def __init__(self, name):
super(SolarSystemApp, self).__init__(name)
self.solar_system_widget = SolarSystem(self.default_width,
self.default_height)
self.use_default_layout(self.solar_system_widget)
pass
def solar_system():
# distance : in millions of km
# radius : in thousands of km, all get divided by 2 and the sun by 10 on top for size on screen
# velocity : in km/s
# mass : in kg
sun = Planet([center_w, center_h], 696.340 / 20, [0, 0], 1.989 * 10**30,
(255, 255, 0), "Sun")
mercury = Planet([center_w - 69.8, center_h], 2.439, [0, 38.86],
3.301 * 10**23, (128, 128, 128), "Mercury")
venus = Planet([center_w - 108, center_h], 6.051, [0, 35], 4.8675 * 10**24,
(255, 128, 0), "Venus")
earth = Planet([center_w - 152.1, center_h], 6.371, [0, 29.3],
5.972 * 10**24, BLUE, "Earth")
mars = Planet([center_w - 228, center_h], 3.390, [0, 21.972],
6.4185 * 10**23, RED, "Mars")
m = 1.5 * 10**29
x = 97.000436
y = 24.308753
vx = 9.3240737
vy = 8.6473146
p1 = Planet([center_w + x, center_h + y], 10, [vx / 2, -vy / 2], m, BLUE)
p2 = Planet([center_w - x, center_h - y], 10, [vx / 2, -vy / 2], m, RED)
p3 = Planet([center_w, center_h], 10, [-vx, vy], m, WHITE)
# planets = [p1, p2, p3] # 8 figure
planets = [sun, mercury, venus, mars, earth] # solar system
return planets, SolarSystem(planets)
def test_period_graph_update(self, beeman, plot, show):
try:
system = SolarSystem(3600, 10.175 * 10**3, Options.NORMAL_RUN,
"CelestialObjects")
Animation.periods_graph(100, system)
except ZeroDivisionError as err:
self.assertEqual(100, beeman.call_count)
def main():
"""
Main function
"""
system = SolarSystem(3600, 11.5517 * 10**3, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(system)
animate.plot()
def __init__(self, sys: SolarSystem):
self.solar_system = sys
self.planets = sys.get_planets()
self.mission = {
'earth': self.planets['earth'],
'mars': self.planets['mars']
}
self.velocity = 0
def test_plot_show(self, mock):
"""Test to prove that plt.show is called in plot() method.
Uses mocking
"""
self.system_probe = SolarSystem(3600, 10000, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(self.system_probe)
animate.plot()
mock.assert_called()
def test_scatterplot_show(self, mock):
"""Test used to prove that plt.show() is called once in scatter_plot method
uses mocking
"""
self.system_probe = SolarSystem(3600, 10000, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(self.system_probe)
animate.scatter_plot(100)
mock.assert_called_once()
def test_Adding_Planet(self):
"""Test used to check that the method add_planet can add a planet correctly into a system.
"""
self.write.add_planet("test",1,1,1,"blue","test")
system = SolarSystem(1,1,Options.PROBE_RUN,"test")
self.assertEqual(len(system.celestial_bodies),7)
self.assertEqual(system.celestial_bodies[len(system.celestial_bodies)-1].name,"test")
self.assertEqual(system.celestial_bodies[len(system.celestial_bodies)-1].mass,1)
self.assertEqual(system.celestial_bodies[len(system.celestial_bodies)-1].orbital_radius,1)
self.assertEqual(system.celestial_bodies[len(system.celestial_bodies)-1].type_of_object,"Planet")
def test_animate_update(self, mock, mock2):
"""Test used to prove that update beeman is calld in the animate method
Uses mocking.
"""
self.system_probe = SolarSystem(3600, 10000, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(self.system_probe)
animate.plot()
animate.init()
animate.animate(0)
mock.assert_called()
def test_scatterplot_update(self, mock, mock2):
"""Test used to prove that update_beeman() is called 100 times in scatter_plot method
if the parameter passed to scatter_plot is 100.
