예제 #1
0
파일: test_filt.py 프로젝트: nmayorov/pyins
def test_propagate_errors():
    # This test is complex and hardly a unit test, but it is strong.
    # I believe it's better than a formal test.
    dt = 0.5
    t = 6 * 3600
    n_samples = int(t / dt)
    lat = np.full(n_samples, 50.0)
    lon = np.full(n_samples, 60.0)
    alt = np.zeros_like(lat)
    h = np.full(n_samples, 10.0)
    r = np.full(n_samples, -5.0)
    p = np.full(n_samples, 3.0)

    traj, gyro, accel = sim.from_position(dt, lat, lon, alt, h, p, r)

    gyro_bias = np.array([1e-8, -2e-8, 3e-8])
    accel_bias = np.array([3e-3, -4e-3, 2e-3])

    gyro += gyro_bias * dt
    accel += accel_bias * dt
    theta, dv = coning_sculling(gyro, accel)

    d_lat = 100
    d_lon = -200
    d_VE = 1
    d_VN = -2
    d_h = 0.01
    d_p = -0.02
    d_r = 0.03

    lat0, lon0 = perturb_ll(traj.lat[0], traj.lon[0], d_lat, d_lon)
    VE0 = traj.VE[0] + d_VE
    VN0 = traj.VN[0] + d_VN
    h0 = traj.h[0] + d_h
    p0 = traj.p[0] + d_p
    r0 = traj.r[0] + d_r

    traj_c = integrate(dt, lat0, lon0, VE0, VN0, h0, p0, r0, theta, dv)
    error_true = traj_diff(traj_c, traj)
    error_linear = propagate_errors(dt, traj, d_lat, d_lon, d_VE, d_VN, d_h,
                                    d_p, d_r, gyro_bias, accel_bias)

    error_scale = np.mean(np.abs(error_true))
    rel_diff = (error_linear - error_true) / error_scale

    assert_allclose(rel_diff.lat, 0, atol=0.1)
    assert_allclose(rel_diff.lon, 0, atol=0.1)
    assert_allclose(rel_diff.VE, 0, atol=0.1)
    assert_allclose(rel_diff.VN, 0, atol=0.1)
    assert_allclose(rel_diff.h, 0, atol=0.1)
    assert_allclose(rel_diff.p, 0, atol=0.1)
    assert_allclose(rel_diff.r, 0, atol=0.1)
예제 #2
0
파일: test_sim.py 프로젝트: tianyeeee/pyins
def test_from_position():
    dt = 1e-1
    n_points = 1000

    lat = np.full(n_points, 50.0)
    lon = np.full(n_points, 45.0)
    alt = np.zeros(n_points)
    h = np.zeros(n_points)
    p = np.zeros(n_points)
    r = np.zeros(n_points)
    VE = np.zeros(n_points)
    VN = np.zeros(n_points)
    VU = np.zeros(n_points)

    slat = np.sin(np.deg2rad(50))
    clat = (1 - slat**2)**0.5

    gyro = earth.RATE * np.array([0, clat, slat]) * dt
    accel = np.array([0, 0, earth.gravity(slat)]) * dt

    traj, gyro_g, accel_g = sim.from_position(dt, lat, lon, alt, h, p, r)
    assert_allclose(traj.lat, 50, rtol=1e-12)
    assert_allclose(traj.lon, 45, rtol=1e-12)
    assert_allclose(traj.VE, 0, atol=1e-7)
    assert_allclose(traj.VN, 0, atol=1e-7)
    assert_allclose(traj.h, 0, atol=1e-8)
    assert_allclose(traj.p, 0, atol=1e-8)
    assert_allclose(traj.r, 0, atol=1e-8)

    for i in range(3):
        assert_allclose(gyro_g[:, i], gyro[i], atol=1e-16)
        assert_allclose(accel_g[:, i], accel[i], atol=1e-7)

    traj, gyro_g, accel_g = sim.from_velocity(dt, 50, 45, 0, VE, VN, VU, h, p,
                                              r)
    assert_allclose(traj.lat, 50, rtol=1e-12)
    assert_allclose(traj.lon, 45, rtol=1e-12)
    assert_allclose(traj.VE, 0, atol=1e-7)
    assert_allclose(traj.VN, 0, atol=1e-7)
    assert_allclose(traj.h, 0, atol=1e-8)
    assert_allclose(traj.p, 0, atol=1e-8)
    assert_allclose(traj.r, 0, atol=1e-8)

    for i in range(3):
        assert_allclose(gyro_g[:, i], gyro[i], atol=1e-16)
        assert_allclose(accel_g[:, i], accel[i], atol=1e-7)
예제 #3
0
파일: test_filt.py 프로젝트: nmayorov/pyins
def test_FeedbackFilter():
    dt = 0.9
    traj = pd.DataFrame(index=np.arange(1 * 3600))
    traj['lat'] = 50
    traj['lon'] = 60
    traj['VE'] = 0
    traj['VN'] = 0
    traj['h'] = 0
    traj['p'] = 0
    traj['r'] = 0

    _, gyro, accel = sim.from_position(dt, traj.lat, traj.lon,
                                       np.zeros_like(traj.lat),
                                       h=traj.h, p=traj.p, r=traj.r)
    theta, dv = coning_sculling(gyro, accel)

    np.random.seed(0)
    obs_data = pd.DataFrame(
        index=traj.index[::10],
        data={
            'lat': traj.lat[::10],
            'lon': traj.lon[::10]
        }
    )
    obs_data['lat'], obs_data['lon'] = perturb_ll(
        obs_data.lat, obs_data.lon,
        10 * np.random.randn(obs_data.shape[0]),
        10 * np.random.randn(obs_data.shape[0]))

    obs = LatLonObs(obs_data, 10)

    f = FeedbackFilter(dt, 5, 1, 0.2, 0.05)

    d_lat = 5
    d_lon = -3
    d_VE = 1
    d_VN = -1
    d_h = 0.1
    d_p = 0.03
    d_r = -0.02

    lat0, lon0 = perturb_ll(50, 60, d_lat, d_lon)
    integrator = Integrator(dt, lat0, lon0, d_VE, d_VN, d_h, d_p, d_r)
    res = f.run(integrator, theta, dv, observations=[obs])
    error = traj_diff(res.traj, traj)
    error = error.iloc[3000:]

    assert_allclose(error.lat, 0, rtol=0, atol=10)
    assert_allclose(error.lon, 0, rtol=0, atol=10)
    assert_allclose(error.VE, 0, rtol=0, atol=1e-2)
    assert_allclose(error.VN, 0, rtol=0, atol=1e-2)
    assert_allclose(error.h, 0, rtol=0, atol=1.5e-3)
    assert_allclose(error.p, 0, rtol=0, atol=1e-4)
    assert_allclose(error.r, 0, rtol=0, atol=1e-4)
    assert_(np.all(np.abs(res.residuals[0] < 4)))

    res = f.run_smoother(integrator, theta, dv, [obs])
    error = traj_diff(res.traj, traj)
    assert_allclose(error.lat, 0, rtol=0, atol=10)
    assert_allclose(error.lon, 0, rtol=0, atol=10)
    assert_allclose(error.VE, 0, rtol=0, atol=1e-2)
    assert_allclose(error.VN, 0, rtol=0, atol=1e-2)
    assert_allclose(error.h, 0, rtol=0, atol=1.5e-3)
    assert_allclose(error.p, 0, rtol=0, atol=1e-4)
    assert_allclose(error.r, 0, rtol=0, atol=1e-4)
    assert_(np.all(np.abs(res.residuals[0] < 4)))