diff --git a/src/tutorials/java/fr/cs/examples/DirectLocation.java b/src/tutorials/java/fr/cs/examples/DirectLocation.java
new file mode 100644
index 0000000000000000000000000000000000000000..b7bc78bdc327e2c57ae2bf4e56ce66b70aaaae0d
--- /dev/null
+++ b/src/tutorials/java/fr/cs/examples/DirectLocation.java
@@ -0,0 +1,177 @@
+/* Copyright 2013-2015 CS Systèmes d'Information
+ * Licensed to CS Systèmes d'Information (CS) under one or more
+ * contributor license agreements. See the NOTICE file distributed with
+ * this work for additional information regarding copyright ownership.
+ * CS licenses this file to You under the Apache License, Version 2.0
+ * (the "License"); you may not use this file except in compliance with
+ * the License. You may obtain a copy of the License at
+ *
+ * http://www.apache.org/licenses/LICENSE-2.0
+ *
+ * Unless required by applicable law or agreed to in writing, software
+ * distributed under the License is distributed on an "AS IS" BASIS,
+ * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
+ * See the License for the specific language governing permissions and
+ * limitations under the License.
+ */
+package fr.cs.examples;
+
+import java.io.File;
+import java.util.ArrayList;
+import java.util.List;
+import java.util.Locale;
+
+import org.apache.commons.math3.geometry.euclidean.threed.Rotation;
+import org.apache.commons.math3.geometry.euclidean.threed.Vector3D;
+import org.apache.commons.math3.util.FastMath;
+import org.orekit.bodies.GeodeticPoint;
+import org.orekit.data.DataProvidersManager;
+import org.orekit.data.DirectoryCrawler;
+import org.orekit.errors.OrekitException;
+import org.orekit.frames.Frame;
+import org.orekit.frames.FramesFactory;
+import org.orekit.frames.Transform;
+import org.orekit.rugged.api.AlgorithmId;
+import org.orekit.rugged.api.BodyRotatingFrameId;
+import org.orekit.rugged.api.EllipsoidId;
+import org.orekit.rugged.api.InertialFrameId;
+import org.orekit.rugged.api.Rugged;
+import org.orekit.rugged.api.RuggedBuilder;
+import org.orekit.rugged.errors.RuggedException;
+import org.orekit.rugged.linesensor.LineSensor;
+import org.orekit.rugged.linesensor.LinearLineDatation;
+import org.orekit.rugged.los.LOSBuilder;
+import org.orekit.rugged.los.FixedRotation;
+import org.orekit.rugged.los.TimeDependentLOS;
+import org.orekit.rugged.utils.ParameterType;
+import org.orekit.time.AbsoluteDate;
+import org.orekit.time.TimeScale;
+import org.orekit.time.TimeScalesFactory;
+import org.orekit.utils.AngularDerivativesFilter;
+import org.orekit.utils.CartesianDerivativesFilter;
+import org.orekit.utils.IERSConventions;
+import org.orekit.utils.PVCoordinates;
+import org.orekit.utils.TimeStampedAngularCoordinates;
+import org.orekit.utils.TimeStampedPVCoordinates;
+
+public class DirectLocation {
+
+ public static void main(String[] args) {
+
+ try {
+
+ // Initialize Orekit, assuming an orekit-data folder is in user home directory
+ File home = new File(System.getProperty("user.home"));
+ File orekitData = new File(home, "orekit-data");
+ DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
+
+ // The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
+ List<Vector3D> rawDirs = new ArrayList<Vector3D>();
+ for (int i = 0; i < 2000; i++) {
+ //20° field of view, 2000 pixels
+ rawDirs.add(new Vector3D(0d, i*FastMath.toRadians(20)/2000d, 1d));
+ }
+
+ // The instrument is oriented 10° off nadir around the X-axis, we need to rotate the viewing
+ // direction to obtain the line of sight in the satellite frame
+ LOSBuilder losBuilder = new LOSBuilder(rawDirs);
+ losBuilder.addTransform(new FixedRotation(ParameterType.FIXED, Vector3D.PLUS_I, FastMath.toRadians(10)));
+
+ TimeDependentLOS lineOfSight = losBuilder.build();
+
+ // We use Orekit for handling time and dates, and Rugged for defining the datation model:
+ TimeScale gps = TimeScalesFactory.getGPS();
+ AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
+ LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
+
+ // With the LOS and the datation now defined , we can initialize a line sensor object in Rugged:
+ LineSensor lineSensor = new LineSensor("mySensor", lineDatation, Vector3D.ZERO, lineOfSight);
+
+ // In our application, we simply need to know the name of the frames we are working with. Positions and
+ // velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
+ // inertial frame.