uses mocking
"""
self.system_probe = SolarSystem(3600, 10000, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(self.system_probe)
animate.scatter_plot(100)
mock.assert_called()
self.assertEqual(mock.call_count, 100)
def test_plot_animate(self, mock, mock2):
"""Test used to check that a FunCAnimator is used in plot()
Uses mocking
"""
mock.return_value = None
self.system_probe = SolarSystem(3600, 10000, Options.PROBE_RUN,
"CelestialObjects")
animate = Animation(self.system_probe)
animate.plot()
mock.assert_called()
def setUp(self):
"""Method that is executed begore each test and that loads all the systems used
"""
self.system_probe = SolarSystem(3600,10000,Options.PROBE_RUN,"CelestialObjects")
self.system = SolarSystem(3600,10000,Options.NORMAL_RUN,"CelestialObjects")
self.system_simple = SolarSystem(3600,10000,Options.NORMAL_RUN,"CelestialObjects")
planetA = CelestialBody("B",1,1,1,"Planet",1,10000,"blue")
star = CelestialBody("A",1,1,1,"Star",0,10000,"blue")
planets = [star,planetA]
self.system_simple.celestial_bodies = planets
self.system_simple.update_initial_acceleration()
def test_beeman(self):
"""Test used to check that Beeman's method works appropiatley.
"""
planetA = CelestialBody("B",1,1,1,"Planet",1,10000,"blue")
star = CelestialBody("A",1,1,1,"Star",0,10000,"blue")
planetB = CelestialBody("B",1,2,1,"Planet",1,10000,"blue")
planetB.position = np.array([-1.0,0.0])
planetB.velocity = np.array([0.0,-planetA.velocity[1]])
system = SolarSystem(3600,1000,Options.NORMAL_RUN,"CelestialObjects")
system.celestial_bodies = [star,planetA,planetB]
system.update_initial_acceleration()
for i in range(100):
system.update_beeman()
self.assertEqual(0.0,star.acceleration[0])
self.assertEqual(0.0,star.acceleration[1])
def energy_graph_comparisson(updates):
"""Function used to generate a comparison graph between Euler's method and Beeman's
to show conservation (or not conservation) of energy in both methods
"""
system = SolarSystem(3600, 10.175 * 10**3, Options.NORMAL_RUN,
"CelestialObjects")
energy_1 = [system.get_energy()]
system2 = SolarSystem(3600, 10.175 * 10**3, Options.NORMAL_RUN,
"CelestialObjects")
energy_2 = [system2.get_energy()]
iterate = updates
iterations = [i * 3600 for i in range(iterate + 1)]
for i in range(iterate):
energy_1.append(system.update_beeman())
energy_2.append(system2.update_euler())
plt.xlabel('time(s)')
plt.ylabel('Energy [J]')
plt.plot(iterations, energy_1, iterations, energy_2)
plt.show()
def search_velocity_to_mars(updates, tries, velocity):
"""Function used to searc for the optimal velocity for the probe to approach mars
it will do it by try and error over different values.
Returns:
(float,float): tuple of distance the minimum distance found and the speed needed to
accomplish it.
"""
start_velocity = velocity
system = SolarSystem(3600, start_velocity, Options.PROBE_RUN,
"CelestialObjects")
min_v = 0
increment = 0.001
minimum = system.distance_to_mars()
for i in range(tries):
system = SolarSystem(3600, start_velocity + i * increment,
Options.PROBE_RUN, "CelestialObjects")
for j in range(updates):
system.update_beeman()
if minimum >= system.distance_to_mars():
minimum = system.distance_to_mars()
min_v = start_velocity + i * increment
return (minimum, min_v)
vx0 = vars.vx0
vy0 = vars.vy0
a = vars.a
e = vars.e
theta0 = vars.theta0
psi0 = vars.psi0
radius = vars.radius
m_star = vars.m_star
m = vars.m
G = vars.G
names = ['Matsat','sunsun', 'Dum','og', 'Deilig', 'Juba', 'juba', 'Pizzatryne', 'Verdens ende']
sun_name = 'pleb'
fullmugg = SolarSystem()
sunsun = Sun(m_star, 0.001, np.array([0,0]), np.array([0,0]), 100000, 'sunsun')
fullmugg.addSun(sunsun)
masses = np.concatenate((np.array([m_star]), m))
radius = np.concatenate((np.array([vars.radius_star]), radius))
x0 = np.concatenate((np.array([0]), x0))
y0 = np.concatenate((np.array([0]), y0))
vx0 = np.concatenate((np.array([0]), vx0))
