File: control

package info (click to toggle)
poliastro 0.17.0-2
  • links: PTS, VCS
  • area: main
  • in suites: bookworm
  • size: 7,136 kB
  • sloc: python: 17,039; makefile: 172
file content (51 lines) | stat: -rw-r--r-- 1,829 bytes parent folder | download
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
Source: poliastro
Maintainer: Debian Astro Team <debian-astro-maintainers@lists.alioth.debian.org>
Uploaders: Ole Streicher <olebole@debian.org>
Section: python
Priority: optional
Build-Depends: debhelper-compat (= 13),
               dh-python,
               flit (>= 3.2),
               pybuild-plugin-pyproject,
               python3-all,
               python3-astropy (>= 3.2~),
               python3-astroquery,
               python3-bs4,
               python3-erfa,
               python3-matplotlib,
               python3-numba,
               python3-numpy,
               python3-pandas,
               python3-plotly (>= 4~),
               python3-pytest,
               python3-pytest-doctestplus,
               python3-pytest-remotedata,
               python3-requests,
               python3-scipy,
               python3-setuptools
Standards-Version: 4.6.2
Vcs-Browser: https://salsa.debian.org/debian-astro-team/poliastro
Vcs-Git: https://salsa.debian.org/debian-astro-team/poliastro.git
Homepage: https://github.com/poliastro/poliastro
Rules-Requires-Root: no

Package: python3-poliastro
Architecture: all
Depends: python3-astropy,
         python3-astroquery,
         python3-erfa,
         python3-matplotlib,
         python3-numba,
         python3-numpy,
         python3-pandas,
         python3-plotly,
         python3-scipy,
         ${misc:Depends},
         ${python3:Depends}
Recommends: python3-numba
Description: Astrodynamics and Orbital Mechanics computations
 Poliastro is an open source pure Python package dedicated to problems
 arising in Astrodynamics and Orbital Mechanics, such as orbit
 propagation, solution of the Lambert's problem, conversion between
 position and velocity vectors and classical orbital elements and
 orbit plotting, focusing on interplanetary applications