Examples with OrekitIllegalArgumentException org.orekit.errors.OrekitIllegalArgumentException used on opensource projects

Example 1 with OrekitIllegalArgumentException

use of org.orekit.errors.OrekitIllegalArgumentException in project Orekit by CS-SI.

the class IonoModifierTest method testTurnAroundRangeIonoModifier.

@Test
public void testTurnAroundRangeIonoModifier() throws OrekitException {
    Context context = EstimationTestUtils.eccentricContext("regular-data:potential:tides");
    final NumericalPropagatorBuilder propagatorBuilder = context.createBuilder(OrbitType.KEPLERIAN, PositionAngle.TRUE, true, 1.0e-6, 60.0, 0.001);
    // Create perfect turn-around measurements
    for (Map.Entry<GroundStation, GroundStation> entry : context.TARstations.entrySet()) {
        final GroundStation masterStation = entry.getKey();
        final GroundStation slaveStation = entry.getValue();
        masterStation.getEastOffsetDriver().setSelected(true);
        masterStation.getNorthOffsetDriver().setSelected(true);
        masterStation.getZenithOffsetDriver().setSelected(true);
        slaveStation.getEastOffsetDriver().setSelected(true);
        slaveStation.getNorthOffsetDriver().setSelected(true);
        slaveStation.getZenithOffsetDriver().setSelected(true);
    }
    final Propagator propagator = EstimationTestUtils.createPropagator(context.initialOrbit, propagatorBuilder);
    final List<ObservedMeasurement<?>> measurements = EstimationTestUtils.createMeasurements(propagator, new TurnAroundRangeMeasurementCreator(context), 1.0, 3.0, 300.0);
    propagator.setSlaveMode();
    final TurnAroundRangeIonosphericDelayModifier modifier = new TurnAroundRangeIonosphericDelayModifier(model);
    for (final ObservedMeasurement<?> measurement : measurements) {
        final AbsoluteDate date = measurement.getDate();
        final SpacecraftState refstate = propagator.propagate(date);
        TurnAroundRange turnAroundRange = (TurnAroundRange) measurement;
        EstimatedMeasurement<TurnAroundRange> evalNoMod = turnAroundRange.estimate(12, 17, new SpacecraftState[] { refstate });
        Assert.assertEquals(12, evalNoMod.getIteration());
        Assert.assertEquals(17, evalNoMod.getCount());
        // Add modifier
        turnAroundRange.addModifier(modifier);
        boolean found = false;
        for (final EstimationModifier<TurnAroundRange> existing : turnAroundRange.getModifiers()) {
            found = found || existing == modifier;
        }
        Assert.assertTrue(found);
        // 
        EstimatedMeasurement<TurnAroundRange> eval = turnAroundRange.estimate(12, 17, new SpacecraftState[] { refstate });
        Assert.assertEquals(evalNoMod.getStatus(), eval.getStatus());
        eval.setStatus(EstimatedMeasurement.Status.REJECTED);
        Assert.assertEquals(EstimatedMeasurement.Status.REJECTED, eval.getStatus());
        eval.setStatus(evalNoMod.getStatus());
        try {
            eval.getParameterDerivatives(new ParameterDriver("extra", 0, 1, -1, +1));
            Assert.fail("an exception should have been thrown");
        } catch (OrekitIllegalArgumentException oiae) {
            Assert.assertEquals(OrekitMessages.UNSUPPORTED_PARAMETER_NAME, oiae.getSpecifier());
        }
        final double diffMeters = eval.getEstimatedValue()[0] - evalNoMod.getEstimatedValue()[0];
        // TODO: check threshold
        Assert.assertEquals(0.0, diffMeters, 30.0);
    }
}

Example 2 with OrekitIllegalArgumentException

use of org.orekit.errors.OrekitIllegalArgumentException in project Orekit by CS-SI.

the class OEMWriterTest method testMultisatelliteFile.

