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Cycle 5 FIFI-LS in SSPOT
Before preparing detailed FIFI-LS observations in SSPOT, please read the FIFI-LS section in the SOFIA Observers Handbook regarding the Observing Modes (Sect. 5.3) as this will assist in understanding the explanations in this document.
FIFI-LS-specific instructions and reminders of general issues are given in the following topics below. Note that all menu selections and selectable options are boldfaced, field names appear as in SSpot, and text to enter into SSpot is displayed in Courier New.
The SSPOT instructions are for SSPOT version 18.104.22.168.
If you have an approved proposal, AORs are created by selecting Download AORs From DCS... in the File menu. To create new AORs, all FIFI-LS observing modes are covered in one Astronomical Observing Template (AOT) accessible from the one FIFI-LS entry in the SSPOT Observation menu. The FIFI-LS specific parameters are distributed over three panels in SSPOT. The Config panel covers the grating configuration, i.e. the wavelength settings. The Mode panel sets the observing mode (Symmetric, Asymmetric Chop Mode, etc.) and the associated chop and nod parameters. The integration time and map parameters are set in the Map panel.
More general instrument independent, optional parameters are covered here on the FORCAST page for SSPOT. Consult the SSPOT Users Guide, which came with the application, for the general usage of SSPOT. If an altitude higher than 38,000 ft was entered in the Exposure Time Estimator, select Low or VeryLow for Requested WV Overburden in the window accessed via the Observing Condition & Acquisition/Tracking button.
The FIFI-LS Specific Panels
The first parameter, Observation Order, informs the instrument scientist in which order the observations should be carried out. In AORs for different targets, the number can be identical and the order is dictated by the observing schedule. However, for AORs with the same target, an order needs to be established. If identical numbers are used for Observation Order on the same target, SSPOT will complain. This information helps the instrument scientist to prepare the observations for execution by defining the Observation Order.
Otherwise, the Config panel allows to set the grating configuration. The user enters the rest wavelengths for the blue (Rest Wavelength Blue field) and red (Rest Wavelength Red field) transition to be observed with this AOR. The rest wavelengths need to be accurate to 0.001μm. Line lists are available at the MPE Garching. For both transitions also enter the width of the spectral feature of interest and the total width of the spectrum to be observed in km/s except for the Spectral Scan mode where the unit is microns. The Width of Spectral Feature is only used by the instrument scientist together with the information in the proposal to judge, if there is enough baseline on both sides of the feature, when the observation returns a spectrum of the requested width. Thus, the value used in the execution of the AOR is the second width parameter. Both width parameters for each channel can be left at 0 km/s for unresolved lines and a minimal spectral dither pattern will be executed, which will include slightly more than the bandwidth (see Sect. 5.2.1). If a wider spectrum is requested the grating scan will be adjusted to include the specified width (the observing wavelength will be in the center of the spectrum). In the map panel, adjust the observing time accordingly (factor ℓ in Sect. 5.2.2).
Enter the radial velocity of the source in km/s. The radial velocity can be rounded to 100 km/s, since the spectrum will be at least 1000 km/s wide.
One of the two dichroics needs to be selected so that an observation of both lines is possible. Typically, the 105_micron Dichroic is used unless a wavelength between 100 and 115 μm is observed. (Sect. 5.1.2).
The choice in the Primary Array field only affects the telescope pointing. It does not indicate a scientific priority. For most applications, the Primary Array can be left at Blue. This choice will place the target coordinates (plus any mapping offsets, if applicable) on the center of the blue array. Ideally this would also be the center of the red array, but actually the red array is offset almost 10''. This offset is not reflected in the SSPOT visualizations. The target coordinates will still be relatively close to the center of the red array. Choosing the red array as primary array will put the target in the center of the red array but relatively close to the edge of the blue array. Spectral 1 (FIF_BLUE) and Spectral 2 (FIF_RED) are fixed values.
In the mode panel shown below, the chopping mode and parameters are set.
The user chooses between the following Instrument Mode selections: Symmetric Chop, Asymmetric Chop (shown in screenshot), Bright Object, and Spectral Scan. When the Bright Object or Spectral Scan is selected, the Chop Type can be chosen to be either symmetrical (Sym) or asymmetrical (Asym). Otherwise, the Chop Type is fixed.
Specify the Total Chop Throw in arcseconds and the position angle for the chop. The position angle of the chop is specified as Chop Pos Angle relative to the chosen Chop Angle Coordinate system: J2000 or HORIZON. In J2000, the Chop Pos Angle runs counterclockwise from north. The choice of HORIZON selects to chop relative to the quasi-horizontal telescope coordinate system and the Chop Angle is fixed to 0 to achieve that.
If the Chop Type is asymmetric (Asym), a reference position is required. This can be done by specifying an offset from the target position or by specifying an absolute position in the Ref Type box. If specifying an absolute position (Ref Type → By Position), the Choose Position button allows the user to enter sexagesimal numbers or to resolve object names. The map offsets (see the map panel) will not be applied to the reference position unless Map Ref. Pos. is set to true.
