  The  following algorithm is supported by the pipeline for low and medium resolution mode  Let us define  the detector pixels in dispersion direction by x and in cross dispersion direction by y  respectively    a  The skew angle along x with    and along y with W    b  The maximum curvature along x with A and along y with e       is defined positive in clockwise direction and Y counter   clockwise  A is positive by increasing x  and     by decreasing y  respectively  Measured values of the distortion parameters are in the low and  medium resolution mode Y   1 6   and Y   0 7    The curvatures in the low resolution mode are  e   1 04 pixel  A   0 08 pixel and for the medium resolution mode are       0 26 pixel  A   0 08 pixel   The center of the lower left of the detector is at  1 1   Therefore  the fix point  which is the detector  center  is at  128 5  128 5  for the n   256 pixel array of the DRS    The fix point is moved to  1 1  by     n 1 n 1    Al y      7  E  6   and the skew is corrected along the cross dispersion   falz  y     u y tan v   y   7     and along the dispersion direction     falx y     x y   z   tan       8     The curvature is a segment of a circle with radius  R in x direction given by  n   2y        2R            and in y direction by  n  2y A   2RA     A   It is corrected along the cross dispersion     falz  y    
28. es for J2000 0  Entries for equinox and proper motions are not   yet  taken into account     VISIR User Manual 21    4 4 Guide stars    Guide stars are mandatory for active optics and field stabilization  Any VLT programme should make  sure that a guide star  USNO catalog  with a V   11     13 mag is available within a field of 8    around  the object    If TEL AG GUIDESTAR is CATALOGUE     a guide stars from the guide star catalog will be automat   ically selected by the TCS  If TEL AG GUIDESTAR is SETUPFILE     the observer has to provide the  coordinates of the GS  The coordinates of the guide star also fix the reference point for the World  Coordinate System coordinates  that appear in the FITS header of the files    In both cases  the telescope operator acknowledges the guide star  Depending on the weather con   ditions or if the star appears double in the guide probe  the telescope operator may have to select  another guide star  Therefore  If the observer has selected a guide star for astrometric purposes     for  example  to insure the repeatability of the pointings between different OBs      a clear note should be  given in the README file  for service mode observations  or be specifically mentioned to the night  time astronomer  in visitor mode  As stated above  the observatory does not guarantee the accuracy  of the world coordinate systems  WCS  keywords in the FITS headers              4 5 Brightness limitations    There are currently no brightness limitations wi
29. g_acq MoveToPixel tsf    To be specified   Range  Da     INS FILTI NAME    INS PFOV  SEQ CHOPNOD DIR    SEQ TIME  TEL AG GUIDESTAR    TEL CHOP POSANG  TEL CHOP THROW  TEL GS1 ALPHA  TEL GS1 DELTA  TEL ROT OFFANGLE  TEL TARG ADDVELALPHA  TEL TARG ADDVELDELTA  TEL TARG ALPHA  TEL TARG DELTA  TEL TARG EQUINOX  TEL TARG OFFSETALPHA  TEL TARG OFFSETDELTA    SIC PAH  ARII SIV_1 SIV  SIV2 PAH2 PAH22 NEIL1  NEII NEIL2 Q1 Q2 Q3  NODE   FAULT    0 075 0 127  0 127    PARALLEL  PERPENDICU   LAR  PARALLEL    30  3600  NODEFAULT   CATALOGUE  SETUPFILE    NONE  CATALOGUE     0  359  0   8  30  8   ra      dec     0  359  0 0    0 0    0 0    ra      dec      2000 0    0 0    0 0     Imager Filter    Imager pixel scale  Relative Chop Nod Direction    Total integration time  sec   Get Guide Star from    Chopping Position Angle  deg   Chopping Amplitude  arcsec   Guide star RA   Guide star DEC   Rotator on Sky    PA on Sky   RA additional tracking velocity  DEC additional tracking velocity    RA blind offset  DEC blind offset       VISIR_img_acq_Preset tsf    To be specified   Range  Da     TEL AG GUIDESTAR    TEL GS1 ALPHA  TEL GS1 DELTA    TEL ROT OFFANGLE  TEL TARG ADDVELALPHA  TEL TARG ADDVELDELTA  TEL TARG ALPHA  TEL TARG DELTA  TEL TARG EQUINOX    CATALOGUE SETUPFILE  NONE  CATALOGUE    ra      dec      0  359  0 0     0 0     0 0    ra      dec       2000 0     Get Guide Star from    Guide star RA   Guide star DEC   Rotator on Sky    PA on Sky   RA additional tracking velocity  DEC add
30. hecklist for Phase 2 preparation    ill    O NN Ek en    Om 0    Ne     10  10  12  13    17  17  17  17  18  19  19  21  21  21  21  22  22  23  23  23  24    24  24  24  25    27  27  21  29  29    30    VISIR User Manual    8 Appendix  VISIR template parameters    81  Acqu  s  on     ee 3 oe 2 8 Soe ka a ee eee pi  DD IODSELVALION  cess ee en ee ee ee e AE OS ad de See ee eR  83     AIDE AIO x  y ERA A E a as ble oe ere i as    9 Appendix  Filter transmission curves    IV    31  31  33  39    37    VISIR User Manual    List of acronyms    BIB  BLIP  BOB  DIT  ETC  FWHM  ICS  IR  IRACE  MIR  OB  P2PP  PAE  pfov  PSF  S N  UT  VISIR  TCS  TMA  WCU    Blocked impurity band  Background limited performance  Broker of observation blocks  Detector integration time  Exposure time calculator   Full width at half maximum  Instrument control software  Infrared   Infrared array control electronics  Mid infrared   Observing block   Phase 2 proposal preparation  Preliminary acceptance in Europe  pixel field of view   Point spread function  Signal to noise ratio   Unit telescope   VLT imager and spectrometer for the mid infrared  Telescope control system   Three mirrors anastigmatic  Warm calibration unit    VISIR User Manual 1    1 Introduction    The VLT spectrometer and imager for the mid infrared  VISIR   built by CEA DAPNIA SAP and  NFRA ASTRON  provides diffraction limited imaging at high sensitivity in two mid infrared  MIR   atmospheric windows  the N band between   8 to 13 um an