@Test
public void testMultisatelliteFile() throws OrekitException, IOException {
    final String id1 = "ID1";
    final String id2 = "ID2";
    StandInEphemerisFile file = new StandInEphemerisFile();
    file.getSatellites().put(id1, new StandInSatelliteEphemeris(id1));
    file.getSatellites().put(id2, new StandInSatelliteEphemeris(id2));
    EphemerisFile ephemerisFile = (EphemerisFile) file;
    String tempOEMFilePath = tempFolder.newFile("TestOEMMultisatellite-1.oem").toString();
    OEMWriter writer1 = new OEMWriter();
    try {
        writer1.write(tempOEMFilePath, ephemerisFile);
        fail("Should have thrown OrekitIllegalArgumentException due to multiple satellites");
    } catch (OrekitIllegalArgumentException e) {
        assertEquals(OrekitMessages.EPHEMERIS_FILE_NO_MULTI_SUPPORT, e.getSpecifier());
    }
    tempOEMFilePath = tempFolder.newFile("TestOEMMultisatellite-2.oem").toString();
    OEMWriter writer2 = new OEMWriter(OEMWriter.DEFAULT_INTERPOLATION_METHOD, null, id1, null);
    writer2.write(tempOEMFilePath, ephemerisFile);
}

Example 3 with OrekitIllegalArgumentException

use of org.orekit.errors.OrekitIllegalArgumentException in project Orekit by CS-SI.

the class OEMWriterTest method testNullFile.

@Test
public void testNullFile() throws OrekitException, IOException {
    final String ex = "/ccsds/OEMExample.txt";
    final InputStream inEntry = getClass().getResourceAsStream(ex);
    final OEMParser parser = new OEMParser().withMu(CelestialBodyFactory.getEarth().getGM()).withConventions(IERSConventions.IERS_2010);
    final OEMFile oemFile = parser.parse(inEntry, "OEMExample.txt");
    final EphemerisFile ephemerisFile = (EphemerisFile) oemFile;
    String originator = oemFile.getOriginator();
    String objectName = oemFile.getEphemeridesBlocks().get(0).getMetaData().getObjectName();
    String objectID = oemFile.getEphemeridesBlocks().get(0).getMetaData().getObjectID();
    String interpolationMethodString = oemFile.getEphemeridesBlocks().get(0).getInterpolationMethod();
    InterpolationMethod interpolationMethod = Enum.valueOf(InterpolationMethod.class, interpolationMethodString);
    OEMWriter writer = new OEMWriter(interpolationMethod, originator, objectID, objectName);
    try {
        writer.write((BufferedWriter) null, ephemerisFile);
        fail("an exception should have been thrown");
    } catch (OrekitIllegalArgumentException oiae) {
        assertEquals(OrekitMessages.NULL_ARGUMENT, oiae.getSpecifier());
        assertEquals("writer", oiae.getParts()[0]);
    }
}

Example 4 with OrekitIllegalArgumentException

use of org.orekit.errors.OrekitIllegalArgumentException in project Orekit by CS-SI.

the class OPMParserTest method testParseOPM1.

