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Example 56 with TimeStampedPVCoordinates

use of org.orekit.utils.TimeStampedPVCoordinates in project Orekit by CS-SI.

the class YawSteeringTest method checkField.

private <T extends RealFieldElement<T>> void checkField(final Field<T> field, final GroundPointing provider, final Orbit orbit, final AbsoluteDate date, final Frame frame) throws OrekitException {
    final Attitude attitudeD = provider.getAttitude(orbit, date, frame);
    final FieldOrbit<T> orbitF = new FieldSpacecraftState<>(field, new SpacecraftState(orbit)).getOrbit();
    final FieldAbsoluteDate<T> dateF = new FieldAbsoluteDate<>(field, date);
    final FieldAttitude<T> attitudeF = provider.getAttitude(orbitF, dateF, frame);
    Assert.assertEquals(0.0, Rotation.distance(attitudeD.getRotation(), attitudeF.getRotation().toRotation()), 1.0e-15);
    Assert.assertEquals(0.0, Vector3D.distance(attitudeD.getSpin(), attitudeF.getSpin().toVector3D()), 4.0e-14);
    Assert.assertEquals(0.0, Vector3D.distance(attitudeD.getRotationAcceleration(), attitudeF.getRotationAcceleration().toVector3D()), 3.0e-12);
    final TimeStampedPVCoordinates pvD = provider.getTargetPV(orbit, date, frame);
    final TimeStampedFieldPVCoordinates<T> pvF = provider.getTargetPV(orbitF, dateF, frame);
    Assert.assertEquals(0.0, Vector3D.distance(pvD.getPosition(), pvF.getPosition().toVector3D()), 2.0e-9);
    Assert.assertEquals(0.0, Vector3D.distance(pvD.getVelocity(), pvF.getVelocity().toVector3D()), 7.0e-8);
    Assert.assertEquals(0.0, Vector3D.distance(pvD.getAcceleration(), pvF.getAcceleration().toVector3D()), 4.0e-5);
}
Also used : FieldSpacecraftState(org.orekit.propagation.FieldSpacecraftState) SpacecraftState(org.orekit.propagation.SpacecraftState) TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) FieldAbsoluteDate(org.orekit.time.FieldAbsoluteDate)

Example 57 with TimeStampedPVCoordinates

use of org.orekit.utils.TimeStampedPVCoordinates in project Orekit by CS-SI.

the class EllipseTest method testProjectionDerivatives.

@Test
public void testProjectionDerivatives() throws OrekitException {
    Ellipse e = new Ellipse(Vector3D.ZERO, Vector3D.PLUS_I, Vector3D.PLUS_J, 6.4e6, 6.3e6, FramesFactory.getGCRF());
    TimeStampedPVCoordinates linearMotion = new TimeStampedPVCoordinates(AbsoluteDate.J2000_EPOCH, new Vector3D(7.0e6, 5.0e6, 0.0), new Vector3D(3.0e3, 4.0e3, 0.0), Vector3D.ZERO);
    TimeStampedPVCoordinates g0 = e.projectToEllipse(linearMotion);
    List<TimeStampedPVCoordinates> sample = new ArrayList<TimeStampedPVCoordinates>();
    for (double dt = -0.25; dt <= 0.25; dt += 0.125) {
        sample.add(e.projectToEllipse(linearMotion.shiftedBy(dt)));
    }
    TimeStampedPVCoordinates ref = TimeStampedPVCoordinates.interpolate(g0.getDate(), CartesianDerivativesFilter.USE_P, sample);
    Assert.assertEquals(0, Vector3D.distance(g0.getPosition(), ref.getPosition()) / ref.getPosition().getNorm(), 1.0e-15);
    Assert.assertEquals(0, Vector3D.distance(g0.getVelocity(), ref.getVelocity()) / ref.getVelocity().getNorm(), 6.0e-12);
    Assert.assertEquals(0, Vector3D.distance(g0.getAcceleration(), ref.getAcceleration()) / ref.getAcceleration().getNorm(), 8.0e-8);
}
Also used : Vector3D(org.hipparchus.geometry.euclidean.threed.Vector3D) ArrayList(java.util.ArrayList) TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) Test(org.junit.Test)

Example 58 with TimeStampedPVCoordinates

use of org.orekit.utils.TimeStampedPVCoordinates in project Orekit by CS-SI.

the class OneAxisEllipsoidTest method testGroundProjectionTaylor.

