Examples with Vector3D org.hipparchus.geometry.euclidean.threed.Vector3D used on opensource projects

Example 6 with Vector3D

use of org.hipparchus.geometry.euclidean.threed.Vector3D in project Orekit by CS-SI.

the class PolynomialParametricAccelerationTest method testEquivalentInertialManeuverField.

@Test
public void testEquivalentInertialManeuverField() throws OrekitException {
    final double delta = FastMath.toRadians(-7.4978);
    final double alpha = FastMath.toRadians(351);
    final Vector3D direction = new Vector3D(alpha, delta);
    final double mass = 2500;
    final double isp = Double.POSITIVE_INFINITY;
    final double duration = 4000;
    final double f = 400;
    final AttitudeProvider maneuverLaw = new InertialProvider(new Rotation(direction, Vector3D.PLUS_I));
    ConstantThrustManeuver maneuver = new ConstantThrustManeuver(initialOrbit.getDate().shiftedBy(-10.0), duration, f, isp, Vector3D.PLUS_I);
    final AttitudeProvider accelerationLaw = new InertialProvider(new Rotation(direction, Vector3D.PLUS_K));
    final PolynomialParametricAcceleration inertialAcceleration = new PolynomialParametricAcceleration(direction, true, "", AbsoluteDate.J2000_EPOCH, 0);
    inertialAcceleration.getParametersDrivers()[0].setValue(f / mass);
    doTestEquivalentManeuver(Decimal64Field.getInstance(), mass, maneuverLaw, maneuver, accelerationLaw, inertialAcceleration, 3.0e-9);
}

Example 7 with Vector3D

use of org.hipparchus.geometry.euclidean.threed.Vector3D in project Orekit by CS-SI.

the class DTM2000Test method testNonEarthRotationAxisAlignedFrame.

@Test
public void testNonEarthRotationAxisAlignedFrame() throws OrekitException {
    // setup
    AbsoluteDate date = AbsoluteDate.J2000_EPOCH;
    Frame ecef = FramesFactory.getITRF(IERSConventions.IERS_2010, true);
    Rotation rotation = new Rotation(Vector3D.PLUS_I, FastMath.PI / 2, RotationConvention.VECTOR_OPERATOR);
    Frame frame = new Frame(ecef, new Transform(date, rotation), "other");
    Vector3D pEcef = new Vector3D(6378137 + 300e3, 0, 0);
    Vector3D pFrame = ecef.getTransformTo(frame, date).transformPosition(pEcef);
    PVCoordinatesProvider sun = CelestialBodyFactory.getSun();
    OneAxisEllipsoid earth = new OneAxisEllipsoid(6378136.460, 1.0 / 298.257222101, ecef);
    SolarInputs97to05 in = SolarInputs97to05.getInstance();
    earth.setAngularThreshold(1e-10);
    DTM2000 atm = new DTM2000(in, sun, earth);
    // action
    final double actual = atm.getDensity(date, pFrame, frame);
    // verify
    Assert.assertEquals(atm.getDensity(date, pEcef, ecef), actual, 0.0);
}

Example 8 with Vector3D

use of org.hipparchus.geometry.euclidean.threed.Vector3D in project Orekit by CS-SI.

the class HarrisPriesterTest method testVelocityDerivative.