+ Frame eme2000 = FramesFactory.getEME2000();
+ boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
+ Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
+
+ ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
+ ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
+
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236d, 0.333952d, -0.844012d, -0.245684d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773d, 0.329336d, -0.837871d, -0.252281d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:30.592937", -0.369237d, 0.324612d, -0.831445d, -0.258824d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:54.592937", -0.3836d, 0.319792d, -0.824743d, -0.265299d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:18.592937", -0.397834d, 0.314883d, -0.817777d, -0.271695d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:42.592937", -0.411912d, 0.309895d, -0.810561d, -0.278001d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:06.592937", -0.42581d, 0.304838d, -0.803111d, -0.284206d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:30.592937", -0.439505d, 0.299722d, -0.795442d, -0.290301d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976d, 0.294556d, -0.787571d, -0.296279d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207d, 0.28935d, -0.779516d, -0.302131d);
+
+
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466d, -5411878.485d, 4637549.599d, -2068.995d, -4500.601d, -5576.736d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267d, -5506500.533d, 4515934.894d, -2058.308d, -4369.521d, -5683.906d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368d, -5598184.195d, 4392036.13d, -2046.169d, -4236.279d, -5788.201d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:47.392937", -885556.748d, -5686883.696d, 4265915.971d, -2032.579d, -4100.944d, -5889.568d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:08.992937", -938326.32d, -5772554.875d, 4137638.207d, -2017.537d, -3963.59d, -5987.957d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:30.592937", -990887.942d, -5855155.21d, 4007267.717d, -2001.046d, -3824.291d, -6083.317d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:52.192937", -1043205.448d, -5934643.836d, 3874870.441d, -1983.107d, -3683.122d, -6175.6d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:13.792937", -1095242.669d, -6010981.571d, 3740513.34d, -1963.723d, -3540.157d, -6264.76d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:35.392937", -1146963.457d, -6084130.93d, 3604264.372d, -1942.899d, -3395.473d, -6350.751d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706d, -6154056.146d, 3466192.446d, -1920.64d, -3249.148d, -6433.531d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381d, -6220723.191d, 3326367.397d, -1896.952d, -3101.26d, -6513.056d);
+
+ Rugged rugged = new RuggedBuilder().
+ setAlgorithm(AlgorithmId.IGNORE_DEM_USE_ELLIPSOID).
+ setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
+ setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
+ setTrajectory(InertialFrameId.EME2000,
+ satellitePVList, 4, CartesianDerivativesFilter.USE_P,
+ satelliteQList, 4, AngularDerivativesFilter.USE_R).
+ addLineSensor(lineSensor).
+ build();
+
+ Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
+ AbsoluteDate firstLineDate = lineSensor.getDate(0);
+ Vector3D los = lineSensor.getLos(firstLineDate, 0);
+ GeodeticPoint upLeftPoint = rugged.directLocation(firstLineDate, position, los);
+ System.out.format(Locale.US, "upper left point: φ = %8.3f °, λ = %8.3f °, h = %8.3f m%n",
+ FastMath.toDegrees(upLeftPoint.getLatitude()),
+ FastMath.toDegrees(upLeftPoint.getLongitude()),
+ upLeftPoint.getAltitude());
+
+ } catch (OrekitException oe) {
+ System.err.println(oe.getLocalizedMessage());
+ System.exit(1);
+ } catch (RuggedException re) {
+ System.err.println(re.getLocalizedMessage());
+ System.exit(1);
+ }
+
+ }
+
+ private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
+ ArrayList<TimeStampedPVCoordinates> satellitePVList,
+ String absDate,
+ double px, double py, double pz, double vx, double vy, double vz)
+ throws OrekitException {
+ AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
+ Vector3D position = new Vector3D(px, py, pz);
+ Vector3D velocity = new Vector3D(vx, vy, vz);
+ PVCoordinates pvITRF = new PVCoordinates(position, velocity);
+ Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
+ Vector3D pEME2000 = transform.transformPosition(pvITRF.getPosition());
+ Vector3D vEME2000 = transform.transformVector(pvITRF.getVelocity());
+ satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pEME2000, vEME2000, Vector3D.ZERO));
+ }
+
+ private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
+ double q0, double q1, double q2, double q3) {
+ AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
+ Rotation rotation = new Rotation(q0, q1, q2, q3, true);
+ TimeStampedAngularCoordinates pair =
+ new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
+ satelliteQList.add(pair);
+ }
+
+}
diff --git a/src/tutorials/java/fr/cs/examples/DirectLocationWithDEM.java b/src/tutorials/java/fr/cs/examples/DirectLocationWithDEM.java
new file mode 100644
index 0000000000000000000000000000000000000000..b25015d11a1deb6289ca82a744fc1b6d3c19acd9
--- /dev/null
+++ b/src/tutorials/java/fr/cs/examples/DirectLocationWithDEM.java
@@ -0,0 +1,226 @@
+/* Copyright 2013-2015 CS Systèmes d'Information
+ * Licensed to CS Systèmes d'Information (CS) under one or more
+ * contributor license agreements. See the NOTICE file distributed with
+ * this work for additional information regarding copyright ownership.