@Test
public void testGroundProjectionTaylor() throws OrekitException {
    Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, true);
    Frame eme2000 = FramesFactory.getEME2000();
    OneAxisEllipsoid model = new OneAxisEllipsoid(Constants.WGS84_EARTH_EQUATORIAL_RADIUS, Constants.WGS84_EARTH_FLATTENING, itrf);
    TimeStampedPVCoordinates initPV = new TimeStampedPVCoordinates(AbsoluteDate.J2000_EPOCH.shiftedBy(584.), new Vector3D(3220103., 69623., 6449822.), new Vector3D(6414.7, -2006., -3180.), Vector3D.ZERO);
    Orbit orbit = new EquinoctialOrbit(initPV, eme2000, Constants.EIGEN5C_EARTH_MU);
    TimeStampedPVCoordinates pv0 = orbit.getPVCoordinates(orbit.getDate(), model.getBodyFrame());
    PVCoordinatesProvider groundTaylor = model.projectToGround(pv0, model.getBodyFrame()).toTaylorProvider(model.getBodyFrame());
    TimeStampedPVCoordinates g0 = groundTaylor.getPVCoordinates(orbit.getDate(), model.getBodyFrame());
    Vector3D zenith = pv0.getPosition().subtract(g0.getPosition()).normalize();
    Vector3D acrossTrack = Vector3D.crossProduct(zenith, g0.getVelocity()).normalize();
    Vector3D alongTrack = Vector3D.crossProduct(acrossTrack, zenith).normalize();
    for (double dt = -1; dt < 1; dt += 0.01) {
        AbsoluteDate date = orbit.getDate().shiftedBy(dt);
        Vector3D taylorP = groundTaylor.getPVCoordinates(date, model.getBodyFrame()).getPosition();
        Vector3D refP = model.projectToGround(orbit.getPVCoordinates(date, model.getBodyFrame()).getPosition(), date, model.getBodyFrame());
        Vector3D delta = taylorP.subtract(refP);
        Assert.assertEquals(0.0, Vector3D.dotProduct(delta, alongTrack), 0.0015);
        Assert.assertEquals(0.0, Vector3D.dotProduct(delta, acrossTrack), 0.0007);
        Assert.assertEquals(0.0, Vector3D.dotProduct(delta, zenith), 0.00002);
    }
}
Also used : Frame(org.orekit.frames.Frame) Orbit(org.orekit.orbits.Orbit) EquinoctialOrbit(org.orekit.orbits.EquinoctialOrbit) CircularOrbit(org.orekit.orbits.CircularOrbit) FieldVector3D(org.hipparchus.geometry.euclidean.threed.FieldVector3D) Vector3D(org.hipparchus.geometry.euclidean.threed.Vector3D) EquinoctialOrbit(org.orekit.orbits.EquinoctialOrbit) PVCoordinatesProvider(org.orekit.utils.PVCoordinatesProvider) TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) FieldAbsoluteDate(org.orekit.time.FieldAbsoluteDate) AbsoluteDate(org.orekit.time.AbsoluteDate) Test(org.junit.Test)

Example 59 with TimeStampedPVCoordinates

use of org.orekit.utils.TimeStampedPVCoordinates in project Orekit by CS-SI.

the class YawCompensationTest method testTarget.

