Tutorial on Visualizing Solar System Observations in APT

Visualizing the instrument field of view for a Solar System observation along a Solar System moving target trajectory, including dithers, in the JWST Astronomer's Proposal Tool (APT), is covered in this article.

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See also: JWST Astronomers Proposal Tool Overview

Words in bold are GUI menus/
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bold italics are buttons in GUI
tools or package parameters.

For Cycle 4,  APT includes the capability to display an Aladin visualization of a moving target on-sky track, instrument field of view, and  dithers. Alternatively, moving target observers can use a fixed target as a proxy to visualize their dithers. Allowed instrument field of view orientation (position angle, or PA) can be determined using the Moving Target Visibility Tool (MTVT), or  from within APT.

This article describes how to determine allowed PA's using APT. Prior to visualizing a Solar System observation in APT, an appropriate target and observation using that target must be created. See the Tutorial on Creating Solar System Targets in APT and the Tutorial on Creating Solar System Observations in APT. The article on Moving Target Field of Regard may also be helpful, especially if you wish to observe the leading or trailing side of a planetary satellite. If you have questions please contact the help desk.

This capability is primarily intended to allow observers to check for bright stars near their target once they have plan windows for an approved program and observation, and to allow visualization of dither pattern (or mosaic) coverage for an observation without having to create a fixed target proxy for their moving target. The ability to display and copy ephemeris data may be useful for some.

Observers who just need a refresher  on visualizing Solar System observations may find this much shorter JWST Help Desk Knowledge Base (KB) article helpful.



Viewing a Solar System target track with instrument FOV and dithers in Aladin

Once you have created a Solar System target and an observation of that target, you can visualize the on-sky track of the target with the instrument field of view (FOV) superposed at intervals along the track. For the center-most position along the track, the instrument FOV is displayed including all dither pointings specified in the observation. The visualization capability is coupled with APT's ability to generate a simple ephemeris for moving targets as viewed from JWST. Both capabilities are accessed via the Solar System tab in the Form Editor for the observation, as shown below.

Figure 1. Accessing the Solar System tab from within the Form Editor for an observation of a Solar System target

The Solar System tab (highlighted by the red box) provides access to special requirements particular to moving targets within the Solar System (as well as ephemeris generation and visualization capabilities for moving targets – see below for more information).


From the Solar System tab, add any constraints on the observing circumstances for your target. The fewer constraints and the wider the ranges you specify, the easier it will be to schedule your observations. Also, unless the V3PA constraint is scientifically necessary, it should be removed from the observation prior to final submission: it's purpose is simply to force Aladin to show the observation at a valid Orient.
Figure 2. Add constraints on the circumstances of your Solar System target observation

The Solar System tab provides access to special requirements particular to moving targets within the Solar System, as well as ephemeris generation and visualization capabilities for moving targets. Click the Add Observing Window button (obscured under the list of window types above) to see the available moving target special requirements. You may also wish to add constraints under the Special Requirements tab (and will see how to add a PA range special requirement below).


Once you have specified your constraints, switch to the Visit Planner (VP) view, using the button at the top of APT. Once there, follow these steps (and see Figure 3):

  1. Click on the Update Display button at the bottom to make the system compute the observability windows for your target and observation. That button will show red text if the observability windows don't reflect the current Solar System Windows, Special Requirements, or overall observation parameters you have specified. Once that calculation is complete (it can take up to a few minutes), the Update Display button will be grayed-out, and you'll see the available observing windows displayed in the VP view.
  2. In the VP view, click on the ">" symbol next to the observation and then next to the visit(s) you wish to visualize to expand full detail of the calculation.
  3. Hover your mouse over the green bars in the "Field of Regard" row of the display, taking care to also examine dates that are within the overall observability windows (black bars) at the "Observation" level in the VP view.
  4. Note the ranges of valid dates ("Observation" row) and PA range ("Field of Regard" row) you wish to use for visualization. Note that the PA range reported is for the observatory V3 axis, not the science instrument aperture PA.

Figure 3. Determining visibility windows and allowed position angles for a moving target

Use the Visit Planner (VP) to determine the date range(s) when your target can be observed, and the V3 position angle (PA) range(s) available. The PA is given by the "Range" couplet when the mouse hovers over a green bar in the "Field of Regard" (FOR) row in the expanded VP display (249°–263° in the case shown). Observers can also access V3PA range data under the Reports button at the bottom of the VP view, and selecting Total Roll Analysis. Note that the allowed range of V3 PA is date-dependent, varying within the apparition of a target within the  FOR. To obtain a valid PA range, be sure the date you examine is also within one of the black bars in the "Observation" row of the VP display.  Users must manually expand the display for the "Observation" and the visit of interest to see the "Field of Regard" details.


