======================= The Skyfield To-Do List ======================= This list includes both a section on immediately-reachable goals that are appropriate for sprints and collaboration, and longer-term goals that the code base is not quite ready for yet but that we do not want to forget. Sprint Possibilities ==================== * Trying to index a unit class should print help suggesting a unit be specified, similar to trying to iterate across one. * Several interesting API questions arise because of `this Stack Overflow question `_. Should I finally go through with renaming ``.position`` to ``.xyz``? Should ``.from_altaz()`` retain observer data so that a follow-up ``.altaz()`` returns the same coordinates? Should positions fully support math, so the computation of the Topos position can only be computed once? Should the result of ``.from_altaz()`` be somehow possible to connect with ``subpoint()``, which is currently stranded over on the ``Geocentric`` class — maybe ``subpoint()`` really should be a constructor on the Topos class that can take any kind of position that’s geocentered? * For #145, skip deflections of planets that can’t affect an observation. * For #145, create a good syntax for combining two ephemerides. * Expand a bit on the documentation for stars, now that they can have an epoch for their position. * Load and use the various offsets between UTC and TAI that were in effect before 1972. * When I wrote `add_deflection()` and needed to know whether Jupiter itself is available in an ephemeris, or whether the Jupiter Barycenter should be used in its place, I tried writing the test `if name not in ephemeris:`. But this sent the code into an infinite loop! Why does `in` not work on an ephemeris object? This should be fixed, and a test written to keep it fixed. * The deflection code should really use integer identifiers instead of using names, which are slower because they need decoding. * The deflection code should have a quick way to reach in and ask an ephemeris for a raw position in au, without having to spin up a body object and have it spin up a `Distance` object. * We currently download most SPICE kernels from NAIF, but have to use FTP for fetching DE422. Are the files from the two sites equivalent and do they have the same data? Should we prefer one or the other? * We should have an illustration of Earth satellite heights above the surface, plotted against a blue atmosphere fading out into the black of space as the plot goes upwards towards the top. * How can users find out what’s in an ephemeris? * The ``Timescale`` object does not currently know where its data comes from, so its ``repr()`` is pretty uninformative. Should it someday be put in charge of loading its data from the data files specified, so that its ``repr()`` can print out which leap second file and delta T file it is using? Should it also display how up to date the files are, and what leap seconds it knows about? Also: it should be told the expiration date of all of its data, so that it can print it out as part of its ``repr()``. * In `stars.rst`, document the other alternatives for how to set the RA and dec of a new Star object. * Solar and lunar eclipses. * We should implement comets and asteroids using the standard formulae (can we find a good vector version, that will match the rest of our approach?) for a Keplerian orbit. Adding more smarts to ephemeris handling ======================================== * When we add or subtract vectors, the new `VectorSum` needs to inherit an `ephemeris` from one of the segments being combined. Right now it just grabs the first one. What if, of the choices of ephemeris among the segments, grabbing the first one gives us an ephemeris that is missing several key large bodies, and so we run into an exception when `.apparent()` tries to compute gravitational deflection? Should we be more intelligent in our choice? Or should we even combine the various ephemerides our segments might offer? Or should we specifically go ahead and look for the deflectors we need and try to find a segment for them each? * And additionally: the error when not enough bodies are available for deflection maybe someday needs to be more helpful. * Bring support for Type 1 and Type 21 JPL ephemerides into Skyfield from the third-party libraries where it now lives. The routines will need to be vectorized and updated to use a Skyfield approach to vector and matrix operations. When complete and documented, make a comment at: https://github.com/skyfielders/python-skyfield/issues/350 For 2.0 ======= * Remove old deprecation warnings for pre-1.0 behaviors. * Remove support and tests for old ephemeris Python packages. Longer-term goals ================= * Make all objects that are `.observe()`’d from Earth include a sublatitude and sublongitude coordinate stating the position on Earth from which they appear directly overhead. When complete, make a note at the PyEphem GitHub issue: https://github.com/brandon-rhodes/pyephem/issues/16 * When Earth Satellites are implemented, include the orbit number of a satellite's current position in the public attributes that are set on the resulting position object, as promised in PyEphem GitHub issue: https://github.com/brandon-rhodes/pyephem/issues/15