31. ier Transform Spectrometer  at a temperature  of 35 K for filters manufactured by the company READING  Their absolute transmission curves are  displayed in Fig  21  The other filters  manufactured by OCLI  have been measured using the WCU  and wavelength scans with the monochromator  Note that for these filters  the transmission curves  are normalized to 1  see Fig  19                             Filter  Arlll Filter  Nell_ref2  120 1 20      100  amp  100          80   80  Y  09   O 6   gt  60 en 60  ace po  cy    40 E AG  WY  WY   E G  o 20     220       O     O    3 80 8 90 XOU 9 10 a2  1236 12 8 13 0 Rene 15 4  Wavelenght  um  Wavelenght  um   Filter  Nell Filter  PAH1_ARlllref 1  120 1 20  Q 100 be 100       80     80  09  Cp   O 6    80 S 60  2 ae  E 40   20 J  09  WY   C C  E 20 Z 20       O        O  gt     12 4 12 6 1226     a 10 2 a 3 0 8 5  gt 20 90  Wavelenght  um  Wavelenght  um   Fler  Paz Filter  QO  120 t20     100   100         80     80  WY  WY   5  S 60 S 60  2 D  E 40 ce AO  N WY      C   gt  20  Z 20       O   EN O la  TUS 159 11 6 122 12 8 1340 1022 16 8 1722 17 8  Wavelenght  um  Wavelenght  um     Figure 21  Transmission curves of VISIR imager filters  manufactured by READING  Overplotted   dashed  is the atmospheric transmission at low resolution  The absolute transmission values are  given  expressed in percent        VISIR User Manual             Filter  07  120     100        0  09   5   gt  360  0    gt  A0  09   c     30     O _ u  15 20 16 5 pac
32. imited either by the diffraction of the telescope  or the atmospheric seeing  The diffraction limit as measured by the diameter of the first Airy ring  increases with wavelength as 1 22 A D  where A is the observing wavelength and D the diameter of  the telescope mirror  see solid line in Fig  2   The wavelength dependence of the seeing can be derived  by studying the spatial coherence radius of the atmosphere in the telescope beam and is to first order  approximated by the Roddier formula  where the seeing is x A7   see dot dashed lines in Fig  2            VISIR User Manual 2    MIR atmosphere transmission at Paranal    Transmission              5 10 15 20  Wavelength  um     5 30    Figure 1  MIR atmospheric transmission at Paranal computed with HITRAN for an altitude of 2600 m  and 1 5 mm of precipitable water vapor at zenith  The US standard model atmosphere is used     However  initial results from VISIR data indicate that this formula overestimates the measured MIR  seeing at Paranal by 20 50   as the size of a UT mirror is comparable to the turbulence outer scale   As a result  VISIR data are already diffraction limited for optical seeing below 0 6        2 3 MIR background    The atmosphere does not only absorb MIR photons coming from astrophysical targets  but also emits  a strong background with the spectral shape of a black body at about 253K  Kirchhoff   s law   The  telescope gives an additional MIR background  The VLT telescopes emits at 283 K with a preliminar
33. imposed is the theoretical photon noise  BLIP performances are approached for higher fluxes  and larger DIT  respectively     memory effects  Stabilization is ensured by introducing dead times where necessary  It is advised to  observe only sources fainter than 500 Jy in N and 2500 Jy in Q    These artifacts are less important in spectroscopy due to the lower light levels but clearly visible on  objects brighter than   2  of the background  However  a TEL CHOP THROW between 9 to 13    shoud  be avoided  in particular for objects bright enough to be seen in individual DITS  as one of the beams  will hit some particularly hot pixels in the lower   left of the spectrometer detector  see Fig 14         3 8 Data acquisition system    Both VISIR detectors are controlled by the ESO standard IRACE acquisition system  In imaging  the read out rate of the detector is high  Up to 200 frames per s are read for a minimum detector  integration time of DIT  5ms  Such a frame rate is too high to store all exposures  One VISIR  image is of size 256x256  each pixel is coded with 4 bytes  long integer   Thus one read out has a  size of 262 kB  During each chopping cycle the elementary exposures are added in real time and only  the result is stored on disk  At a chopping frequency of fchop   0 25 Hz every Tenop   48 one VISIR       VISIR User Manual 14                                                 GE  SST o  S   m nn Zn   6 5  T 7  e   31 90x10        e  Bx 0 PA att Le A   tt  D p a gett      
34. ities are the reference for classification of VISIR service mode observations   and the basis to assess the feasibility of an observing programme  In particular  classifications of  service mode OBs will be based on sensitivity measurements made at zenith  Calibrations will  be provided following the guidelines given in 34 7  For up to date information  please consult  http   www eso org instruments visir  The use the VISIR exposure time calculator  ETC  lo   cated at http    www eso org observing etc   is recommended to estimate the on source integra     tion time                   3 Instrument description and offered observing modes    For P76  VISIR offers two spatial scales in imaging and several spectral resolution modes in slit  spectroscopy  The imager and spectrograph are two sub instruments  They have independent light  paths  optics and detectors  The cryogenic optical bench is enclosed in a vacuum vessel  The vessel  is a cylinder  1 2m long and 1 5m in diameter  Standard Gifford McMahon closed cycle coolers are  used to maintain the required temperature  33 K for most of the structure and optics and  lt  15K for  the parts near the detector  The detectors are cooled down to   7K        3 1 Imager    The imager is based on an all reflective design  The optical design is shown in Fig  6  It consists of  two parts     e A collimator  which provides an 18mm diameter cold stop pupil in parallel light  As generally  designed for IR instruments  the pupil of the telescop