Once you have chosen a valid range of position angles (and the corresponding date range) for your observation, as described above, follow these steps (see Figure 4):

  1. Switch to the Form Editor using the button at the top left of the APT GUI
  2. Return to the observation you wish to visualize in the left-hand panel
  3. Open the Special Requirements tab
  4. Add a PA Range special requirement, entering the range you determined above. At any given time the allowed PA range is approximately ±10°, but the allowed PA range over a span of days will be larger.

These steps are necessary because APT does not know when your observation will be scheduled (even if you specify so many constraints there is only a single time at which it can be scheduled). Adding the PA range special requirement will also force the correct orientation of the instrument field of view when you visualize your observation.

Figure 4. Adding a Position Angle (PA Range) range special requirement

Red boxes highlight the steps for adding a PA Range special requirement. This is needed so that the visualization in Aladin will show the instrument field of view at a valid position angle. Note: The APT Visit Planner reports valid V3 PA values, not aperture PA—be sure to enter the PA Range for V3 in the dialog for the PA range.


Once the observation has been completely defined, including adding the PA Range window described above, the target track and instrument field of view can be visualized in Aladin. The first step is to generate the ephemeris (see Figure 5):

  1. In the APT Form Editor, return to the Solar System tab on the observation
  2. Click the Generate New Ephemeris button at the bottom of the Solar System tab
  3. Enter the date range (or dates within the range) that you noted from above
  4. You can select JWST or Earth as the Ephemeris Center in the dialog; use JWST
  5. Enter a Step Size for the ephemeris, i.e., the time between points along the ephemeris.
  6. Click Generate.
    NOTE: Initially this button is grayed out. Observers will need to click somewhere in the APT window, then Generate will become active.

Observers primarily interested in the target's track may wish to use a fairly large range of dates; if the interest is in seeing the dither pattern or mosaic coverage, only a single date is really needed. Setting the Step Size to provide a few points along the track is a good starting point. Note that for instrument apertures that are very small (like the NIRSpec IFU or MIRI MRS) it can be hard to see them plotted along the ephemeris track. Starting with a small range of dates and about 10 ephemeris points may help (see Figure 7).

As of APT 2024.5, ephemeris generation is only possible for proposals that have a proposal ID (as submitted and approved proposals do). If you are working on a draft proposal you can submit your proposal and it will be given a proposal ID. Then you can resubmit later when the proposal is completed.  You can note in the title and/or abstract that is a test submission. 

Figure 5. Ephemeris generation for a moving target

At the bottom of the Solar System tab the ephemeris of the target can be generated (and must be for visualization). See notes in the text above for choosing values to enter after clicking the Generate New Ephemeris button.


Ephemeris generation is usually fairly quick (< 1 min). Once complete, the observer-supplied parameters used to generate the ephemeris, as well as the start and end on-sky position will be shown below the Generate New Ephemeris button. 
Figure 6. Ephemeris complete, ready to visualize

Once the ephemeris has been generated, it can be viewed (and the values can be copied by selecting a range of rows in the displayed table) using the View Ephemeris Table button. The moving target positions and instrument FOV can also be visualized at this point by clicking the View in Aladin button at the top of the APT window. Red boxes highlight these buttons in the figure.


Clicking the View in Aladin button at the top of the APT GUI will open the Aladin window, with the instrument FOV displayed at the date range and spacing specified in the Generate New Ephemeris step, above. Points along the ephemeris are not connected by lines (the orange lines in Figure 7 were added). For this NIRSpec IFU observation, the  FOV is so small as to be nearly invisible at the zoom level imposed by the date range and total target motion. The simplest way to add images of the sky to the Aladin display is with the Load DSS button, highlighted in Figure 7. In particular, if Load DSS is used, it is easy to update the background image when the target is changed, or if the interval of the ephemeris is updated (simply hit the button after changing target or interval). If an image is displayed from within the Aladin window itself the process is more complicated, but is addressed in this knowledge base article. The Aladin viewer is discussed in the APT Aladin Viewer article.
Figure 7. Visualization of a NIRSpec IFU observation at an ephemeris interval of 3 days spanning 6 days with the Aladin window and a portion of the APT window in the Aladin view