@Test
public void testParseOPM1() throws OrekitException {
    // simple test for OPM file, contains p/v entries and other mandatory
    // data.
    final String ex = "/ccsds/OPMExample.txt";
    final OPMParser parser = new OPMParser().withMu(398600e9).withConventions(IERSConventions.IERS_2010).withSimpleEOP(true);
    final InputStream inEntry = getClass().getResourceAsStream(ex);
    final OPMFile file = parser.parse(inEntry, "OPMExample.txt");
    Assert.assertEquals(IERSConventions.IERS_2010, file.getConventions());
    // Check Header Block;
    Assert.assertEquals(2.0, file.getFormatVersion(), 1.0e-10);
    Assert.assertEquals(new AbsoluteDate(1998, 11, 06, 9, 23, 57, TimeScalesFactory.getUTC()), file.getCreationDate());
    Assert.assertEquals("JAXA", file.getOriginator());
    // Check Metadata Block;
    Assert.assertEquals("GODZILLA 5", file.getMetaData().getObjectName());
    Assert.assertEquals("1998-057A", file.getMetaData().getObjectID());
    Assert.assertEquals(1998, file.getMetaData().getLaunchYear());
    Assert.assertEquals(57, file.getMetaData().getLaunchNumber());
    Assert.assertEquals("A", file.getMetaData().getLaunchPiece());
    Assert.assertEquals("EARTH", file.getMetaData().getCenterName());
    Assert.assertTrue(file.getMetaData().getHasCreatableBody());
    Assert.assertEquals(CelestialBodyFactory.getEarth(), file.getMetaData().getCenterBody());
    Assert.assertEquals(CCSDSFrame.ITRF97.toString(), file.getMetaData().getFrame().getName());
    Assert.assertEquals(CcsdsTimeScale.TAI, file.getMetaData().getTimeSystem());
    Assert.assertFalse(file.hasCovarianceMatrix());
    // Check State Vector data Block;
    Assert.assertEquals(new AbsoluteDate(1998, 12, 18, 14, 28, 15.1172, TimeScalesFactory.getTAI()), file.getEpoch());
    checkPVEntry(new PVCoordinates(new Vector3D(6503514.000, 1239647.000, -717490.000), new Vector3D(-873.160, 8740.420, -4191.076)), file.getPVCoordinates());
    try {
        file.generateCartesianOrbit();
        Assert.fail("an exception should have been thrown");
    } catch (OrekitIllegalArgumentException oiae) {
        Assert.assertEquals(OrekitMessages.NON_PSEUDO_INERTIAL_FRAME, oiae.getSpecifier());
        Assert.assertEquals("ITRF97", oiae.getParts()[0]);
    }
    try {
        file.generateKeplerianOrbit();
        Assert.fail("an exception should have been thrown");
    } catch (OrekitIllegalArgumentException oiae) {
        Assert.assertEquals(OrekitMessages.NON_PSEUDO_INERTIAL_FRAME, oiae.getSpecifier());
        Assert.assertEquals("ITRF97", oiae.getParts()[0]);
    }
    try {
        file.generateSpacecraftState();
        Assert.fail("an exception should have been thrown");
    } catch (OrekitIllegalArgumentException oiae) {
        Assert.assertEquals(OrekitMessages.NON_PSEUDO_INERTIAL_FRAME, oiae.getSpecifier());
        Assert.assertEquals("ITRF97", oiae.getParts()[0]);
    }
}

Example 5 with OrekitIllegalArgumentException

use of org.orekit.errors.OrekitIllegalArgumentException in project Orekit by CS-SI.

the class FieldDateDetector method addEventDate.

/**
 * Add an event date.
 * <p>The date to add must be:</p>
 * <ul>
 *   <li>less than the smallest already registered event date minus the maxCheck</li>
 *   <li>or more than the largest already registered event date plus the maxCheck</li>
 * </ul>
 * @param target target date
 * @throws IllegalArgumentException if the date is too close from already defined interval
 * @see #FieldDateDetector(RealFieldElement, RealFieldElement, FieldTimeStamped...)
 */
public void addEventDate(final FieldAbsoluteDate<T> target) throws IllegalArgumentException {
    final boolean increasing;
    if (currentIndex < 0) {
        increasing = (gDate == null) ? true : target.durationFrom(gDate).getReal() > 0.0;
        currentIndex = 0;
        eventDateList.add(new FieldEventDate<>(target, increasing));
    } else {
        final int lastIndex = eventDateList.size() - 1;
        if (eventDateList.get(0).getDate().durationFrom(target).getReal() > getMaxCheckInterval().getReal()) {
            increasing = !eventDateList.get(0).isgIncrease();
            eventDateList.add(0, new FieldEventDate<>(target, increasing));
            currentIndex++;
        } else if (target.durationFrom(eventDateList.get(lastIndex).getDate()).getReal() > getMaxCheckInterval().getReal()) {
            increasing = !eventDateList.get(lastIndex).isgIncrease();
            eventDateList.add(new FieldEventDate<>(target, increasing));
        } else {
            throw new OrekitIllegalArgumentException(OrekitMessages.EVENT_DATE_TOO_CLOSE, target, eventDateList.get(0).getDate(), eventDateList.get(lastIndex).getDate(), getMaxCheckInterval());
        }
    }
}