franzbinder

from astropy.time import Time
from poliastro.twobody import propagation
from typing import List
from poliastro.twobody import Orbit
from poliastro.bodies import  Sun
import matplotlib as mpl
import numpy as np
from astropy import units as u
from astropy.coordinates import CartesianRepresentation
from matplotlib import pyplot as plt

franzbinder

Traceback (most recent call last):
  File "C:/Users/taiko/PycharmProjects/untitled/solar_system_toy.py", line 125, in <module>
    orbit_list[idx] = orbit_list[idx].propagate(1*u.day,method=cowell,ad=ad)
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\orbit.py", line 999, in propagate
    cartesian = propagate(self, time_of_flight, method=method, rtol=rtol, **kwargs)
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\propagation.py", line 468, in propagate
    orbit.attractor.k, orbit.r, orbit.v, time_of_flight.to(u.s), rtol=rtol, **kwargs
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\poliastro\twobody\propagation.py", line 105, in cowell
    dense_output=True,
  File "C:\Users\taiko\AppData\Local\Programs\Python\Python37-32\lib\site-packages\scipy\integrate\_ivp\ivp.py", line 477, in solve_ivp