Top: Blue dots represent the NIRSpec IFU FOV at the 3 dates specified in the Generate New Ephemeris step. Orange lines have been added to highlight the target's motion over the 6 day interval. The FOV button and and the Labels button (both highlighted in red boxes) can help observers locate the instrument FOV when zoomed out and get oriented to the JWST focal plane. Bottom: A zoomed-in view of the central ephemeris position in the top view. Images of the sky are best added using the Load DSS button in the View in Aladin view of the main APT window (red rectangle at upper-right in both panels). An interactive tool for varying the PA of the observation can be added using the Orient Ranges button in the View in Aladin view of the main APT window; the green arc shows the PA range allowed by the PA range special requirement added to the observation; the V3 PA can be adjusted on-the-fly by dragging the head of the V3PA arrow around the instrument field of view.


Once the view is displayed in Aladin dither parameters can be adjusted in the Form Editor view in the APT window; changes to the dither (or mosaic) pattern will be reflected in real time in the Aladin display. If the ephemeris date range is changed significantly and a new ephemeris generated, it will be necessary to update the Aladin display by clicking the Load DSS button again. It also sometimes necessary to click a different item in the APT hierarchical tree (left panel) and then back on the observation of interest to get the footprints to update in the Aladin viewer.

As of APT 2024.5, if the ephemeris is regenerated using a different date range or step size the Aladin display will not automatically update. The work-around is to click somewhere in the proposal tree other than on the observation you are visualizing, and then click on that observation. The Aladin display will update to show the ephemeris and instrument FOVs using the latest ephemeris generation parameters.

The Clear Ephemeris button will simply clear the ephemeris currently in memory (including deleting the ephemeris table data), but will not change the Aladin display.

Limitations:

  • APT / Aladin does not support visualizations of planets and their satellites, neither in their apparent size nor their relative positions. Observers with approved programs can request assistance from their program coordinator, or use online tools such as NASA's Planetary Data System Ring-Moon Systems Node visualization tools (https://pds-rings.seti.org/tools/).
  • Start and end dates for ephemeris generation are not required to be consistent with periods when the target is within the JWST field of regard. The ephemeris table and on-sky visualization can, then, include dates when the target is not actually observable from JWST. Observers should be sure to specify date ranges that are consistent with the observation windows in the Visit Planner.
  • Dithers are only shown for the middle time and position along the ephemeris track (or the time just following the mid-time, if an even number of steps are specified). Dithers are executed the same way regardless of pointing or track rate, so this is a fairly minor limitation.
  • Observers must re-enter all fields presented after clicking the Generate New Ephemeris button.
  • A valid proposal ID (number) must be present on the cover sheet of the proposal. See the note above Figure 5 for more information.



Viewing dithers with a fixed target  proxy for a moving target (legacy method)

The example below defines a fixed target, M35 (an open cluster on the ecliptic), as a proxy for Callisto. Picking a proxy on the ecliptic near RA = 6hr  (as for M35) or 18hr is useful because the allowed V3 position angles are parallel, to within ±5°, with lines of constant Dec (i.e., PA near +90 or -90). Observers may instead wish to pick a fixed target near the expected positions of their moving target, but then the evaluation of the valid PA values is more complex (see above). Visualization of the instrument FOV, placement of the FOV for various dither and mosaic-tile offsets, and depth of coverage is then possible by changing (temporarily) the target of the observation from Callisto to M35.

Switching targets in APT, for example, M35 back to Callisto, will cause the Default Solar System target windows to repopulate. If you previously deleted any of the editable default target windows, you will have to do so again.

In order to visualize the dithers, click on the View in Aladin button at the top of the window. The Aladin viewer is discussed in the APT Aladin Viewer article.

Figure 8. Defining a fixed target proxy


In the Aladin window, as shown in Figure 9, any observations you have highlighted in the left sidebar will be displayed over the sky catalog of your choice (DSS, 2MASS, Simbad, etc.). 

Pan and zoom to display at the level you want. Figure 10 shows a screenshot of a NIRCam subpixel dither. 


Links

Download the Astronomer's Proposal Tool




Notable updates
  •  
    Updated with instructions for the new (APT 2024.5) capability to generate and visualize the ephemeris for a moving target observation.
Originally published