35. itional tracking velocity       VISIR User Manual 32    VISIR_spec_acq_MoveToslit tsf    To be specified   Range Default    INS FILT2 NAME NSW NLW ARII NEIL1   Acquisition Filter  NEIL2  NODEFAULT   INS SLIT1 TYPE LONG SHORT  LONG  Spectrometer Slit Type  long or  short  INS SLIT1 WIDTH 0 40 0 75 1 00  NODEFAULT  ic O Slit Width  arcsec   SEQ CHOPNOD DIR PARALLEL  PERPENDICU    Relative Chop Nod Direction  LAR  PARALLEL   SEQ TIME 30  3600  NODEFAULT  Total integration time  sec   TEL AG GUIDESTAR CATALOGUE SETUPFILE   Get Guide Star from  NONE  CATALOGUE   TEL CHOP POSANG 0  359  0  Chopping Position Angle  deg   TEL CHOP THROW 8  30  8  Chopping Amplitude  arcsec   TEL GS1 ALPHA ra    Guide star RA  TEL GS1 DELTA dec    Guide star DEC  TEL ROT OFFANGLE 0  359  0 0  Rotator on Sky    PA on Sky   TEL TARG ADDVELALPHA    0 0  RA additional tracking velocity  TEL TARG ADDVELDELTA  0 0  DEC additional tracking velocity  TEL TARG ALPHA ra     TEL TARG DELTA dec     TEL TARG EQUINOX  2000 0   TEL TARG OFFSETALPHA    0 0  RA blind offset  TEL TARG OFFSETDELTA  0 0  DEC blind offset       VISIR User Manual    8 2 Observation    33    VISIR_img_obs_AutoChopNod tsf    To be specified   Range Default    Imager Filter    INS FILT1 NAME    INS PFOV  SEQ CATG    SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    SIC PAH  ARII SIV_1 SIV  SIV2 PAH2 PAH22 NEILI  NEII NEII 2 Q1 Q2 Q3  NODE   FAULT    0 075 0 127  0 127   PRE IMAGE SCIENCE  SCI   ENCE    PARALLEL
36. ity  mJy 100 1h                 8 9 10 11 12 13  wavelength  um           100007               model   M        median p                                            1000           sensitivity  mJy 100 1h                                                HAIR    12 70 12 75 12 80 12 85 12 90  wavelength  um              Figure 5  Sensitivity as a function of wavelength for low  top  and high  bottom  resolution mode   Four offered settings of the N band low resolution are stitched together  Atmospheric molecular  absorption  e g  at 9 55  11 8 and 12 5 um  is evident  Note the detector feature at 8 8 ym  Dots  indicate individual observations  full lines represent median and the dashed line the best sensitivities   In the 12 81 um region several settings of the high resolution mode are shown  Theoretical model  curves correspond to BLIP           VISIR User Manual 8  entrance window    diaphragm   focal plane     i     IN    TMA optics  filter    AN          Figure 6  The optical path of the imager in the intermediate field  0 127     pixel  is shown from the  entrance window down to the detector     filter Ac half band width maximum sensitivity   um    um   transmission  mJy 100 1h    7   theory median   BLIP  SF IF  PAH1 8 59 0 42 77 1 6 5 8  ArTII 8 99 0 14 72 4 1 6 70  SIV_1 9 821 0 18 12 4 0 30 60  SIV 10 49 0 16 70 4 5 8 13  SIV 2 10 77  0 19 70 4 6 9 20  PAH2 11 25 0 59 75 2 3 6 9  SiC 11 85 2 34 75 1 2 7 18  PAH22 11 88  0 37 58 4 1 7 l5  Nell1 12 27  0 18 51 6 9 12 20  Ne
37. ll 12 81 0 21 64 6 1 12 18  Nell_2 13 04 0 22 68 6 3 15 22  Q1 17 65 0 83 59 11 1 50 120  Q2 18 72 0 88 49 13 6 50 80  Q3 19 50 0 40 50 41 7 100 160    Table 2  VISIR imager filter characteristics  following the manufacturer specifications  except for the  central wavelengths noted with   which were re determined with a monochromator and the WCU  because they deviate from specifications  The last 3 columns give  respectively  the theoretical expec   tations under BLIP and excellent weather conditions  and the measured median sensitivities for the  Small and Intermediate Field obtained in various weather conditions  The measured sensitivities were  obtained using the curve of growth method on data obtained in perpendicular chopping nodding  directions  4 beams            VISIR User Manual 9    3 2 Spectrometer    VISIR offers slit spectroscopy at three spectral resolutions with a pixel scale of 0 127     This is obtained  by means of two arms  one with low order gratings for the low and medium spectral resolution  the  other with large echelle gratings providing high spectral resolution     VLT FOCAL    DIAPHRAGM  WHEEL          i IMAGER    OLDSTOP  ILTER WHEEL       TALON WHEEL                             LMR De  GRATING UNIT kan r Er   4 GRATING SCANNERS  DUO ECHELLE  1 RETURN FLAT  GRATING UNIT  Ny ESOLUTION SELECTION  MECHANISM  LMR  MLW COLLIMATOR  R  CAMERA N COLLIMATOR    en IN    CAMERA  a w  wu a   E renner   lt    EE oo OoOO  V Sl Z  wW  PUPIL    gt   IMAGING  LENS T
38. monochromatic point source with adjustable wavelength or  an extended black body source with adjustable temperature  A selection mirror allows to switch from  the telescope to the simulator beam  It can be used for calibration and tests  also during daytime   Fig  8 shows the unit on top of the enclosure     VISIR User Manual 11           range Ac grating spect    resol  dispersion   um    um  order  measured  1   slit   pixels um    7 7 9 3 8 5 2 300     390 160 01  8 0 9 6 8 8 2 300     390 160 02   9 0 10 6 9 8 2 305     360 160 05  10 34 12 46 11 4 1 185     220 119 94  11 14 13 26 12 2 1 215     250 119 96  11 34 13 46 12 4 1 215     250 119 96    Table 4  VISIR low resolution offered settings  The first column gives the wavelength range of a  spectrum for the central wavelength  Ace  listed in the 2nd column  The measured sensitivities are    50mJy at 100 1h in the clean regions of the spectrum  cf  Fig  5  for a slit width of 1     Offered  slits have widths of 0 40  0 75 and 1 00     The spectral resolution of the 8 5um and 12 2um settings  has not been independently measured  values for the 8 8um and 12 4um settings are reported instead     A     range Ne grating spect  resol  dispersion   um    um  order  measured  1   slit   pixels um    8 706 8 893 8 8 2   3500 1367 43  11 274 11 526 11 4 1   1800 1011 2    Table 5  VISIR medium resolution setting  The measured sensitivities are   200 mJy at 100 1h   Offered slits have widths of 0 40  0 75 and 1 00        mode Ac 
