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從plotting orbital trajectories開始,我們有以下代碼。價值已經改變爲已知的IC工作。python執行3d圖時會凍結
如果此代碼是正確的(它不能是雖然),它會產生
運行這段代碼只是凍結我的電腦或輸出絕對錯誤的地塊。有人可以幫我找到解決這個問題的方法嗎?
import numpy as np
from scipy.integrate import odeint
import matplotlib.pyplot as plt
from numpy import linspace
from mpl_toolkits.mplot3d import Axes3D
mu = 398600
# r0 = [-149.6 * 10 ** 6, 0.0, 0.0] # Initial position
# v0 = [29.9652, -5.04769, 0.0] # Initial velocity
u0 = [-4069.503, 2861.786, 4483.608, -5.114, -5.691, -5]
def deriv(u, dt):
n = -mu/np.sqrt(u[0] ** 2 + u[1] ** 2 + u[2] ** 2)
return [u[3], # dotu[0] = u[3]'
u[4], # dotu[1] = u[4]'
u[5], # dotu[2] = u[5]'
u[0] * n, # dotu[3] = u[0] * n
u[1] * n, # dotu[4] = u[1] * n
u[2] * n] # dotu[5] = u[2] * n
dt = np.arange(0.0, 24 * 3600, .01) # Time to run code in seconds'
u = odeint(deriv, u0, dt)
x, y, z, x2, y2, z2 = z.T
fig = plt.figure()
ax = fig.add_subplot(111, projection='3d')
ax.plot(x, y, z)
plt.show()