def test_flight_path_angle():
# Data from Curtis, example 2.5
nu = 109.5 # deg
ecc = 0.6
expected_gamma = 35.26 # deg
gamma = angles.fp_angle(np.deg2rad(nu), ecc)
assert_almost_equal(gamma, np.deg2rad(expected_gamma), decimal=3)
def test_flight_path_angle():
# Data from Curtis, example 2.5
nu = 109.5 * u.deg
ecc = 0.6 * u.one
expected_gamma = 35.26 * u.deg
gamma = angles.fp_angle(np.deg2rad(nu), ecc)
assert_almost_equal(gamma.to(u.rad).value, expected_gamma.to(u.rad).value,
decimal=3)
def test_flight_path_angle():
# Data from Curtis, example 2.5
nu = 109.5 * u.deg
ecc = 0.6 * u.one
expected_gamma = 35.26 * u.deg
gamma = angles.fp_angle(np.deg2rad(nu), ecc)
assert_quantity_allclose(gamma, expected_gamma, rtol=1e-3)
def test_flight_path_angle():
# Data from Curtis, example 2.5
nu = 109.5 * u.deg
ecc = 0.6 * u.one
expected_gamma = 35.26 * u.deg
gamma = angles.fp_angle(np.deg2rad(nu), ecc)
assert_quantity_allclose(gamma, expected_gamma, rtol=1e-3)
def test_flight_path_angle():
# Data from Curtis, example 2.5
nu = 109.5 * u.deg
ecc = 0.6 * u.one
expected_gamma = 35.26 * u.deg
gamma = angles.fp_angle(np.deg2rad(nu), ecc)
assert_almost_equal(gamma.to(u.rad).value,
expected_gamma.to(u.rad).value,
decimal=3)