39. nds to an approximate sensitivity  limit around 1 Jy in the continuum  A high resolution  cross dispersed mode with a 4    short slit is  available for wavelength settings around 9 66  H2_S3  and 12 27 um  H2_S2         Please consult http    www eso org instruments visir for the latest update of the list of offered  modes and slits     3 5 Low resolution  offered central wavelengths    In addition to the 4 central wavelengths  8 8  9 8  11 4 and 12 4 um   announced in Phase 1  two  additional ones are offered for Phase 2  at 8 5 and 12 2 um   The main reason justifying these  two new settings is of cosmetic nature  As described below  the detector has a number of    bad     pixels  In particular  some of them  mainly located at the bottom left of the detector appear to cause  particularly severe striping in the chopped images if their illumination is slightly different in the two  chopping positions  This situation can be produced either if one of the beams of a bright object falls  on these pixels or because of a residual scanner jitter of the grating units  The 8 5um setting moves  the blue wing of the ozone band off the wavelength range covered by the detector  at the expense of  having a larger part of the detector covering the red wing of the water vapour band  The 12 2um  setting avoids the CO2 band       3 6 Calibration units    A warm calibration unit  WCU  is located on top of the VISIR vacuum enclosure  The WCU is also  called star simulator  It simulates either a 
40. ng and nodding technique on observations of the blue compact  galaxy He2 10  The galaxy only appears after chopping and nodding  courtesy VISIR commissioning  team  June 2004      VISIR User Manual 5                               DEERE RAS OEA IRENE ei rer  A median small field  1 00 E   y median intermed  field E  a E VW      Y    O         2        E      a 4   gt          E u      y y     el    10   ii     a 4 a      Yo  a4 7 das A y  7 r io ie 1 4 a      LE ea TAUR en i  D A  Y  F   e  y    ARIII SIV PAH2 PAH2_2 NEII  4 PAH1 SIV_1 SIV_2 SIC NEIl 1 NEII_2  pas  yo e sh the A A AA ERAN Fear Ar DS e ITA ERE O AE  j   ATA di    BER   8 9 1 11 12 13  wavelength  um   SE E sl  A median small field       median Intermed  field i    y  S 100    4 E  2 i 6 y d  k A    a  E A l   gt     2  0  E  O  2 10F    k Q1 Q2 Q3 1                          170 175 180 185 19 0 19 5 20 0  wavelength  um     Figure 4  Sensitivities for the VISIR imager for the N  top  and Q band  bottom   Small and in   termediate field observations are displaced for clarity  Background noise limits are indicated for the  individual filter bandpasses     VISIR User Manual 6    obtained  with the central one containing twice as much flux as the two other ones    Table 4 to 6 list typical sensitivities measured in low  medium and high resolution modes away from  strong sky emission lines for the wavelength ranges offered in P76  Figure 5 shows the dependence  of the sensitivity on wavelength    The median sensitiv
41. ng to the two  chopper positions  may therefore not be equal  If this difference is larger than a few tens of ADUs   structures in the gain maps will appear as low level stripes  Such stripes tend to smooth out on long  integrations     4 8 3 Bad residuals    The chopping and nodding technique does not always lead to a satisfactory removal of all the structures  seen in individual images  Bad residuals have been found to occur in the following situations        e in observations carried out close to zenith and  to a lesser extent  close to the meridian in general   the likely cause is the fast rotation of the field relative to the telescope structure     e in variable atmospheric conditions     In addition  it seems that imaging of extended objects are also more likely to be affected by low level  bad residuals  similar to fringes in some aspects  whose orientation on the images changes at the same  angular velocity as the rotator  The origin of these structures is not understood     4 8 4 Residuals of sky emission lines    In spectroscopy  the scanners of the grating units may still show a small residual motion at the  beginning of an exposure  or  mainly for the HR or HRX modes  show some jitter after a nodding  offset  The first few frames at a given wavelength setting may therefore show stronger than expected  residuals at the wavelength of the sky emission lines  more exactly  of the wings of sky emission lines    For the HR and HRX modes  the residuals of the scanner ji
