import matplotlib.pyplot as plt
import numpy as np
if __name__ == "__main__":
fig = plt.figure(figsize=(15.2, 8))
ax = fig.add_subplot(111)
R = 10 # planet radius
pp = [0, 0] # planet position
ps = [40, 0] # satellite position
k = 2750 # force scale
dist = lambda p1, p2: np.sqrt( (p1[0]-p2[0])**2 (p1[1]-p2[1])**2 ) # Euclidean distance
irsq = lambda p: 1 / dist(p, ps)**2 # inverse square distance
gmag = lambda p: k*irsq(p) # satellite's gravity force magnitude
gdir = lambda p: np.divide(np.subtract(ps, p), dist(ps, p)) # satellite's gravity force direction
gvec = lambda p: gmag(p)*gdir(p) # satellite's gravity force vector
gp = gvec(pp) # satellite's gravity vector at center of planet
tvec = lambda p: gvec(p)-gp # satellite's tide force vector
theta = np.linspace(-np.pi, np.pi, 50) # circle internal angle
for ti in theta:
pi = [-R * np.cos(ti), R * np.sin(ti)] # evaluation point on the perimeter (planet's surface)
ti = tvec(pi) # tide at evaluation point
gi = gvec(pi) # gravity at evaluation point
ax.arrow(pp[0], pp[1], gp[0], gp[1], head_width=0.5/2, head_length=0.7/2, fc='b', color='b')
ax.arrow(pi[0], pi[1], gi[0], gi[1], head_width=0.5/2, head_length=0.7/2, fc='b', color='b')
ax.arrow(pi[0], pi[1], ti[0], ti[1], head_width=0.5/1, head_length=0.7/1, fc='r', color='r')
ax.plot(pp[0], pp[1], 'ok')
#ax.annotate(r" ", xytext=(0,0), size=30, xy=(0,0), ha="center", va="center")
ax.annotate(r"O", xytext=(-1,0), size=30, xy=(0,0), ha="center", va="center")
ax.annotate(r"S", xy=(25,0), xytext=(15,0),
size=30, va="center",
arrowprops=dict(arrowstyle="fancy", fc='k'))
ax.set_xlim(-13, 25)
ax.set_ylim(-11, 11)
ax.plot(R*np.cos(theta), R*np.sin(theta), '-k', linewidth=3.)
ax.set_aspect('equal', 'box')
ax.axis('off')
plt.savefig('field tidal.svg', bbox_inches='tight', pad_inches=.15, transparent='true')