@Test
public void testVelocityDerivative() throws OrekitException {
    final Frame eme2000 = FramesFactory.getEME2000();
    final HarrisPriester hp = new HarrisPriester(sun, earth);
    final Vector3D pos = earth.getBodyFrame().getTransformTo(eme2000, date).transformPosition(earth.transform(new GeodeticPoint(-1.7, 4.2, 987654.321)));
    double dP = 100.0;
    double dVxdX = gradientComponent(hp, pos, Vector3D.PLUS_I, dP, eme2000, v -> v.getX());
    double dVxdY = gradientComponent(hp, pos, Vector3D.PLUS_J, dP, eme2000, v -> v.getX());
    double dVxdZ = gradientComponent(hp, pos, Vector3D.PLUS_K, dP, eme2000, v -> v.getX());
    double dVydX = gradientComponent(hp, pos, Vector3D.PLUS_I, dP, eme2000, v -> v.getY());
    double dVydY = gradientComponent(hp, pos, Vector3D.PLUS_J, dP, eme2000, v -> v.getY());
    double dVydZ = gradientComponent(hp, pos, Vector3D.PLUS_K, dP, eme2000, v -> v.getY());
    double dVzdX = gradientComponent(hp, pos, Vector3D.PLUS_I, dP, eme2000, v -> v.getZ());
    double dVzdY = gradientComponent(hp, pos, Vector3D.PLUS_J, dP, eme2000, v -> v.getZ());
    double dVzdZ = gradientComponent(hp, pos, Vector3D.PLUS_K, dP, eme2000, v -> v.getZ());
    DSFactory factory = new DSFactory(3, 1);
    FieldVector3D<DerivativeStructure> dsPos = new FieldVector3D<>(factory.variable(0, pos.getX()), factory.variable(1, pos.getY()), factory.variable(2, pos.getZ()));
    FieldVector3D<DerivativeStructure> dsVel = hp.getVelocity(new FieldAbsoluteDate<>(factory.getDerivativeField(), date), dsPos, eme2000);
    Assert.assertEquals(dVxdX, dsVel.getX().getPartialDerivative(1, 0, 0), 1.0e-16);
    Assert.assertEquals(dVxdY, dsVel.getX().getPartialDerivative(0, 1, 0), 1.0e-16);
    Assert.assertEquals(dVxdZ, dsVel.getX().getPartialDerivative(0, 0, 1), 1.0e-16);
    Assert.assertEquals(dVydX, dsVel.getY().getPartialDerivative(1, 0, 0), 1.0e-16);
    Assert.assertEquals(dVydY, dsVel.getY().getPartialDerivative(0, 1, 0), 1.0e-16);
    Assert.assertEquals(dVydZ, dsVel.getY().getPartialDerivative(0, 0, 1), 1.0e-16);
    Assert.assertEquals(dVzdX, dsVel.getZ().getPartialDerivative(1, 0, 0), 1.0e-16);
    Assert.assertEquals(dVzdY, dsVel.getZ().getPartialDerivative(0, 1, 0), 1.0e-16);
    Assert.assertEquals(dVzdZ, dsVel.getZ().getPartialDerivative(0, 0, 1), 1.0e-16);
}

Example 9 with Vector3D

use of org.hipparchus.geometry.euclidean.threed.Vector3D in project Orekit by CS-SI.

the class HarrisPriesterTest method testUserTab.