42. of bad pixels   lt  2   Fig 12   The imager detector also  suffers from striping and appearances of ghosts  The relatively wide rectangular area in the lower  right corner  South   West corner for PA   0 deg  of the imager detector or some other rectangular  areas are masked out to avoid such disturbances  Fig  13   For bright objects the DRS detector shows    VISIR User Manual 13                0 4 F    QZ       Detective quantum efficiency  nG           Oe ee NE E NE ne ne EEE  O    10   Es 20 2 SO  Wavelength  um        Figure 9  Detector quantum efficiency at 12K provided by DRS  solid line   The same curve  dashed   but scaled by 0 72 reflects a lower limit of the quantum efficiency  The scaling was derived from  laboratory measurements  Note the sharp absorption feature at 8 8 um that will appear in raw  spectroscopic data                                                                          6000 En Zr E ee 1500 a    t Large Cap  tel sus    0 5 me   Small Cap  det_sub   OV  T 5 1 K x a     ey    Se 1022 Jake      R se L 6G   1 013  _ 4000   j Ja WOOO R O ar      eo f nn     D O  0 n     O B  Z   Z  2000 f 500      Data Data  gt   Fit of the data          Fit of the data           L Photon noise   Photon noise  O 1   1 1 f f   j   fi f O Ll L Ll L   Ll Ll 1 f Ll Ll      Ll  0 5 0x10   1 0x10  1  5107 0 5 0109 1 0x10   1 5x10    Signal  e     Signal  e        Figure 10  Noise as a function of the incoming flux in the large  left  and small  right  capacity mode   Super
43. onding science templates  but allow to monitor the  sensitivity and image quality by observing calibration standard stars     7    VISIR User Manual   30    Checklist for Phase 2 preparation      Acquisition  Are the coordinates accurate in the equinox J2000 0 reference frame  For high     proper motion objects  are they valid for the epoch of the observations  For solar system  objects  are they in the topocentric  ICRF or FK5  J2000 0 reference frame at the epoch of the  observations       Acquisition  Is relative good astrometric accuracy required  if yes  a guide star should be    provided whose distance relative to the target is accurately known       Pre imaging  If OBs are part of the pre imaging run of your programme  the name of the OB    must start by PRE and the SEQ CATG keyword must be set to PRE IMAGE       Calibrations  For calibration OBs  use the appropriate VISIR img cal AutoChopNod or    VISIR_spc_cal_LR MR HR HRXAutoChopNod templates       Position angle  If the observations must be carried out at a position angle different from    0  check 34 2 1 and 34 2 2  In particular  it is useful to clearly indicates in the README  file if TEL  CHOP POSANG is not equal to TEL ROT OFFANGLE to warn the instrument operator  about the non standard configuration  In spectroscopy  TEL CHOP POSANG must be equal to  TEL ROT OFFANGLE in order to have the 3 beams along the slit     VISIR User Manual    8 Appendix  VISIR template parameters    8 1 Acquisition    31    VISIR _im
44. org observing p2pp P2PP too1 html  Acquisitions  observations and cali   brations are coded via observing templates  One or more templates build up an observing block   OB   They contain all the information necessary for the execution of a complete observing  sequence  An overview of the available VISIR templates and their parameters is given in 86 of  this manual     e For each science template  the user has to provide a finding chart so that the target can be  acquired  In addition to the general instruction on how to create these finding charts  see  http    www eso org observing p2pp ServiceMode html  the following VISIR requirements    apply            All finding charts have to be made using existing infrared  K band or longer wavelength   images  Typically  2MASS or DENIS K band images are acceptable  although higher spatial  resolution may be preferable         If the wavelength at which the finding chart has been taken is different from that of the  science observation  e g  a K band finding chart for a 10um spectroscopic template  the  user has to describe clearly how to identify the target at the observing wavelength in the  README section of the programme description  Adequate examples of such comments  are     x The target will be the brightest source in the field of view at 10um         x At 10um   there will be two bright sources in our field of view  The science target is  the southernmost of these two     Note that observations close to zenith during meridian
45. pendicular  direction  Note that while the telescope offset is in positive  East  direction  the resulting image on the  detector will move to the West  This technique is recommended for point or relatively small extended    lt  5     sources  Fig  3      spar       Nodding Position A Nodding Position B  Nodding Position A Nodding Position B      Figure 19  Schematic drawing of the content of a frame obtained with TEL CHOP POSANG   O and  SEQ CHOPNOD DIR   PARALLEL  top  and SEQ CHOPNOD DIR PERPENDICULAR  bottom   In the indi   vidual nodding positions  the positive beams correspond to the chopper position A and the negative  beams to the chopper position B  Note that the default pointing position of the telescope corresponds  to the center of the detector  Within the accuracy of the telescope pointing  this location matches the  nodding position A  chopper position A if SEQ CHOPNOD DIR   PARALLEL     The keywords SEQ  JITTER WIDTH allows chopping and nodding with random offsets so that a jitter  pattern is performed  This technique allows to reconstruct bad pixels  For SEQ  JITTER WIDTH   Ono  jitter is performed and the resulting image depends on the setting of SEQ  CHOPNOD DIR  The chopping  period is set by the system and the nodding period is fixed to 90s  The number of nodding cycles  Neyel_nod 18 computed according to the total observation time    3 8      VISIR User Manual 28    VISIR_ img _obs GenericChopNod   This imaging template enhances the flexibility of nodding
