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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 |
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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 |
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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, | |
) |
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""" 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 |
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""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""" | |
" | |
" | |
" CUSTON CONFIGURATION FOR VIM | |
" Author: Jorge Martínez | |
" | |
""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""""" | |
""""""""""""""""""""""""""""""""""""""""""""""""""" VIM General: Configuration | |
set nocompatible " required |
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