+ * CS licenses this file to You under the Apache License, Version 2.0
+ * (the "License"); you may not use this file except in compliance with
+ * the License. You may obtain a copy of the License at
+ *
+ * http://www.apache.org/licenses/LICENSE-2.0
+ *
+ * Unless required by applicable law or agreed to in writing, software
+ * distributed under the License is distributed on an "AS IS" BASIS,
+ * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
+ * See the License for the specific language governing permissions and
+ * limitations under the License.
+ */
+package fr.cs.examples;
+
+import java.io.File;
+import java.util.ArrayList;
+import java.util.List;
+import java.util.Locale;
+
+import org.apache.commons.math3.geometry.euclidean.threed.Rotation;
+import org.apache.commons.math3.geometry.euclidean.threed.Vector3D;
+import org.apache.commons.math3.util.FastMath;
+import org.orekit.bodies.GeodeticPoint;
+import org.orekit.data.DataProvidersManager;
+import org.orekit.data.DirectoryCrawler;
+import org.orekit.errors.OrekitException;
+import org.orekit.frames.Frame;
+import org.orekit.frames.FramesFactory;
+import org.orekit.frames.Transform;
+import org.orekit.rugged.api.AlgorithmId;
+import org.orekit.rugged.api.BodyRotatingFrameId;
+import org.orekit.rugged.api.EllipsoidId;
+import org.orekit.rugged.api.InertialFrameId;
+import org.orekit.rugged.api.Rugged;
+import org.orekit.rugged.api.RuggedBuilder;
+import org.orekit.rugged.errors.RuggedException;
+import org.orekit.rugged.linesensor.LineSensor;
+import org.orekit.rugged.linesensor.LinearLineDatation;
+import org.orekit.rugged.los.LOSBuilder;
+import org.orekit.rugged.los.FixedRotation;
+import org.orekit.rugged.los.TimeDependentLOS;
+import org.orekit.rugged.raster.TileUpdater;
+import org.orekit.rugged.raster.UpdatableTile;
+import org.orekit.rugged.utils.ParameterType;
+import org.orekit.time.AbsoluteDate;
+import org.orekit.time.TimeScale;
+import org.orekit.time.TimeScalesFactory;
+import org.orekit.utils.AngularDerivativesFilter;
+import org.orekit.utils.CartesianDerivativesFilter;
+import org.orekit.utils.Constants;
+import org.orekit.utils.IERSConventions;
+import org.orekit.utils.PVCoordinates;
+import org.orekit.utils.TimeStampedAngularCoordinates;
+import org.orekit.utils.TimeStampedPVCoordinates;
+
+public class DirectLocationWithDEM {
+
+ public static void main(String[] args) {
+
+ try {
+
+ // Initialize Orekit, assuming an orekit-data folder is in user home directory
+ File home = new File(System.getProperty("user.home"));
+ File orekitData = new File(home, "orekit-data");
+ DataProvidersManager.getInstance().addProvider(new DirectoryCrawler(orekitData));
+
+ // The raw viewing direction of pixel i with respect to the instrument is defined by the vector:
+ List<Vector3D> rawDirs = new ArrayList<Vector3D>();
+ for (int i = 0; i < 2000; i++) {
+ //20° field of view, 2000 pixels
+ rawDirs.add(new Vector3D(0d, i*FastMath.toRadians(20)/2000d, 1d));
+ }
+
+ // The instrument is oriented 10° off nadir around the X-axis, we need to rotate the viewing
+ // direction to obtain the line of sight in the satellite frame
+ LOSBuilder losBuilder = new LOSBuilder(rawDirs);
+ losBuilder.addTransform(new FixedRotation(ParameterType.FIXED, Vector3D.PLUS_I, FastMath.toRadians(10)));
+
+ TimeDependentLOS lineOfSight = losBuilder.build();
+
+ // We use Orekit for handling time and dates, and Rugged for defining the datation model:
+ TimeScale gps = TimeScalesFactory.getGPS();
+ AbsoluteDate absDate = new AbsoluteDate("2009-12-11T16:59:30.0", gps);
+ LinearLineDatation lineDatation = new LinearLineDatation(absDate, 1d, 20);
+
+ // With the LOS and the datation now defined , we can initialize a line sensor object in Rugged:
+ LineSensor lineSensor = new LineSensor("mySensor", lineDatation, Vector3D.ZERO, lineOfSight);
+
+ // In our application, we simply need to know the name of the frames we are working with. Positions and
+ // velocities are given in the ITRF terrestrial frame, while the quaternions are given in EME2000
+ // inertial frame.