46. r or in the slit by   manual intervention by the operator    There are two acquisition templates for imaging  VISIR_img_acq Preset  VISIR_img_acq MoveToPixel  and one for spectroscopy  VISIR_spec_acq_MoveToSlit  The observing parameters are described in   38 1    The effect of all acquisition templates is first to point the telescope so that the center of the detector   match the target coordinates entered by the user  within the accuracy of the VLT pointing  see below     For VISIR_spec_acq MoveToSlit  the first acquisition images are obtained with the OPEN  15 37    slit    Then     e Both VISIR_ img _acq MoveToPixel and VISIR_spec_acq_MoveToSlit requires interaction with  the instrument operator or night support astronomer in order to center the target at the appro   priate location on the detector  Without further indication given by the observer  the default  locations are         the center of the detector  for VISIR_img_acq MoveToPixel and SEQ CHOPNOD DIR   PAR   ALLEL     3 This convention is identical to the UVES one  but differs  from example  from the ISAAC or NACO one     VISIR User Manual 20        in the top left quadrant of the detector  at a distance equal to TEL CHOP THROW 72  from the center of the detector in both X and Y  for VISIR img acq MoveToPixel and  SEQ CHOPNOD DIR   PERPENDICULAR         at the center of the chosen slit  for VISIR_spec_acq_MoveToSlit     In service mode  acquisition with these templates are limited to objects brighter than 0 2 Jy  
47. s are supplied to the user on an experimental basis           4 8 Known problems   In addition to effects caused by the cosmetic quality of the detectors mentioned above  83 7   the  following problems may affect the quality of the observations    4 8 1 Decreased image quality    The image quality can be severely degraded in observations obtained with a large   gt  15     chopper  throw  as can be seen in Fig 17  The origin of this problem has been localized and all efforts will be  made to implement a solution as soon as possible     VISIR User Manual 23      oe       x  VISIR 2005 01 29703 48 24 517_tp1_0000  fits    Figure 17  Image of a star obtained in the PAHI filter in the Small Field  0 075     pixel   and with  TEL CHOP THROW   25      SEQ CHOPNOD DIR   PARALLEL and TEL CHOP POSANG   90    Left  the  core of the star image appears double with two peaks separated by   0 2      Right  the wings of the  image reveals 2 additional components on both sides of the core  separated by 1 8    and containing    4  of the total flux  Note also the electronic ghosts that appear as white features immediately  above and below the core  and which only affect bright sources     4 8 2 Low level stripes    The background level of individual DIT images fluctuates not only with the varying sky background  but also with the detector temperature  The latter follows the 1Hz period of the closed cycle cryo   cooler  The mean background level in two consecutive half cycle frames  correspondi
48. source geometries might require larger amplitudes  and or   SEQ CHOPNOD DIR   PERPENDICULAR in order to avoid self cancellation        Low and medium resolution   Templates for low and medium resolution spectroscopy are    VISIR_spec_obs_LRAutoChopNod and VISIR_spec_obs_MRAutoChopNod  respectively  Observing pa   rameters are  total integration time  SEQ TIME   central wavelength  INS GRAT1 WLEN   the slit width  INS SLIT1 WIDTH and SEQ CHOPNOD DIR  8 6 2      High resolution  long slit mode   Template for high resolution spectroscopy is VISIR_spc_obs HRAutoChopNod  Three order sorting  filter at 8 02  12 81 and 17 03um  INS FILT2 NAME     H2_S4   Ne 11   H2 S1   are available  Other  observing parameters are  total integration time  SEQ TIME   central wavelength  INS GRAT1 WLEN    the slit width  INS SLIT1 WIDTH  and SEQ  CHOPNOD DIR    6 2      High resolution  cross   dispersed mode   VISIR_spc_obs_HRXAutoChopNod is functionally similar to VISIR_spc_obs_HRAutoChopNod  but uses a  grism for cross dispersion and order separation  Two central wavelength settings  9 66 and 12 27 um   are currently available  Note that the effective length of the spectrograph slit is limited to   4     Total  integration time  SEQ TIME   the slit width  INS SLIT1 WIDTH  and SEQ CHOPNOD DIR are specified  as usual  8 6 2         6 4 Calibration    Specific templates exist for the observations of photometric and spectro photometric standard stars   They offer the same functionality as the corresp
49. tely transparent  at others partly or completely opaque  Differential absorption is often corrected  by dividing the extracted spectrum by a reference spectrum  This procedure may cause numerical  instabilities at wavelengths close to strong sky lines that might amplify the noise        Photometry   Spectro photometric calibration of low and medium resolution spectra can be achieved with the MIR  standard star list provided by the Observatory  see    4 7   For high resolution spectroscopy only  calibrators known with high precision  such as  A stars or asteroids  should be considered  However   even early    stars are known to have some hydrogen absorption lines in the N and Q band     VISIR User Manual 27    6 VISIR templates description    6 1 Acquisition  Each OB needs to start with an acquisition template  they are described in 8 4 3     6 2 Observing with the imager    VISIR_img_obs_AutoChopNod   This template permits observing a source in imaging configuration with various sub settings  The  observer must specify filter  pixel scale  chopper throw  which is in the range of 8    to 30     The  keyword SEQ CHOPNOD DIR is set to PARALLEL or PERPENDICULAR  which results in images as shown  in Fig  19  PARALLEL considers an equal nodding and chopping amplitude which are both in parallel  direction  It is recommended for faint  extended sources  for which the spatial resolution is not so  crucial  PERPENDICULAR considers an equal nodding and chopping amplitude  however in per