vy0 = np.concatenate((np.array([0]), vy0))
initial_rocket_mass = 1.456e+05/1.989e30
m_sat = 1100/1.989e30
m_rock = np.array([m_sat])
def test_period_graph_plot(self, plot, show):
system = SolarSystem(1000000, 10.175 * 10**3, Options.NORMAL_RUN,
"CelestialObjects")
system.celestial_bodies = system.celestial_bodies[0:2]
Animation.periods_graph(10, system)
show.assert_called_once()
from solar_system import SolarSystem from solar_time import UniversalTime ss = SolarSystem() ut = UniversalTime(year=2020, month=3, day=14, hour=0, minute=0, second=0) ss.plot_planets(ut, [0, 1, 2, 3])
class TestSolarSystem(unittest.TestCase):
def setUp(self):
"""Method that is executed begore each test and that loads all the systems used
"""
self.system_probe = SolarSystem(3600,10000,Options.PROBE_RUN,"CelestialObjects")
self.system = SolarSystem(3600,10000,Options.NORMAL_RUN,"CelestialObjects")
self.system_simple = SolarSystem(3600,10000,Options.NORMAL_RUN,"CelestialObjects")
planetA = CelestialBody("B",1,1,1,"Planet",1,10000,"blue")
star = CelestialBody("A",1,1,1,"Star",0,10000,"blue")
planets = [star,planetA]
self.system_simple.celestial_bodies = planets
self.system_simple.update_initial_acceleration()
def test_initial_accelerations(self):
"""Test used to check that the initial accelerations of the bodies of the systems are
not zero.
"""
for planet in self.system.celestial_bodies:
self.assertNotEqual(0.0,planet.acceleration[0])
self.assertEqual(0.0,planet.acceleration[1],planet.name)
for planet in self.system.celestial_bodies:
self.assertNotEqual(0.0,planet.acceleration[0])
if (planet.name!="Mars" and planet.name != "Probe"):
self.assertEqual(0.0,planet.acceleration[1],planet.name)
def test_potential_energy_simple(self):
"""Test used to check that the value of the potential energy for a siple system is calculated
correctly.
"""
expected_value = -CelestialBody.G
self.assertEqual(expected_value,self.system_simple.get_potential_energy())
def test_kinetic_energy_simple(self):
"""Test used to check that the value of the kinetic energy for a siple system is calculated
correctly.
"""
expected_value = 1/2 * 1 * CelestialBody.G
self.assertEqual(expected_value,self.system_simple.get_kinetic_energy())
def test_kinetic_energy(self):
"""Test used to check that the value of the kinetic energy of a system is calculated
correctly.
"""
expected_value = 0
for body in self.system.celestial_bodies:
expected_value+= 1/2 *body.mass * np.linalg.norm(body.velocity)**2
self.assertEqual(expected_value,self.system.get_kinetic_energy())
def test_potential_energy(self):
"""Test used to check that the value of the potential energy of a system is calculated
correctly.
"""
expected_value = 0
for bodyA in self.system.celestial_bodies:
for bodyB in self.system.celestial_bodies:
if bodyA.name != bodyB.name:
expected_value += -CelestialBody.G * bodyB.mass*0.5 *bodyA.mass/(np.linalg.norm(bodyB.position-bodyA.position))
self.assertEqual(expected_value,self.system.get_potential_energy())
def test_total_energy(self):
"""Test used to check that the value of the total energy of a system is calculated
correctly.
"""
potential = 0
for bodyA in self.system.celestial_bodies:
for bodyB in self.system.celestial_bodies:
if bodyA.name != bodyB.name:
potential += -CelestialBody.G * bodyB.mass*0.5 *bodyA.mass/(np.linalg.norm(bodyB.position-bodyA.position))
kinetic_energy = 0
for body in self.system.celestial_bodies:
kinetic_energy+= 1/2 *body.mass * np.linalg.norm(body.velocity)**2
self.assertEqual(potential+kinetic_energy,self.system.get_energy())
def test_distance_to_earth(self):
"""Test used to check that the initial distance between the probe and the Earth is correctly set
"""
expected_value = 6.371*10**6
self.assertEqual(expected_value,self.system_probe.distance_to_earth())
def test_euler(self):
"""Test used to check that Euler's method works appropiatley.
