diff --git a/pom.xml b/pom.xml
index 43a00d58763177a359d7132a02f1267131848ffe..6f9517726f27314621c183eae45d36f2d7e85b81 100644
--- a/pom.xml
+++ b/pom.xml
@@ -4,7 +4,7 @@
<modelVersion>4.0.0</modelVersion>
<groupId>org.orekit</groupId>
<artifactId>rugged</artifactId>
- <version>2.3-SNAPSHOT</version>
+ <version>3.0-SNAPSHOT</version>
<packaging>jar</packaging>
<name>Rugged</name>
<url>https://www.orekit.org/rugged</url>
@@ -19,7 +19,7 @@
<!-- COTS version -->
- <rugged.orekit.version>10.2</rugged.orekit.version>
+ <rugged.orekit.version>11.0.1</rugged.orekit.version>
<rugged.junit.version>4.13.2</rugged.junit.version>
<!-- Compilers and Tools version -->
diff --git a/src/changes/changes.xml b/src/changes/changes.xml
index 8510a3b315e5730d9c19926fdc7662c50f4d6b38..fbc9ab788a6f931f00f3d17f5dc6395280b05883 100644
--- a/src/changes/changes.xml
+++ b/src/changes/changes.xml
@@ -20,7 +20,10 @@
<title>Rugged Changes</title>
</properties>
<body>
- <release version="2.3" date="TBD" description="TBD">
+ <release version="3.0" date="TBD" description="TBD">
+ <action dev="luc" type="update" issue="387">
+ Updated dependencies to Orekit 11.0.1 (and Hipparchus 2.0).
+ </action>
</release>
<release version="2.2" date="2020-07-31" description="This is a minor release.
It adds access to algorithm identifier,
diff --git a/src/main/java/org/orekit/rugged/api/RuggedBuilder.java b/src/main/java/org/orekit/rugged/api/RuggedBuilder.java
index b1ffd05dc0a186e715f96dd846da65abc90c0728..7c4f9c7dfab5966954e62188080c070262b6eafb 100644
--- a/src/main/java/org/orekit/rugged/api/RuggedBuilder.java
+++ b/src/main/java/org/orekit/rugged/api/RuggedBuilder.java
@@ -32,8 +32,6 @@ import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.propagation.Propagator;
-import org.orekit.propagation.SpacecraftState;
-import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.errors.RuggedInternalError;
import org.orekit.rugged.errors.RuggedMessages;
@@ -733,19 +731,14 @@ public class RuggedBuilder {
new ArrayList<TimeStampedPVCoordinates>();
final List<TimeStampedAngularCoordinates> quaternions =
new ArrayList<TimeStampedAngularCoordinates>();
- propagator.setMasterMode(interpolationStep, new OrekitFixedStepHandler() {
-
- /** {@inheritDoc} */
- @Override
- public void handleStep(final SpacecraftState currentState, final boolean isLast) {
- final AbsoluteDate date = currentState.getDate();
- final PVCoordinates pv = currentState.getPVCoordinates(inertialFrame);
- final Rotation q = currentState.getAttitude().getRotation();
- positionsVelocities.add(new TimeStampedPVCoordinates(date, pv.getPosition(), pv.getVelocity(), Vector3D.ZERO));
- quaternions.add(new TimeStampedAngularCoordinates(date, q, Vector3D.ZERO, Vector3D.ZERO));
- }
-
- });
+ propagator.getMultiplexer().add(interpolationStep,
+ currentState -> {
+ final AbsoluteDate date = currentState.getDate();
+ final PVCoordinates pv = currentState.getPVCoordinates(inertialFrame);
+ final Rotation q = currentState.getAttitude().getRotation();
+ positionsVelocities.add(new TimeStampedPVCoordinates(date, pv.getPosition(), pv.getVelocity(), Vector3D.ZERO));
+ quaternions.add(new TimeStampedAngularCoordinates(date, q, Vector3D.ZERO, Vector3D.ZERO));
+ });
propagator.propagate(minDate.shiftedBy(-interpolationStep), maxDate.shiftedBy(interpolationStep));
// orbit/attitude to body converter
diff --git a/src/site/markdown/index.md b/src/site/markdown/index.md
index da4f937de519388509304be8c0573628a82769ae..01ee8f9b7ab8c535aeb9528b93b2017f8f727e07 100644
--- a/src/site/markdown/index.md
+++ b/src/site/markdown/index.md
@@ -98,7 +98,7 @@ interoperability in space systems.
