python-ephem
Scientific-grade astronomy routines for Python
- Developed at devel:languages:python
- Sources inherited from project openSUSE:Factory
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Source Files
Filename | Size | Changed |
---|---|---|
ephem-4.1.4.tar.gz | 0001256106 1.2 MB | |
python-ephem.changes | 0000006350 6.2 KB | |
python-ephem.spec | 0000002076 2.03 KB |
Revision 7 (latest revision is 8)
Dominique Leuenberger (dimstar_suse)
accepted
request 1046298
from
Dirk Mueller (dirkmueller)
(revision 7)
- update to 4.1.4: * A memory leak has been resolved, that was failing to free the storage for the satellite name (a Python string) and catalog number (a Python integer) when the satellite object itself was freed. * In previous versions, if you asked for the position of a body (a) whose elliptical or hyperbolic orbit has an eccentricity very close to 1.0 and (b) which is very far from perihelion, then the underlying C library would print a warning ``Near-parabolic orbit: inaccurate result`` but let your Python script continue on unawares. Now, no message is printed directly to the screen, and instead a ``RuntimeError`` will tell you why PyEphem can’t compute the body’s position. * The underlying C library should no longer produce a segmentation fault if given the floating point number ``NaN`` as a date. The Python rising and setting logic now also watches out for ``NaN`` dates, and raises a ``ValueError`` when one is detected.
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