use of org.orekit.utils.FieldPVCoordinates in project Orekit by CS-SI.
the class FieldCartesianOrbitTest method doTestErr1.
private <T extends RealFieldElement<T>> void doTestErr1(Field<T> field) throws IllegalArgumentException {
T zero = field.getZero();
FieldAbsoluteDate<T> date = new FieldAbsoluteDate<>(field);
FieldVector3D<T> position = new FieldVector3D<>(zero.add(-26655470.0), zero.add(29881667.0), zero.add(-113657.0));
FieldVector3D<T> velocity = new FieldVector3D<>(zero.add(-1125.0), zero.add(-1122.0), zero.add(195.0));
FieldPVCoordinates<T> FieldPVCoordinates = new FieldPVCoordinates<>(position, velocity);
double mu = 3.9860047e14;
new FieldCartesianOrbit<>(FieldPVCoordinates, new Frame(FramesFactory.getEME2000(), Transform.IDENTITY, "non-inertial", false), date, mu);
}
use of org.orekit.utils.FieldPVCoordinates in project Orekit by CS-SI.
the class FieldCircularOrbitTest method doTestCopyNonKeplerianAcceleration.
private <T extends RealFieldElement<T>> void doTestCopyNonKeplerianAcceleration(Field<T> field) throws OrekitException {
final Frame eme2000 = FramesFactory.getEME2000();
// Define GEO satellite position
final FieldVector3D<T> position = new FieldVector3D<>(field.getZero().add(42164140), field.getZero(), field.getZero());
// Build PVCoodrinates starting from its position and computing the corresponding circular velocity
final FieldPVCoordinates<T> pv = new FieldPVCoordinates<>(position, new FieldVector3D<>(field.getZero(), position.getNorm().reciprocal().multiply(mu).sqrt(), field.getZero()));
// Build a KeplerianOrbit in eme2000
final FieldOrbit<T> orbit = new FieldCircularOrbit<>(pv, eme2000, FieldAbsoluteDate.getJ2000Epoch(field), mu);
// Build another KeplerianOrbit as a copy of the first one
final FieldOrbit<T> orbitCopy = new FieldCircularOrbit<>(orbit);
// Shift the orbit of a time-interval
// This works good
final FieldOrbit<T> shiftedOrbit = orbit.shiftedBy(10);
// This does not work
final FieldOrbit<T> shiftedOrbitCopy = orbitCopy.shiftedBy(10);
Assert.assertEquals(0.0, FieldVector3D.distance(shiftedOrbit.getPVCoordinates().getPosition(), shiftedOrbitCopy.getPVCoordinates().getPosition()).getReal(), 1.0e-10);
Assert.assertEquals(0.0, FieldVector3D.distance(shiftedOrbit.getPVCoordinates().getVelocity(), shiftedOrbitCopy.getPVCoordinates().getVelocity()).getReal(), 1.0e-10);
}
use of org.orekit.utils.FieldPVCoordinates in project Orekit by CS-SI.
the class FieldEquinoctialOrbitTest method doTestCopyNonKeplerianAcceleration.
private <T extends RealFieldElement<T>> void doTestCopyNonKeplerianAcceleration(Field<T> field) throws OrekitException {
final Frame eme2000 = FramesFactory.getEME2000();
// Define GEO satellite position
final FieldVector3D<T> position = new FieldVector3D<>(field.getZero().add(42164140), field.getZero(), field.getZero());
// Build PVCoodrinates starting from its position and computing the corresponding circular velocity
final FieldPVCoordinates<T> pv = new FieldPVCoordinates<>(position, new FieldVector3D<>(field.getZero(), position.getNorm().reciprocal().multiply(mu).sqrt(), field.getZero()));
// Build a KeplerianOrbit in eme2000
final FieldOrbit<T> orbit = new FieldKeplerianOrbit<>(pv, eme2000, FieldAbsoluteDate.getJ2000Epoch(field), mu);
// Build another KeplerianOrbit as a copy of the first one
final FieldOrbit<T> orbitCopy = new FieldKeplerianOrbit<>(orbit);
// Shift the orbit of a time-interval
// This works good
final FieldOrbit<T> shiftedOrbit = orbit.shiftedBy(10);
// This does not work
final FieldOrbit<T> shiftedOrbitCopy = orbitCopy.shiftedBy(10);
Assert.assertEquals(0.0, FieldVector3D.distance(shiftedOrbit.getPVCoordinates().getPosition(), shiftedOrbitCopy.getPVCoordinates().getPosition()).getReal(), 1.0e-10);
Assert.assertEquals(0.0, FieldVector3D.distance(shiftedOrbit.getPVCoordinates().getVelocity(), shiftedOrbitCopy.getPVCoordinates().getVelocity()).getReal(), 1.0e-10);
}
use of org.orekit.utils.FieldPVCoordinates in project Orekit by CS-SI.
the class FieldKeplerianOrbitTest method doTestNonInertialFrame.
private <T extends RealFieldElement<T>> void doTestNonInertialFrame(final Field<T> field) throws IllegalArgumentException {
FieldAbsoluteDate<T> date = new FieldAbsoluteDate<>(field);
FieldVector3D<T> position = new FieldVector3D<>(field.getZero().add(-4947831.), field.getZero().add(-3765382.), field.getZero().add(-3708221.));
FieldVector3D<T> velocity = new FieldVector3D<>(field.getZero().add(-2079.), field.getZero().add(5291.), field.getZero().add(-7842.));
FieldPVCoordinates<T> pvCoordinates = new FieldPVCoordinates<>(position, velocity);
new FieldKeplerianOrbit<>(pvCoordinates, new Frame(FramesFactory.getEME2000(), Transform.IDENTITY, "non-inertial", false), date, mu);
}
use of org.orekit.utils.FieldPVCoordinates in project Orekit by CS-SI.