## Maintained library
-Rugged has been in development since 2014 inside [CS GROUP](http://www.c-s.fr/ "CS GROUP homepage")
+Rugged has been in development since 2014 inside [CS GROUP](https://www.csgroup.eu/ "CS GROUP homepage")
and is still used and maintained by its dual teams
of space dynamics and image processing experts.
diff --git a/src/test/java/org/orekit/rugged/TestUtils.java b/src/test/java/org/orekit/rugged/TestUtils.java
index 418a9a1b3b9288e447ebadca51284889d6c1f9ce..baaea0d93dcd5ac572c0f8882e66076af14ebcbe 100644
--- a/src/test/java/org/orekit/rugged/TestUtils.java
+++ b/src/test/java/org/orekit/rugged/TestUtils.java
@@ -58,7 +58,6 @@ import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.KeplerianPropagator;
import org.orekit.propagation.numerical.NumericalPropagator;
-import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials;
import org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators;
import org.orekit.rugged.linesensor.SensorPixel;
@@ -302,14 +301,10 @@ public class TestUtils {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedPVCoordinates(currentState.getDate(),
- currentState.getPVCoordinates().getPosition(),
- currentState.getPVCoordinates().getVelocity(),
- Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedPVCoordinates(currentState.getDate(),
+ currentState.getPVCoordinates().getPosition(),
+ currentState.getPVCoordinates().getVelocity(),
+ Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
@@ -325,13 +320,9 @@ public class TestUtils {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<TimeStampedAngularCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
- currentState.getAttitude().getRotation(),
- Vector3D.ZERO, Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
+ currentState.getAttitude().getRotation(),
+ Vector3D.ZERO, Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
diff --git a/src/test/java/org/orekit/rugged/adjustment/util/PleiadesOrbitModel.java b/src/test/java/org/orekit/rugged/adjustment/util/PleiadesOrbitModel.java
index 5f76ebb808a0f108adb6a8eea66650655959c8e3..cca8dbc4d0a7e557a8f0ca387aeeab0826b79243 100644
--- a/src/test/java/org/orekit/rugged/adjustment/util/PleiadesOrbitModel.java
+++ b/src/test/java/org/orekit/rugged/adjustment/util/PleiadesOrbitModel.java
@@ -166,12 +166,11 @@ public class PleiadesOrbitModel {
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(step,
- (currentState, isLast) ->
- list.add(new TimeStampedPVCoordinates(currentState.getDate(),
- currentState.getPVCoordinates().getPosition(),
- currentState.getPVCoordinates().getVelocity(),
- Vector3D.ZERO)));
+ propagator.getMultiplexer().add(step,
+ currentState -> list.add(new TimeStampedPVCoordinates(currentState.getDate(),
+ currentState.getPVCoordinates().getPosition(),
+ currentState.getPVCoordinates().getVelocity(),
+ Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
@@ -187,12 +186,11 @@ public class PleiadesOrbitModel {
propagator.setAttitudeProvider(createAttitudeProvider(earth, orbit));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<>();
- propagator.setMasterMode(step,
- (currentState, isLast) ->
- list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
- currentState.getAttitude().getRotation(),
- Vector3D.ZERO,
- Vector3D.ZERO)));
+ propagator.getMultiplexer().add(step,
+ currentState -> list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
+ currentState.getAttitude().getRotation(),
+ Vector3D.ZERO,
+ Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
diff --git a/src/test/java/org/orekit/rugged/api/RuggedBuilderTest.java b/src/test/java/org/orekit/rugged/api/RuggedBuilderTest.java
index f24730bda5eee803bbd53af9ca1afa73f77473f8..825e85ae17108c2672ea285f8151452f1e17a8a7 100644
