def test_inertia_eigenvec(self, value):
state = np.array([1., 0., 0., 0., 0.1, -0.02, -0.2])
mySat = Satellite(state, 128.05)
mySat.setPos(value)
mySat.setVel(np.array([5.60, -5.0, 0.0]))
result = dist.gg_torque(mySat)
self.assertTrue(np.allclose(result, [0., 0., 0.]))
def test_gg_data_type(self):
sat = Satellite(np.array([1., 0., 0., 0., 0., 0., 0.]), 13.)
sat.setPos(np.array([7070e3, 0., 0.]))
result = dist.gg_torque(sat)
self.assertEqual(type(result), np.ndarray)