50. ter Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR User Manual    8 3 Calibration    INS FILT1 NAME    INS PFOV  SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    VISIR_img_cal_AutoChopNod tsf    To be specified   Range Default    Imager Filter    SIC PAH  ARII SIV_1 SIV  SIV2 PAH2 PAH22 NEILI  NEII NEII 2 Q1 Q2 Q3  NODE   FAULT    0 075 0 127  0 127    PARALLEL PERPENDICU   LAR  PERPENDICULAR   0  10  0    30  3600  NODEFAULT    0  359  0    8  30  8     99    Imager pixel scale  Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_cal_LRAutoChopNod tsf    Range  Default     To be specified   Parameter  INS GRAT1 WLEN    SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP THROW    8 5 8 8 9 8 11 4 12 2 12 4  NODE   FAULT    PARALLEL  PERPENDICU   LAR  PARALLEL    0  10  0    30  3600  NODEFAULT    0  359  0    8  30  8     Spectrometer Wavelength  mi     crons   Relative Chop Nod Direction    Random Jitter Width  arcsec   Total integration time  sec   Chopping Position Angle  deg   Chopping Amplitude  arcsec        VISIR_spec_cal MRAutoChopNod tsf    To be specified   Range  Deja     INS GRAT1 WLEN  SEQ CHOPNOD DIR    SEQ JITTER WIDTH  SEQ TIME  TEL CHOP POSANG  TEL CHOP 
51. th VISIR  However  it is advised to observe only  sources fainter than 500 Jy in N and 2500 Jy in Q to avoid detector artifacts  8 3 7      4 6 Overheads    The VLT telescope overhead for one OB which includes active optics setting  selection of guide star   field stabilization is 6 min     VISIR instrument configurations can be changed in a short time  For example a complete change of  instrument settings takes less than 2 minutes  The total time for an image acquisition of a bright  sources   gt 1Jy  takes   5min  for one fine acquisition iteration  or in blind preset 2min  Spectro   scopic acquisitions take longer and are strongly dependent on the source brightness   an overhead of  15min  is accounted for sources  gt 1 Jy  while 30min  are required for sources between 0 2 and 1 Jy   respectively        Instrument overheads due to chopping and nodding duty cycle losses have been measured to be 25   of the observing time for the imager and 50  for the spectrometer  respectively           The total observing time requested by the observer must include telescope and instrument overheads     4 7 Calibration observations    MIR observations depend strongly on the ambient conditions such as humidity  temperature or air   mass  In service mode science observations are interlace by calibration observations on a timescale of  3h  Observations of photometric standards will be provided by the observatory within a time interval  of three hours w r t  the science observations    Calibr
52. the photons emitted by the telescope and the  atmosphere  The dark current is removed by the observation technique  chopping or nodding   It is  at least 6 times lower than the photon noise for the spectrometer and negligible for the imager    The detectors have a switchable pixel     well     capacity  The large capacity is used for broad band  imaging and the small capacity for narrow band imaging and spectroscopy  Detector saturation due to  the enormous MIR background is avoided by a storage capacity of 1 9  10  e  in small and 1 8 107 e7  in large capacity modes  respectively  For background limited noise performance  BLIP   the optimal  operational range of the detector is half of the dynamic range for the large capacity  and between 1 2  and 1 5 for the small capacity  The detector is linear over 2 3 of its dynamic range  Fig  11  and its  working point is set in the middle of the dynamic range  During commissioning it was found that  for  about half of the array  the gain does not differ by more than 2  peak to peak  By comparison with  other limitations  flat field corrections  which are difficult to implement in the MIR  are not considered  important  The detector integration time  DIT  is a few milli seconds in broad band imaging and  may increase to   2s in high resolution spectroscopy  The DIT is determined by the instrument  software according to the filter and pfov  It is not a parameter to be chosen by the observer    The DRS detectors contain a fair fraction 
53. to ensure that correct target coordinates are  provided for the equinox J2000 0 ideally at the epoch of the observations   The following cases require  special care     e imaging in the small field  in some conditions  an error of less than 10    on the coordinates can  bring the target outside of the field     e spectroscopic acquisition  in some conditions  an error of less than 7 5    on the coordinates can  bring the target outside of the wide slit used     Errors of such scale are common in the following situations     e high proper motion stars  in particular  if the epoch of the VISIR observations is significantly  different from the epoch for which the coordinates were determined        e point like sources within extended objects  such as an AGN  a number of catalogues do not  provide accurate coordinates of the nucleus  Coordinates given by 2MASS are more reliable     e coordinates obtained with low spatial resolution instrument  such as MSX  etc       For solar system objects  the J2000 0 equinox  topocentric  ICRF or FK5 coordinates at the epoch  of the observations are required  as the Telescope Control System takes into account precession   nutation  annual aberration and refraction  On the contrary  the topocentric  apparent coordinates at  the observatory  often used in other observatories  should not be used  Additional velocity parameters  corresponding to  a  cos    and u     must be given in     s        In particular  note that P2PP only accepts coordinat
