New in poliastro 0.4.2¶
Fixed packaging problems.
New in poliastro 0.4.0¶
This is a new major release, focused on improving stability and code quality. New angle conversion and modified equinoctial elements functions were added and an important backwards incompatible change was introduced related to classical orbital elements.
- Angle conversion functions: Finally brought back from poliastro 0.1, new functions were added to convert between true \(\nu\), eccentric \(E\) and mean \(M\) anomaly, see #45.
- Equinoctial elements: Now it’s possible to convert between classical and equinoctial elements, as well as from/to position and velocity vectors, see #61.
- Numerical propagation: A new propagator using SciPy Dormand & Prince 8(5,3) integrator was added, see #64.
- MIT license: The project has been relicensed to a more popular license. poliastro remains commercial-friendly through a permissive, OSI-approved license.
- Python 3.5 and NumPy 1.10 compatibility. poliastro retains compatibility with legacy Python (Python 2) and NumPy 1.9. Next version will be Python 3 only.
- Issue #62: Conversion between coe and rv is not transitive
- Issue #69: Incorrect plotting of certain closed orbits
Backward incompatible changes:
- Creation of orbits from classical elements: poliastro has
switched to the semilatus rectum \(p\) instead of the semimajor
axis \(a\) to define
Stateobjects, and the function has been renamed to
from_classical(). Please update your programs accordingly.
- Removed specific angular momentum \(h\) property to avoid a name clash
with the fourth modified equinoctial element, use
New in poliastro 0.3.1¶
This is a new minor release, with some bug fixes backported from the main development branch.
New in poliastro 0.3.0¶
This is a new major release, focused on switching to a pure Python codebase. Lambert problem solving and ephemerides computation came back, and a couple of bugs were fixed.
- Pure Python codebase: Forget about Fortran linking problems and nightmares on Windows, because now poliastro is a pure Python package. A new dependency, numba, was introduced to accelerate the algorithms, but poliastro will use it only if it is installed.
- Lambert problem solving: New module
iodto determine an orbit given two position vectors and the time of flight.
- PR #42: Planetary ephemerides computation: New module
ephemwith functions to deal with SPK files and compute position and velocity vectors of the planets.
- PR #38: New method
parabolic()to create parabolic orbits.
- New conda package: visit poliastro binstar channel!
- New organization and logo.
New in poliastro 0.2.1¶
This is a bugfix release, no new features were introduced since 0.2.0.
- Fixed #35 (failing tests with recent astropy versions), thanks to Sam Dupree for the bug report.
- Updated for recent Sphinx versions.
New in poliastro 0.2¶
- Totally refactored code to provide a more pythonic API (see PR #14 and wiki for further information) heavily inspired by Plyades by Helge Eichhorn.
- Easy plotting of orbits in two dimensions using matplotlib.
examplewith sample data to start testing the library.
These features were removed temporarily not to block the release and will see the light again in poliastro 0.3:
- Conversion between anomalies.
- Ephemerides calculations, will look into Skyfield and the JPL ephemerides prepared by Brandon Rhodes (see issue #4).
- Lambert problem solving.
- Perturbation analysis.