--- a/src/test/java/org/orekit/rugged/api/RuggedBuilderTest.java
+++ b/src/test/java/org/orekit/rugged/api/RuggedBuilderTest.java
@@ -63,7 +63,6 @@ import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.KeplerianPropagator;
import org.orekit.propagation.numerical.NumericalPropagator;
-import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.rugged.errors.RuggedException;
import org.orekit.rugged.errors.RuggedMessages;
import org.orekit.rugged.linesensor.LineDatation;
@@ -825,14 +824,10 @@ public class RuggedBuilderTest {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedPVCoordinates(currentState.getDate(),
- currentState.getPVCoordinates().getPosition(),
- currentState.getPVCoordinates().getVelocity(),
- Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedPVCoordinates(currentState.getDate(),
+ currentState.getPVCoordinates().getPosition(),
+ currentState.getPVCoordinates().getVelocity(),
+ Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
@@ -845,13 +840,9 @@ public class RuggedBuilderTest {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<TimeStampedAngularCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
- currentState.getAttitude().getRotation(),
- Vector3D.ZERO, Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
+ currentState.getAttitude().getRotation(),
+ Vector3D.ZERO, Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
diff --git a/src/test/java/org/orekit/rugged/api/RuggedTest.java b/src/test/java/org/orekit/rugged/api/RuggedTest.java
index cd8aae3f4f3f95bc64e7b56894fc2eb6032b2c78..29ea82e5da514c9ab0bb7c3a861ca7e0e61d8791 100644
--- a/src/test/java/org/orekit/rugged/api/RuggedTest.java
+++ b/src/test/java/org/orekit/rugged/api/RuggedTest.java
@@ -59,6 +59,7 @@ import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.orbits.Orbit;
+import org.orekit.propagation.EphemerisGenerator;
import org.orekit.propagation.Propagator;
import org.orekit.rugged.TestUtils;
import org.orekit.rugged.adjustment.GroundOptimizationProblemBuilder;
@@ -136,9 +137,9 @@ public class RuggedTest {
Propagator propagator = TestUtils.createPropagator(earth, gravityField, orbit);
propagator.propagate(lineDatation.getDate(firstLine).shiftedBy(-1.0));
- propagator.setEphemerisMode();
+ final EphemerisGenerator generator = propagator.getEphemerisGenerator();
propagator.propagate(lineDatation.getDate(lastLine).shiftedBy(+1.0));
- Propagator ephemeris = propagator.getGeneratedEphemeris();
+ Propagator ephemeris = generator.getGeneratedEphemeris();
Rugged rugged = new RuggedBuilder().
setDigitalElevationModel(updater, 8).
diff --git a/src/test/java/org/orekit/rugged/linesensor/SensorMeanPlaneCrossingTest.java b/src/test/java/org/orekit/rugged/linesensor/SensorMeanPlaneCrossingTest.java
index 9107078602bfd311812dc4fd407ff33d9d07f6c9..3b051ac62423b75f0738c812ba32bbe9451ac403 100644
--- a/src/test/java/org/orekit/rugged/linesensor/SensorMeanPlaneCrossingTest.java
+++ b/src/test/java/org/orekit/rugged/linesensor/SensorMeanPlaneCrossingTest.java
@@ -44,9 +44,7 @@ import org.orekit.orbits.CircularOrbit;
import org.orekit.orbits.Orbit;
import org.orekit.orbits.PositionAngle;
import org.orekit.propagation.Propagator;
-import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.KeplerianPropagator;
-import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.rugged.TestUtils;
import org.orekit.rugged.linesensor.SensorMeanPlaneCrossing.CrossingResult;
import org.orekit.rugged.los.LOSBuilder;
@@ -316,14 +314,10 @@ public class SensorMeanPlaneCrossingTest {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedPVCoordinates> list = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedPVCoordinates(currentState.getDate(),
- currentState.getPVCoordinates().getPosition(),
- currentState.getPVCoordinates().getVelocity(),
- Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedPVCoordinates(currentState.getDate(),
+ currentState.getPVCoordinates().getPosition(),
+ currentState.getPVCoordinates().getVelocity(),
+ Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
@@ -336,13 +330,9 @@ public class SensorMeanPlaneCrossingTest {
propagator.setAttitudeProvider(new YawCompensation(orbit.getFrame(), new NadirPointing(orbit.getFrame(), earth)));
propagator.propagate(minDate);
final List<TimeStampedAngularCoordinates> list = new ArrayList<TimeStampedAngularCoordinates>();
- propagator.setMasterMode(step, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
- currentState.getAttitude().getRotation(),
- Vector3D.ZERO, Vector3D.ZERO));
- }
- });
+ propagator.getMultiplexer().add(step, currentState -> list.add(new TimeStampedAngularCoordinates(currentState.getDate(),
+ currentState.getAttitude().getRotation(),
+ Vector3D.ZERO, Vector3D.ZERO)));
propagator.propagate(maxDate);
return list;
}
diff --git a/src/test/java/org/orekit/rugged/utils/RoughVisibilityEstimatorTest.java b/src/test/java/org/orekit/rugged/utils/RoughVisibilityEstimatorTest.java
index e26b8eaf21381954906f9a64544905e0116e9b14..ccca03bc6e44494026ad98ffb1b425378c00e5f0 100644
--- a/src/test/java/org/orekit/rugged/utils/RoughVisibilityEstimatorTest.java
+++ b/src/test/java/org/orekit/rugged/utils/RoughVisibilityEstimatorTest.java
@@ -50,7 +50,6 @@ import org.orekit.orbits.PositionAngle;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.numerical.NumericalPropagator;
-import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScalesFactory;
import org.orekit.utils.Constants;
@@ -69,18 +68,17 @@ public class RoughVisibilityEstimatorTest {
Orbit orbit = createOrbit(gravityField.getMu());
Propagator propagator = createPropagator(earth, gravityField, orbit);
final List<TimeStampedPVCoordinates> pv = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(1.0, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- pv.add(currentState.getPVCoordinates());
- }
- });
+ propagator.getMultiplexer().add(1.0, currentState -> pv.add(currentState.getPVCoordinates()));
propagator.propagate(orbit.getDate().shiftedBy(3 * orbit.getKeplerianPeriod()));
RoughVisibilityEstimator estimator = new RoughVisibilityEstimator(ellipsoid, orbit.getFrame(), pv);
AbsoluteDate d = estimator.estimateVisibility(new GeodeticPoint(FastMath.toRadians(-81.5),
FastMath.toRadians(-2.0),
0.0));
- Assert.assertEquals("2012-01-01T03:47:08.814", d.toString(TimeScalesFactory.getUTC()));
+ Assert.assertEquals(0.0,
+ new AbsoluteDate("2012-01-01T03:47:08.814121623",
+ TimeScalesFactory.getUTC()).durationFrom(d),
+ 1.0e-9);
}
@@ -94,18 +92,17 @@ public class RoughVisibilityEstimatorTest {
Orbit orbit = createOrbit(gravityField.getMu());
Propagator propagator = createPropagator(earth, gravityField, orbit);
final List<TimeStampedPVCoordinates> pv = new ArrayList<TimeStampedPVCoordinates>();
- propagator.setMasterMode(1.0, new OrekitFixedStepHandler() {
- public void handleStep(SpacecraftState currentState, boolean isLast) {
- pv.add(currentState.getPVCoordinates());
- }
- });
+ propagator.getMultiplexer().add(1.0, currentState -> pv.add(currentState.getPVCoordinates()));
propagator.propagate(orbit.getDate().shiftedBy(orbit.getKeplerianPeriod()));
RoughVisibilityEstimator estimator = new RoughVisibilityEstimator(ellipsoid, orbit.getFrame(), pv);
AbsoluteDate d = estimator.estimateVisibility(new GeodeticPoint(FastMath.toRadians(43.303),
FastMath.toRadians(-46.126),
0.0));
- Assert.assertEquals("2012-01-01T01:02:39.123", d.toString(TimeScalesFactory.getUTC()));
+ Assert.assertEquals(0.0,
+ new AbsoluteDate("2012-01-01T01:02:39.122526662",
+ TimeScalesFactory.getUTC()).durationFrom(d),
+ 1.0e-9);
}