jorgepiloto

"""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""
"
"
"		   CUSTON CONFIGURATION FOR VIM
"		      Author: Jorge Martínez
"
"""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""

""""""""""""""""""""""""""""""""""""""""""""""""""" VIM General: Configuration
set nocompatible              " required

jorgepiloto

""" This script holds the function for plotting the groundtracks. """

# Poliastro modules
from poliastro.twobody import Orbit
from poliastro.bodies import Earth

# Astropy modules
from astropy import coordinates as coord
from astropy import units as u

jorgepiloto

Σ Φ Ψ Ξ Δ λ Ψ Δ Λ Σ Φ Δ λ Ψ ξ Δ ϗ Ξ Δ Φ Ψ Ξ ϑ λ Ψ Λ Σ Θ ϑ Ξ ϗ Φ ϑ λ Ψ Σ Ξ Ψ λ ϑ Ξ Ψ ζ β Σ φ Δ Ψ Σ Φ Ψ Σ Ξ Ψ ξ Λ ϗ Ξ Ξ ϑ Ψ ϖ Σ Ξ Ψ Π Σ ϖ Λ Σ φ Δ Ξ Ψ Ω Ψ Π Λ Σ Φ ϖ ϗ ϖ ϑ Ψ Δ Ψ Ξ Δ Ψ Θ Δ φ ϗ Δ Ψ ϖ Σ Ψ Ξ ϑ λ Ψ Γ Δ Θ ϗ Φ ϑ λ Ψ Σ Ξ Ψ Δ Λ Λ ϗ Σ Λ ϑ Ψ α Δ Ψ Σ Ξ Ψ Δ Λ Λ ϗ Σ Λ ϑ Ψ α Δ Ψ Σ λ Ψ ξ Δ Φ ϖ Σ Λ Δ Ψ ϖ Σ Ψ Φ ϗ Σ ξ Ξ Δ Ψ λ β Ψ Π ϑ Φ Γ Ρ ϑ Ψ Δ Ξ Ψ α ϗ Σ Φ μ ϑ Ψ Ξ ϑ Ψ λ Δ Ξ β ϖ Δ Φ Ψ Ξ Δ λ Ψ ε Ξ Δ β μ Δ λ Ψ ϖ Σ Ξ Ψ Π Δ ζ ϑ Φ Δ Ξ Ψ Ω Ψ Δ Φ ϗ Θ Δ Φ ϖ ϑ Ψ Ξ Δ Ψ μ Λ ϑ Π Δ Ψ Π Δ Λ Ψ Σ λ ϑ λ Ψ Γ Σ Λ Λ ϑ λ Ψ Σ Ξ Ψ Δ Λ Λ ϗ Σ Λ ϑ Ψ α Δ Ψ Σ Ξ Ψ Δ Λ Λ ϗ Σ Λ ϑ Ψ α Δ Ψ Ξ Δ λ Ψ Π Σ Φ Δ λ Ψ Ω Ψ Ξ Δ λ Ψ α Δ η β ϗ μ Δ λ Ψ λ Σ Ψ α Δ Φ Ψ Π Δ Λ Ψ Ξ Δ Ψ Θ ϗ λ Θ Δ Ψ λ Σ Φ ϖ Δ Ψ Ξ Δ λ Ψ Π Σ Φ Δ λ Ψ λ ϑ Φ Ψ ϖ Σ Ψ Φ ϑ λ ϑ μ Λ ϑ λ Ψ Ξ Δ λ Ψ α Δ η β ϗ μ Δ λ Ψ λ ϑ Φ Ψ Δ ζ Σ Φ Δ λ 

jorgepiloto

import numpy as np
from astropy import units as u

from poliastro.bodies import Earth
from poliastro.core.angles import (
    E_to_nu,
    _kepler_equation,
    _kepler_equation_prime,
    nu_to_M,
)

jorgepiloto

from astropy import units as u

from poliastro.bodies import Earth
from poliastro.twobody import Orbit
from poliastro.twobody.propagation import cowell, kepler_improved


def test_near_parabolic_orbit():
    """ Compares Cowell and Kepler improved propagators for bug in #474. """
    r = [8.0e3, 1.0e3, 0.0] * u.km

jorgepiloto

import matplotlib.pyplot as plt
from astropy import units as u
from astropy.time import Time

from poliastro.bodies import Earth
from poliastro.frames import GeocentricSolarEcliptic
from poliastro.plotting.static import StaticOrbitPlotter
from poliastro.twobody import Orbit

EPOCH = Time("2018-02-19")

jorgepiloto

import matplotlib.pyplot as plt
from astropy import units as u
from astropy.time import Time

from poliastro.bodies import Earth, Mars
from poliastro.maneuver import Maneuver
from poliastro.plotting.static import StaticOrbitPlotter
from poliastro.twobody import Orbit

# Departure and time of flight for the mission

jorgepiloto

from astropy import units as u
from poliastro.twobody.angles import nu_to_M
from poliastro.core.angles import nu_to_M as nu_to_M_core

nu = 150 * u.deg
ecc = 0.08 * u.one

# If making use of radians in high-level function
M = nu_to_M(nu.to(u.rad), ecc)
print("\nHigh level function radian input results")

jorgepiloto

from astropy.io import ascii                                                    
from astropy import units as u                                                  
from poliastro.atmosphere.models import COESA62                                 
from prettytable import PrettyTable                                             
import numpy as np                                                              
                                                                                 
coesa62 = COESA62()                                                             
                                                                                 
t = PrettyTable()                                                               
t.align='l'                                                                     

jorgepiloto

# -*- coding: utf-8 -*-
"""
Introductory example - Plotting sin
===================================

This is a general example demonstrating a Matplotlib plot output, embedded
rST, the use of math notation and cross-linking to other examples. It would be
useful to compare the :download:`source Python file <plot_0_sin.py>` with the
output below.