Example #1
0
    def test_compare_a_eci_to_rv(self):
        X0_mee = mee_0
        X0_rv = rv_0
        order_H = 6
        kep_dyn_mee = mee.KeplerianDynamics()
        zon_grav_mee = mee.ZonalGravity(order=order_H)
        kep_dyn_rv = rv.KeplerianDynamics()
        zon_grav_rv = rv.ZonalGravity(order=order_H)

        segs_per_orbit = 6
        segments = orbits * segs_per_orbit
        domains = [k * period / segs_per_orbit for k in range(segments + 1)]
        seg_number = len(domains) - 1
        N = (order_mcpi, ) * seg_number
        mcpi_mee = mcpyi.MCPI(kep_dyn_mee, domains, N, 'warm', X0_mee, tol)
        mcpi_rv = mcpyi.MCPI(kep_dyn_rv, domains, N, 'warm', X0_rv, tol)
        X_mee = mcpi_mee.solve_serial()(T)
        X_rv = mcpi_rv.solve_serial()(T)

        zon_grav_mee.eci_acceleration(T, convert.rv_mee(X_mee))
        zon_grav_rv.eci_acceleration(T, X_rv)

        np.testing.assert_allclose(zon_grav_mee.a_eci,
                                   zon_grav_rv.a_eci,
                                   rtol=0,
                                   atol=tol)
Example #2
0
    def test_compare_zonal_to_coe(self):
        X0_mee = mee_0
        X0_coe = coe_0
        order_H = 6
        kep_dyn_mee = mee.KeplerianDynamics()
        zon_grav_mee = mee.ZonalGravity(order=order_H)
        sysmee = utl.SystemDynamics(kep_dyn_mee, zon_grav_mee)
        kep_dyn_coe = coe.KeplerianDynamics()
        zon_grav_coe = coe.ZonalGravity(order=order_H)
        syscoe = utl.SystemDynamics(kep_dyn_coe, zon_grav_coe)

        segs_per_orbit = 6
        orbits = 1
        segments = orbits * segs_per_orbit
        domains = [k * period / segs_per_orbit for k in range(segments + 1)]
        seg_number = len(domains) - 1
        N = (order_mcpi, ) * seg_number
        mcpi_mee = mcpyi.MCPI(sysmee, domains, N, 'warm', X0_mee, tol)
        mcpi_coe = mcpyi.MCPI(syscoe, domains, N, 'warm', X0_coe, tol)
        X_mee = mcpi_mee.solve_serial()(T)
        X_coe = mcpi_coe.solve_serial()(T)

        diff = convert.mod_angles(np.abs(X_coe - convert.coe_mee(X_mee)))
        indices_2pi = np.where(2 * np.pi - tol < diff)
        diff[indices_2pi] -= 2 * np.pi

        np.testing.assert_allclose(diff, 0., rtol=0, atol=tol)
Example #3
0
    def test_zonal_gravity(self):
        X0 = mee_0
        order_H = 6
        kep_dyn = mee.KeplerianDynamics()
        zon_grav = mee.ZonalGravity(order=order_H)
        system = utl.SystemDynamics(kep_dyn, perturbations=zon_grav)

        segs_per_orbit = 6
        segments = orbits * segs_per_orbit
        domains = [k * period / segs_per_orbit for k in range(segments + 1)]
        seg_number = len(domains) - 1
        N = (order_mcpi, ) * seg_number
        mcpi = mcpyi.MCPI(system, domains, N, 'warm', X0, tol)

        X = mcpi.solve_serial()(T)

        H = mee.Hamiltonian(order=order_H)(T, X)

        np.testing.assert_allclose(H[0, 0], H, rtol=0, atol=tol * 10)
Example #4
0
    def test_compare_zonal_to_mee(self):
        X0_meeMl0 = meeMl0_0
        X0_mee = mee_0
        order_H = 6
        kep_dyn_meeMl0 = meeMl0.KeplerianDynamics()
        zon_grav_meeMl0 = meeMl0.ZonalGravity(order=order_H)
        sysmeeMl0 = utl.SystemDynamics(kep_dyn_meeMl0, zon_grav_meeMl0)
        kep_dyn_mee = mee.KeplerianDynamics()
        zon_grav_mee = mee.ZonalGravity(order=order_H)
        sysmee = utl.SystemDynamics(kep_dyn_mee, zon_grav_mee)

        segs_per_orbit = 6
        segments = orbits * segs_per_orbit
        domains = [k * period / segs_per_orbit for k in range(segments + 1)]
        seg_number = len(domains) - 1
        N = (order_mcpi, ) * seg_number
        mcpi_meeMl0 = mcpyi.MCPI(sysmeeMl0, domains, N, 'warm', X0_meeMl0, tol)
        mcpi_mee = mcpyi.MCPI(sysmee, domains, N, 'warm', X0_mee, tol)

        X_meeMl0 = mcpi_meeMl0.solve_serial()(T)
        X_mee = mcpi_mee.solve_serial()(T)
        diff = convert.mod_angles(X_mee - convert.mee_meeMl0(T, X_meeMl0))

        np.testing.assert_allclose(diff, 0.0, rtol=0, atol=tol * 10)