54. total on source integration time is     leonie   4  Neyanod     Nesei ch  p  NDIT   DIT  3     The total rejected time is     tskip   4  Noyel_chop   DIT    NDITSKIP   Neyel_noa   NDIT   NCYSKIP   4     and the total observing time is     ttot   source E tskip  5   Typical duty cycles  tsource ttot  are about 70      nereko eyo chop Ncyskp  N Cycl_ chop  mg  gt     An e Bn  Si Bn An      T_nod re  DIFSRIP NDIT NDITSKIP  ee bs        DIT  T_chop    Figure 15  Data timing in VISIR  Ac and Bc refer to the two chopper positions  An and Bn refer to  the two nodding  telescope  positions  Note the AnBnBnAn cycle sequence for the nodding to save  observing time        VISIR User Manual 17    4 Observing with VISIR at the VLT    4 1 Proposal preparation       Tools are available to prepare the observations  either during phase 1  call for proposals   or during  phase 2  creation of observing blocks by the observer      e The exposure time calculator  ETC available at http    www eso org observing etc   may be  used to estimate the integration time needed to obtain the required S N for a given instrument  setting  because of the numerous sky absorption lines and the detector feature  see Fig  5   it  is recommended to display the S N as a function of wavelength when using the spectrograph  ETC        e As for all VLT instruments  astronomers with granted VISIR telescope time prepare their obser   vations using the phase 2 proposal preparation tool  P2PP   described at  http   www eso 
55. tter tend to cancel out on long integrations   and lead to a very slight decrease of the spectral resolution     VISIR User Manual 24    4 8 5 Fringes       The DRS detector shows fringes which are generated in the detector substrate  One example of such  fringes is shown in Fig  18 for the medium resolution mode  The fringes are stable and are not appar   ent in chopped images  but the spectra are modulated  Division of the extracted spectra by standard  star spectra simultaneously removes most of the fringes and corrects for telluric features     u        A QFLPbP    a         adl    Figure 18  VISIR spectrum in staring  medium resolution mode showing the detector fringing  white    The detector absorption feature at 8 8 um is visible as black horizontal bar  cf  Fig  9   Dark vertical  stripes are caused by the non   uniform gain of the different electronic amplifiers  These features are  largely removed by chopping     5 VISIR data    5 1 Data format    One FITS file is saved for each telescope nodding position  This file is a data cube and contains for  each chopping cycle     1  half cycle frames of the on source position  A  of the chopper        2  the average of the current and all previous A B  chopped frames        In addition  the last plane of the cube contains the average of all chopped frames    For the default value of the rotator angle  00   images are oriented North up and East left  Spec   troscopic data are aligned horizontally in the spatial and verticall
56. y  emissivity estimate of  lt  15   The VISIR instrument is cooled to avoid internal background contami   nation  The detectors are at   7K and the interior of the cryostat at 33K  The background radiation  at 10um is typically my      5 mag arcsec   3700 Jy arcsec     and at 20um mo      7 3 mag arcsec    8300 Jy  arcsec      Consequently  the number of photons reaching the detector is huge  often more than 10  photons s   Therefore  the exposure time of an individual integration   the Detector Integration TIme  DIT    is  short  of the order of a few tens of milli seconds in imaging mode     2 4 Chopping and nodding    The basic idea to suppress the MIR background is to perform differential observations  using the  chopping nodding technique    In the chopping technique two observations are performed  One set of exposures on source  include  the background and the astronomical source     second set of off source exposures measures the pure  background  The on  and off source observations have to be alternated at a rate faster than the  rate of the background fluctuations  In practice  it is achieved by moving the secondary mirror of the  telescope  For VISIR at Paranal  a chopping frequency of 0 25 Hz has been found to be adequate for N   band imaging observations  while 0 5 Hz are adopted for Q band imaging  Spectroscopic observations  are performed with lower chopper frequencies  at 0 1 Hz        VISIR User Manual 3                   10 0     Y  D  nn  2  C  z  Er  O  N  
57. y in the dispersion direction  cf   Fig 18   For the LR and MR modes  the short wavelength appear at the top of the frames  For the  HR and HRX modes  the short wavelength is at the top of the frame if the side B of the dual grating  is used  and at the bottom of the frame of the side A is used     5 2 Pipeline    The VISIR pipeline has been developed by ESO DMD and uses the ESO CPL library  The main  observation templates are supported by the pipeline reductions  Raw images of imaging and spectro   scopic observations are recombined  Spectra are extracted and calibrated in wavelength  8 5 3  for all    VISIR User Manual 25    spectroscopic modes in low   medium   and high resolution  Sensitivity estimates based on standard  star observations are provided both in imaging and spectroscopy  8 4 7   Public release of the VISIR  pipeline is foreseen for the beginning of P76    The pipeline currently supports the following templates      e VISIR img _obs_ AutoChopNod   e VISIR_spec_obs_LRAutoChopNod  e VISIR spec_obs MRAutoChopNod  e VISIR spec_obs HRAutoChopNod  e VISIR spec_obs HRXAutoChopNod       In mosaic  or raster  mode  VISIR_img_obs_GenericChopNod  only raw frames are delivered  e g   mapping reconstruction algorithms are not supported     5 3 VISIR spectrometer data    Optical distortion correction   Spectra are deformed by optical distortion and slit curvatures  The VISIR spectrograph uses curved  slits to cancel the distortion of the pre slit optics  Thus the slit proj
    
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