/**
 * Test that pointed target remains the same with or without yaw compensation
 */
@Test
public void testTarget() throws OrekitException {
    // Attitude laws
    // **************
    // Target pointing attitude provider without yaw compensation
    NadirPointing nadirLaw = new NadirPointing(circOrbit.getFrame(), earthShape);
    // Target pointing attitude provider with yaw compensation
    YawCompensation yawCompensLaw = new YawCompensation(circOrbit.getFrame(), nadirLaw);
    // Check target
    // *************
    // without yaw compensation
    TimeStampedPVCoordinates noYawObserved = nadirLaw.getTargetPV(circOrbit, date, itrf);
    // with yaw compensation
    TimeStampedPVCoordinates yawObserved = yawCompensLaw.getTargetPV(circOrbit, date, itrf);
    // Check difference
    PVCoordinates observedDiff = new PVCoordinates(yawObserved, noYawObserved);
    Assert.assertEquals(0.0, observedDiff.getPosition().getNorm(), Utils.epsilonTest);
    Assert.assertEquals(0.0, observedDiff.getVelocity().getNorm(), Utils.epsilonTest);
    Assert.assertEquals(0.0, observedDiff.getAcceleration().getNorm(), Utils.epsilonTest);
    Assert.assertSame(nadirLaw, yawCompensLaw.getUnderlyingAttitudeProvider());
}
Also used : TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) PVCoordinates(org.orekit.utils.PVCoordinates) TimeStampedFieldPVCoordinates(org.orekit.utils.TimeStampedFieldPVCoordinates) TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) Test(org.junit.Test)

Example 60 with TimeStampedPVCoordinates

use of org.orekit.utils.TimeStampedPVCoordinates in project Orekit by CS-SI.

the class YawCompensationTest method testSlidingDerivatives.

/**
 * Test the derivatives of the sliding target
 */
@Test
public void testSlidingDerivatives() throws OrekitException {
    GroundPointing law = new YawCompensation(circOrbit.getFrame(), new NadirPointing(circOrbit.getFrame(), earthShape));
    List<TimeStampedPVCoordinates> sample = new ArrayList<TimeStampedPVCoordinates>();
    for (double dt = -0.1; dt < 0.1; dt += 0.01) {
        Orbit o = circOrbit.shiftedBy(dt);
        sample.add(law.getTargetPV(o, o.getDate(), o.getFrame()));
    }
    TimeStampedPVCoordinates reference = TimeStampedPVCoordinates.interpolate(circOrbit.getDate(), CartesianDerivativesFilter.USE_P, sample);
    TimeStampedPVCoordinates target = law.getTargetPV(circOrbit, circOrbit.getDate(), circOrbit.getFrame());
    Assert.assertEquals(0.0, Vector3D.distance(reference.getPosition(), target.getPosition()), 1.0e-15 * reference.getPosition().getNorm());
    Assert.assertEquals(0.0, Vector3D.distance(reference.getVelocity(), target.getVelocity()), 3.0e-11 * reference.getVelocity().getNorm());
    Assert.assertEquals(0.0, Vector3D.distance(reference.getAcceleration(), target.getAcceleration()), 7.0e-6 * reference.getAcceleration().getNorm());
}
Also used : FieldOrbit(org.orekit.orbits.FieldOrbit) Orbit(org.orekit.orbits.Orbit) CircularOrbit(org.orekit.orbits.CircularOrbit) KeplerianOrbit(org.orekit.orbits.KeplerianOrbit) ArrayList(java.util.ArrayList) TimeStampedPVCoordinates(org.orekit.utils.TimeStampedPVCoordinates) Test(org.junit.Test)

Aggregations

TimeStampedPVCoordinates (org.orekit.utils.TimeStampedPVCoordinates)103 Vector3D (org.hipparchus.geometry.euclidean.threed.Vector3D)64 Test (org.junit.Test)50 AbsoluteDate (org.orekit.time.AbsoluteDate)48 SpacecraftState (org.orekit.propagation.SpacecraftState)36 Frame (org.orekit.frames.Frame)27 ArrayList (java.util.ArrayList)24 FieldVector3D (org.hipparchus.geometry.euclidean.threed.FieldVector3D)23 Transform (org.orekit.frames.Transform)22 CartesianOrbit (org.orekit.orbits.CartesianOrbit)20 Orbit (org.orekit.orbits.Orbit)19 FieldAbsoluteDate (org.orekit.time.FieldAbsoluteDate)18 KeplerianOrbit (org.orekit.orbits.KeplerianOrbit)17 PVCoordinates (org.orekit.utils.PVCoordinates)17 OrekitException (org.orekit.errors.OrekitException)15 BoundedPropagator (org.orekit.propagation.BoundedPropagator)12 DSFactory (org.hipparchus.analysis.differentiation.DSFactory)11 CircularOrbit (org.orekit.orbits.CircularOrbit)11 Propagator (org.orekit.propagation.Propagator)11 FieldTransform (org.orekit.frames.FieldTransform)10