@Test
public void testUserTab() throws OrekitException {
    final double[][] userTab = { { 100000., 4.974e+02, 4.974e+02 }, { 110000., 7.800e+01, 7.800e+01 }, { 120000., 2.490e+01, 2.400e+01 }, { 130000., 8.377e+00, 8.710e+00 }, { 140000., 3.899e+00, 4.059e+00 }, { 150000., 2.122e+00, 2.215e+00 }, { 160000., 1.263e+00, 1.344e+00 }, { 170000., 8.008e-01, 8.758e-01 }, { 180000., 5.283e-01, 6.010e-01 }, { 190000., 3.618e-01, 4.297e-01 }, { 200000., 2.557e-01, 3.162e-01 }, { 210000., 1.839e-01, 2.396e-01 }, { 220000., 1.341e-01, 1.853e-01 }, { 230000., 9.949e-02, 1.455e-01 }, { 240000., 7.488e-02, 1.157e-01 }, { 250000., 5.709e-02, 9.308e-02 }, { 260000., 4.403e-02, 7.555e-02 }, { 270000., 3.430e-02, 6.182e-02 }, { 280000., 2.697e-02, 5.095e-02 }, { 290000., 2.139e-02, 4.226e-02 }, { 300000., 1.708e-02, 3.526e-02 }, { 320000., 1.099e-02, 2.511e-02 }, { 340000., 7.214e-03, 1.819e-02 }, { 360000., 4.824e-03, 1.337e-02 }, { 380000., 3.274e-03, 9.955e-03 }, { 400000., 2.249e-03, 7.492e-03 }, { 420000., 1.558e-03, 5.684e-03 }, { 440000., 1.091e-03, 4.355e-03 }, { 460000., 7.701e-04, 3.362e-03 }, { 480000., 5.474e-04, 2.612e-03 }, { 500000., 3.916e-04, 2.042e-03 }, { 520000., 2.819e-04, 1.605e-03 }, { 540000., 2.042e-04, 1.267e-03 }, { 560000., 1.488e-04, 1.005e-03 }, { 580000., 1.092e-04, 7.997e-04 }, { 600000., 8.070e-05, 6.390e-04 }, { 620000., 6.012e-05, 5.123e-04 }, { 640000., 4.519e-05, 4.121e-04 }, { 660000., 3.430e-05, 3.325e-04 }, { 680000., 2.632e-05, 2.691e-04 }, { 700000., 2.043e-05, 2.185e-04 }, { 720000., 1.607e-05, 1.779e-04 }, { 740000., 1.281e-05, 1.452e-04 }, { 760000., 1.036e-05, 1.190e-04 }, { 780000., 8.496e-06, 9.776e-05 }, { 800000., 7.069e-06, 8.059e-05 }, { 850000., 4.800e-06, 5.500e-05 }, { 900000., 3.300e-06, 3.700e-05 }, { 950000., 2.450e-06, 2.400e-05 }, { 1000000., 1.900e-06, 1.700e-05 }, { 1100000., 1.180e-06, 8.700e-06 }, { 1200000., 7.500e-07, 4.800e-06 }, { 1300000., 5.300e-07, 3.200e-06 }, { 1400000., 4.100e-07, 2.000e-06 }, { 1500000., 2.900e-07, 1.350e-06 }, { 1600000., 2.000e-07, 9.500e-07 }, { 1700000., 1.600e-07, 7.700e-07 }, { 1800000., 1.200e-07, 6.300e-07 }, { 1900000., 9.600e-08, 5.200e-07 }, { 2000000., 7.300e-08, 4.400e-07 } };
    // Position at 1500 km height
    final GeodeticPoint point = new GeodeticPoint(0, 0, 1500000.);
    final Vector3D pos = earth.transform(point);
    final HarrisPriester hp = new HarrisPriester(sun, earth, userTab);
    // COMPUTE DENSITY KG/M3 RHO
    final double rho = hp.getDensity(date, pos, earthFrame);
    Assert.assertEquals(2.9049E-7, rho, 1.0e-11);
    final HarrisPriester hp6 = new HarrisPriester(sun, earth, userTab, 6);
    final double rho6 = hp6.getDensity(date, pos, earthFrame);
    final HarrisPriester hp2 = new HarrisPriester(sun, earth, userTab, 2);
    final double rho2 = hp2.getDensity(date, pos, earthFrame);
    final double c2Psi2 = 0.02163787;
    Assert.assertEquals(c2Psi2, (rho6 - rho2) / (rho - rho2) - 1., 1.0e-8);
}

Example 10 with Vector3D

use of org.hipparchus.geometry.euclidean.threed.Vector3D in project Orekit by CS-SI.

the class HarrisPriesterTest method testParameterN.

@Test
public void testParameterN() throws OrekitException {
    final HarrisPriester hp = new HarrisPriester(sun, earth);
    // Position at 500 km height
    final GeodeticPoint point = new GeodeticPoint(0, 0, 500000.);
    final Vector3D pos = earth.transform(point);
    // COMPUTE DENSITY KG/M3 RHO
    final double rho4 = hp.getDensity(date, pos, earthFrame);
    final HarrisPriester hp2 = new HarrisPriester(sun, earth, 2);
    // COMPUTE DENSITY KG/M3 RHO
    final double rho2 = hp2.getDensity(date, pos, earthFrame);
    final HarrisPriester hp6 = new HarrisPriester(sun, earth, 6);
    // COMPUTE DENSITY KG/M3 RHO
    final double rho6 = hp6.getDensity(date, pos, earthFrame);
    final double c2Psi2 = 0.02163787;
    Assert.assertEquals(c2Psi2, (rho6 - rho2) / (rho4 - rho2) - 1., 1.e-8);
}