the class FieldTransformTest method doTestJacobianPVA.
private <T extends RealFieldElement<T>> void doTestJacobianPVA(Field<T> field) {
// base directions for finite differences
@SuppressWarnings("unchecked") FieldPVCoordinates<T>[] directions = (FieldPVCoordinates<T>[]) Array.newInstance(FieldPVCoordinates.class, 9);
directions[0] = new FieldPVCoordinates<>(FieldVector3D.getPlusI(field), FieldVector3D.getZero(field), FieldVector3D.getZero(field));
directions[1] = new FieldPVCoordinates<>(FieldVector3D.getPlusJ(field), FieldVector3D.getZero(field), FieldVector3D.getZero(field));
directions[2] = new FieldPVCoordinates<>(FieldVector3D.getPlusK(field), FieldVector3D.getZero(field), FieldVector3D.getZero(field));
directions[3] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getPlusI(field), FieldVector3D.getZero(field));
directions[4] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getPlusJ(field), FieldVector3D.getZero(field));
directions[5] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getPlusK(field), FieldVector3D.getZero(field));
directions[6] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getZero(field), FieldVector3D.getPlusI(field));
directions[7] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getZero(field), FieldVector3D.getPlusJ(field));
directions[8] = new FieldPVCoordinates<>(FieldVector3D.getZero(field), FieldVector3D.getZero(field), FieldVector3D.getPlusK(field));
double h = 0.01;
RandomGenerator random = new Well19937a(0xd223e88b6232198fl);
for (int i = 0; i < 20; ++i) {
// generate a random transform
FieldTransform<T> combined = randomTransform(field, random);
// compute Jacobian
T[][] jacobian = MathArrays.buildArray(field, 9, 9);
for (int l = 0; l < jacobian.length; ++l) {
for (int c = 0; c < jacobian[l].length; ++c) {
jacobian[l][c] = field.getZero().add(1 + 0.1 * c);
}
}
combined.getJacobian(CartesianDerivativesFilter.USE_PVA, jacobian);
for (int j = 0; j < 100; ++j) {
FieldPVCoordinates<T> pv0 = new FieldPVCoordinates<>(randomVector(field, 1e3, random), randomVector(field, 1.0, random), randomVector(field, 1.0e-3, random));
double epsilonP = 2.0e-12 * pv0.getPosition().getNorm().getReal();
double epsilonV = 6.0e-11 * pv0.getVelocity().getNorm().getReal();
double epsilonA = 2.0e-9 * pv0.getAcceleration().getNorm().getReal();
for (int c = 0; c < directions.length; ++c) {
// eight points finite differences estimation of a Jacobian column
FieldPVCoordinates<T> pvm4h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, -4 * h, directions[c]));
FieldPVCoordinates<T> pvm3h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, -3 * h, directions[c]));
FieldPVCoordinates<T> pvm2h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, -2 * h, directions[c]));
FieldPVCoordinates<T> pvm1h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, -1 * h, directions[c]));
FieldPVCoordinates<T> pvp1h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, +1 * h, directions[c]));
FieldPVCoordinates<T> pvp2h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, +2 * h, directions[c]));
FieldPVCoordinates<T> pvp3h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, +3 * h, directions[c]));
FieldPVCoordinates<T> pvp4h = combined.transformPVCoordinates(new FieldPVCoordinates<>(1.0, pv0, +4 * h, directions[c]));
FieldPVCoordinates<T> d4 = new FieldPVCoordinates<>(pvm4h, pvp4h);
FieldPVCoordinates<T> d3 = new FieldPVCoordinates<>(pvm3h, pvp3h);
FieldPVCoordinates<T> d2 = new FieldPVCoordinates<>(pvm2h, pvp2h);
FieldPVCoordinates<T> d1 = new FieldPVCoordinates<>(pvm1h, pvp1h);
double d = 1.0 / (840 * h);
FieldPVCoordinates<T> estimatedColumn = new FieldPVCoordinates<>(-3 * d, d4, 32 * d, d3, -168 * d, d2, 672 * d, d1);
// check analytical Jacobian against finite difference reference
Assert.assertEquals(estimatedColumn.getPosition().getX().getReal(), jacobian[0][c].getReal(), epsilonP);
Assert.assertEquals(estimatedColumn.getPosition().getY().getReal(), jacobian[1][c].getReal(), epsilonP);
Assert.assertEquals(estimatedColumn.getPosition().getZ().getReal(), jacobian[2][c].getReal(), epsilonP);
Assert.assertEquals(estimatedColumn.getVelocity().getX().getReal(), jacobian[3][c].getReal(), epsilonV);
Assert.assertEquals(estimatedColumn.getVelocity().getY().getReal(), jacobian[4][c].getReal(), epsilonV);
Assert.assertEquals(estimatedColumn.getVelocity().getZ().getReal(), jacobian[5][c].getReal(), epsilonV);
Assert.assertEquals(estimatedColumn.getAcceleration().getX().getReal(), jacobian[6][c].getReal(), epsilonA);
Assert.assertEquals(estimatedColumn.getAcceleration().getY().getReal(), jacobian[7][c].getReal(), epsilonA);
Assert.assertEquals(estimatedColumn.getAcceleration().getZ().getReal(), jacobian[8][c].getReal(), epsilonA);
}
}
}
}
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