"""
planetA = CelestialBody("B",1,1,1,"Planet",1,10000,"blue")
star = CelestialBody("A",1,1,1,"Star",0,10000,"blue")
planetB = CelestialBody("B",1,2,1,"Planet",1,10000,"blue")
planetB.position = np.array([-1.0,0.0])
planetB.velocity = np.array([0.0,-planetA.velocity[1]])
system = SolarSystem(3600,1000,Options.NORMAL_RUN,"CelestialObjects")
system.celestial_bodies = [star,planetA,planetB]
system.update_initial_acceleration()
for i in range(100):
system.update_euler()
self.assertEqual(0.0,star.acceleration[0])
self.assertEqual(0.0,star.acceleration[1])
def test_beeman(self):
"""Test used to check that Beeman's method works appropiatley.
"""
planetA = CelestialBody("B",1,1,1,"Planet",1,10000,"blue")
star = CelestialBody("A",1,1,1,"Star",0,10000,"blue")
planetB = CelestialBody("B",1,2,1,"Planet",1,10000,"blue")
planetB.position = np.array([-1.0,0.0])
planetB.velocity = np.array([0.0,-planetA.velocity[1]])
system = SolarSystem(3600,1000,Options.NORMAL_RUN,"CelestialObjects")
system.celestial_bodies = [star,planetA,planetB]
system.update_initial_acceleration()
for i in range(100):
system.update_beeman()
self.assertEqual(0.0,star.acceleration[0])
self.assertEqual(0.0,star.acceleration[1])
def test_timeStep(self):
"""Test used to check that the variable time step is implemented.
"""
self.system_probe.update_beeman()
self.assertEqual(self.system_probe.time_step,20)
for i in range(1000):
self.system_probe.update_beeman()
self.assertEqual(self.system_probe.time_step,3600)
def test_search(self):
for body in self.system.celestial_bodies:
self.assertEqual(self.system.search_body(body.name).name,body.name)
def test_exception_search(self):
with self.assertRaises(ValueError) as context:
self.system.search_body("Probe")
self.assertTrue("The given name is not in the actual list of bodies" in str(context.exception))
def test_variable_time_step(self):
self.assertEqual(self.system_probe.time_step, 20)
self.system_probe.initial = False
self.system_probe.search_body("Probe").position = np.array([1000.0,0.0])
self.system_probe.update_beeman()
self.assertEqual(self.system_probe.time_step, 3600)
def main():
t = 0
dt = 1
s = SolarSystem(2.50e+11, "Solar System", dt, 3)
# Data info
# initial conditions obtained from date: A.D. 2020 - Jul - 18
# vector ephemeris data is obtained from: https://ssd.jpl.nasa.gov/horizons.cgi#top
# km/s converted to m/s
s.add_body(
Particle(1.9890e+30, -8.115575219749061E+05, 1.023358542970559E+06,
1.030475383803935E+04, -1.367124428632311E+01,
-7.255536346983386E0, 3.953653246527174E-01, 7.000E+06,
"Sun"))
# #
s.add_body(
Particle(6.4190e+23, 1.700911233235551E+08, -1.154793014669231E+08,
-6.623490315706909E+06, 1.455681174959298E+04,
2.208572786142721E+04, 1.059053211570298E+03, 4.000E+05,
"Mars"))
#
#
# s.add_body(Particle(5.9740e+24, 6.478846194962674E+07, -1.361379609312382E+08, 1.655851550595462E+04,
# 2.638665577941761E+04, 1.273331100378729E+04, -1.385515264764159E00, 5.000E+06, "Earth"))
# s.add_body(Particle(1.8982E+27, 2.925974889403378E+08, -7.120923141565894E+08, -3.592415407148212E+06,
# 1.192504812263601E+04, 5.588195368858322E+03, -2.898746577296276E+02, 8.000E+06, "Jupiter"))
# s.add_body(Particle(7.34767309E+22, 6.484283712254966E+07, -1.357523313359251E+08, 1.235756001138687E+04,
# 2.538303859564986E+04, 1.282111106220561E+04, 9.061949758449295E+01, 5.000E+04, "Moon (Earth)"))
while t < 25000:
vpy.rate(100)
s.net_forces()
s.acceleration()
s.velocity()
t += dt
s.plot()
def test_WrittingFile(self):
"""Test used to check that the method write_file works correctly.
"""
system = SolarSystem(1,1,Options.PROBE_RUN,"test")
self.assertEqual(len(system.celestial_bodies),6)