+ Frame eme2000 = FramesFactory.getEME2000();
+ boolean simpleEOP = true; // we don't want to compute tiny tidal effects at millimeter level
+ Frame itrf = FramesFactory.getITRF(IERSConventions.IERS_2010, simpleEOP);
+
+ ArrayList<TimeStampedAngularCoordinates> satelliteQList = new ArrayList<TimeStampedAngularCoordinates>();
+ ArrayList<TimeStampedPVCoordinates> satellitePVList = new ArrayList<TimeStampedPVCoordinates>();
+
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:58:42.592937", -0.340236d, 0.333952d, -0.844012d, -0.245684d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:06.592937", -0.354773d, 0.329336d, -0.837871d, -0.252281d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:30.592937", -0.369237d, 0.324612d, -0.831445d, -0.258824d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T16:59:54.592937", -0.3836d, 0.319792d, -0.824743d, -0.265299d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:18.592937", -0.397834d, 0.314883d, -0.817777d, -0.271695d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:00:42.592937", -0.411912d, 0.309895d, -0.810561d, -0.278001d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:06.592937", -0.42581d, 0.304838d, -0.803111d, -0.284206d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:30.592937", -0.439505d, 0.299722d, -0.795442d, -0.290301d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:01:54.592937", -0.452976d, 0.294556d, -0.787571d, -0.296279d);
+ addSatelliteQ(gps, satelliteQList, "2009-12-11T17:02:18.592937", -0.466207d, 0.28935d, -0.779516d, -0.302131d);
+
+
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:58:42.592937", -726361.466d, -5411878.485d, 4637549.599d, -2068.995d, -4500.601d, -5576.736d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:04.192937", -779538.267d, -5506500.533d, 4515934.894d, -2058.308d, -4369.521d, -5683.906d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:25.792937", -832615.368d, -5598184.195d, 4392036.13d, -2046.169d, -4236.279d, -5788.201d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T16:59:47.392937", -885556.748d, -5686883.696d, 4265915.971d, -2032.579d, -4100.944d, -5889.568d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:08.992937", -938326.32d, -5772554.875d, 4137638.207d, -2017.537d, -3963.59d, -5987.957d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:30.592937", -990887.942d, -5855155.21d, 4007267.717d, -2001.046d, -3824.291d, -6083.317d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:00:52.192937", -1043205.448d, -5934643.836d, 3874870.441d, -1983.107d, -3683.122d, -6175.6d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:13.792937", -1095242.669d, -6010981.571d, 3740513.34d, -1963.723d, -3540.157d, -6264.76d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:35.392937", -1146963.457d, -6084130.93d, 3604264.372d, -1942.899d, -3395.473d, -6350.751d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:01:56.992937", -1198331.706d, -6154056.146d, 3466192.446d, -1920.64d, -3249.148d, -6433.531d);
+ addSatellitePV(gps, eme2000, itrf, satellitePVList, "2009-12-11T17:02:18.592937", -1249311.381d, -6220723.191d, 3326367.397d, -1896.952d, -3101.26d, -6513.056d);
+
+ Rugged rugged = new RuggedBuilder().
+ setAlgorithm(AlgorithmId.DUVENHAGE).
+ setDigitalElevationModel(new VolcanicConeElevationUpdater(new GeodeticPoint(FastMath.toRadians(37.58),
+ FastMath.toRadians(-96.95),
+ 2463.0),
+ FastMath.toRadians(30.0), 16.0,
+ FastMath.toRadians(1.0), 1201),
+
+ 8).