Use the visualization in SSPOT to check the chop parameters. Make sure that you are not chopping/nodding into emission. The best estimate for continuum emission may be Herschel/PACS-photometer maps which may be available at 70 μm, 100 μm, or 160 μm, which can be loaded into SSPOT from a FITS-file. The image below is a screen shot from SSPOT visualizing the asymmetric chop with only one map position on a PACS 100 μm map. The chop and nod parameters in this example are the ones from the screenshot above. If the Chop Angle Coordinate system is HORIZON, the visualization in SSPOT cannot know the corresponding position angle on the sky and plots the chop aligned with the FOV. Different position angles can be simulated by changing the FOV Angle on the Map panel.
The concentric red and blue squares are the FIFI-LS FOVs. The star in it denotes the source coordinates. The green squares are the off-source chop separated from the target by 300" at an position angle of 240˚ (north is up here, but that depends on the orientation of the loaded background image). The turquoise squares are the reference position specified as a relative offset. A magenta square shows the off-chop for the reference position, but is outside of the image here. The yellow squares show locations of possible guide stars. The yellow circle has a diameter of about 9' and is the field-of-view of the focal plane imager (FPI).
When chopping asymmetrically, the maximum chop amplitude varies with the position angle. The maximum chop throw varies between 250" and 600". The range of position angles (PAs) where the maximum chop throw is below 600" is fixed with respect to the telescope. That means that the range of PAs with a limited chop throw is limited with respect to equatorial coordinates (J2000) depends on the rotation of field during the observation or in other words, when the observations is carried out. Since that is not known while the AORs have to be prepared, you need to enter a range of possible chop angles, if the chop throw is larger than 250". Then the button Set Chop Angle Ranges is sensitive. Use it to open a dialog box to enter range(s) of possible chop angles. The visualization above shows a possible range from 190˚ to 320˚.
Apart from the map parameters, the integration time is set on the map panel, which is shown below.
First, specify tnod (On-source exp. time per cycle) per nod cycle. Since a nod cycle must not take too long, the maximum values are 30 s and 15 s for the symmetric and asymmetric chopping, respectively. These values yield the best observing efficiency. To achieve longer exposure times, increase the number of nod Cycles to reach the desired ton, the on-source integration time per map position, as ton = cycles x tnod. The on-source exposure time ton is derived by the FIFI-LS exposure time calculator (see also Sect 5.2.2).
If shorter integration times are sufficient, the maximum values might still be the best option as the observing efficiency goes down with smaller values for tnod and the grating scan will get coarser (less spectral redundancy) as less time is available for it. The smallest tnod in the Symmetric chop mode (Sym) is 20 s and 10 s in the Asymmetric mode. For bright objects, where one chop cycle is already sufficient, i.e. ton is 10 s or less, the Bright Object mode can be used. It is more efficient because two map positions are observed per reference position.
The overhead estimate for the Spectral Scan Mode is a rough estimate for this Shared Risk mode and will depend on the exact nature of the observation. Please contact the Instrument Scientist through the helpdesk.
The field On-source exp. time reports tnod times the number of map positions. Multiply this duration with the number of cycles to get the total on-source exposure time for the whole observation or click the Observation Est... button to get the total on-source time, the overhead, and total observing time. The total duration includes a 60 s overhead to setup the observation.
The Min Contiguous Exp Time field can be left at 0 s unless a long observation ( >1 h) is requested that must not be split and scheduled on separate observing legs or flights. Set this value to the minimum duration required for an observing leg. See also Sect 4.1 of the Flight Planning White Paper.
The position angle of the FOV of FIFI-LS is specified via the "FOV angle" parameter (see also Sect. 5.1.3). If the angle is 0, the FOV is aligned so that North is up on the array. This angle rotates the FOV and any map offsets counterclockwise.
Two types of maps are supported: Grid and Custom. If Grid is selected, a rectangular grid of map positions can be specified, including an offset of the center of such a grid from the target position. If Custom is selected, the map offsets for a custom map optimized for the source geometry can be read in from a two-column csv file containing the map offsets in arcseconds. Make sure that there are no empty lines in the file. For both types, the offsets are specified along the FOV axes. The screen shot below shows the use of a custom map: three positions diagonally offset by 4" for optimal spatial sampling. The visualization below shows this map, including the -25˚ FOV rotation from the example above on top of M82 with a symmetric chop.
The map position either from Grid or Custom maps can be exported as csv files either as offsets from the source coordinate or as absolute coordinates with the respective buttons. It might be useful to create a Grid map first, export the offsets, and trim it and/or create shifted extra coverage in an editor for csv files. After importing the edited csv file, the result can be checked in the overlay.
The parameter Map Priority informs the instrument scientists how to prioritize the map observation. If Map Order is selected, the order of the map positions is strictly followed as listed in SSPOT. If for unforeseen circumstances the observing time is cut short during a flight, the last map positions might be missing but most of the map positions will have been observed as long as planned. If Coverage is selected, the map is observed by looping through the map positions a few times, which ensures that the whole map is observed if the observing time is cut short but it will be (partly) less deep than planned.
If you have any questions, please contact the SOFIA help-desk