+ setEllipsoid(EllipsoidId.WGS84, BodyRotatingFrameId.ITRF).
+ setTimeSpan(absDate, absDate.shiftedBy(60.0), 0.01, 5 / lineSensor.getRate(0)).
+ setTrajectory(InertialFrameId.EME2000,
+ satellitePVList, 4, CartesianDerivativesFilter.USE_P,
+ satelliteQList, 4, AngularDerivativesFilter.USE_R).
+ addLineSensor(lineSensor).
+ build();
+
+ Vector3D position = lineSensor.getPosition(); // This returns a zero vector since we set the relative position of the sensor w.r.T the satellite to 0.
+ AbsoluteDate firstLineDate = lineSensor.getDate(0);
+ Vector3D los = lineSensor.getLos(firstLineDate, 0);
+ GeodeticPoint upLeftPoint = rugged.directLocation(firstLineDate, position, los);
+ System.out.format(Locale.US, "upper left point: φ = %8.3f °, λ = %8.3f °, h = %8.3f m%n",
+ FastMath.toDegrees(upLeftPoint.getLatitude()),
+ FastMath.toDegrees(upLeftPoint.getLongitude()),
+ upLeftPoint.getAltitude());
+
+ } catch (OrekitException oe) {
+ System.err.println(oe.getLocalizedMessage());
+ System.exit(1);
+ } catch (RuggedException re) {
+ System.err.println(re.getLocalizedMessage());
+ System.exit(1);
+ }
+
+ }
+
+ private static void addSatellitePV(TimeScale gps, Frame eme2000, Frame itrf,
+ ArrayList<TimeStampedPVCoordinates> satellitePVList,
+ String absDate,
+ double px, double py, double pz, double vx, double vy, double vz)
+ throws OrekitException {
+ AbsoluteDate ephemerisDate = new AbsoluteDate(absDate, gps);
+ Vector3D position = new Vector3D(px, py, pz);
+ Vector3D velocity = new Vector3D(vx, vy, vz);
+ PVCoordinates pvITRF = new PVCoordinates(position, velocity);
+ Transform transform = itrf.getTransformTo(eme2000, ephemerisDate);
+ Vector3D pEME2000 = transform.transformPosition(pvITRF.getPosition());
+ Vector3D vEME2000 = transform.transformVector(pvITRF.getVelocity());
+ satellitePVList.add(new TimeStampedPVCoordinates(ephemerisDate, pEME2000, vEME2000, Vector3D.ZERO));
+ }
+
+ private static void addSatelliteQ(TimeScale gps, ArrayList<TimeStampedAngularCoordinates> satelliteQList, String absDate,
+ double q0, double q1, double q2, double q3) {
+ AbsoluteDate attitudeDate = new AbsoluteDate(absDate, gps);
+ Rotation rotation = new Rotation(q0, q1, q2, q3, true);
+ TimeStampedAngularCoordinates pair =
+ new TimeStampedAngularCoordinates(attitudeDate, rotation, Vector3D.ZERO, Vector3D.ZERO);
+ satelliteQList.add(pair);
+ }
+
+ private static class VolcanicConeElevationUpdater implements TileUpdater {
+
+ private GeodeticPoint summit;
+ private double slope;
+ private double base;
+ private double size;
+ private int n;
+
+ public VolcanicConeElevationUpdater(GeodeticPoint summit, double slope, double base,
+ double size, int n) {
+ this.summit = summit;
+ this.slope = slope;
+ this.base = base;
+ this.size = size;
+ this.n = n;
+ }
+
+ public void updateTile(double latitude, double longitude, UpdatableTile tile)
+ throws RuggedException {
+ double step = size / (n - 1);
+ double minLatitude = size * FastMath.floor(latitude / size);
+ double minLongitude = size * FastMath.floor(longitude / size);
+ double sinSlope = FastMath.sin(slope);
+ tile.setGeometry(minLatitude, minLongitude, step, step, n, n);
+ for (int i = 0; i < n; ++i) {
+ double cellLatitude = minLatitude + i * step;
+ for (int j = 0; j < n; ++j) {
+ double cellLongitude = minLongitude + j * step;
+ double distance = Constants.WGS84_EARTH_EQUATORIAL_RADIUS *
+ FastMath.hypot(cellLatitude - summit.getLatitude(),
+ cellLongitude - summit.getLongitude());
+ double altitude = FastMath.max(summit.getAltitude() - distance * sinSlope,
+ base);
+ tile.setElevation(i, j, altitude);
+ }
+ }
+ }
+
+ }
+}