diff --git a/src/main/java/org/orekit/rugged/errors/Dump.java b/src/main/java/org/orekit/rugged/errors/Dump.java
index aa3f098c347729730c8fe78bdc314d6708c6d8d4..041ca5c5bda13dcd571b4dc14c7c9f3fb564ecf9 100644
--- a/src/main/java/org/orekit/rugged/errors/Dump.java
+++ b/src/main/java/org/orekit/rugged/errors/Dump.java
@@ -23,6 +23,7 @@ import java.util.List;
import java.util.Locale;
import java.util.TimeZone;
+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.apache.commons.math3.util.OpenIntToDoubleHashMap;
@@ -143,7 +144,7 @@ class Dump {
throws RuggedException {
writer.format(Locale.US,
"direct location: date = %s position = %22.15e %22.15e %22.15e los = %22.15e %22.15e %22.15e ligthTime = %b aberration = %b%n",
- highAccuracyDate(date),
+ convertDate(date),
position.getX(), position.getY(), position.getZ(),
los.getX(), los.getY(), los.getZ(),
lightTimeCorrection, aberrationOfLightCorrection);
@@ -152,11 +153,12 @@ class Dump {
/** Dump an observation transform transform.
* @param scToBody provider for observation
* @param index index of the transform
- * @param transform transform
+ * @param bodyToInertial transform from body frame to inertial frame
+ * @param scToInertial transfrom from spacecraft frame to inertial frame
* @exception RuggedException if reference date cannot be converted to UTC
*/
- public void dumpTransform(final SpacecraftToObservedBody scToBody,
- final int index, final Transform transform)
+ public void dumpTransform(final SpacecraftToObservedBody scToBody, final int index,
+ final Transform bodyToInertial, final Transform scToInertial)
throws RuggedException {
if (tranformsDumped == null) {
final AbsoluteDate minDate = scToBody.getMinDate();
@@ -165,18 +167,17 @@ class Dump {
final int n = 1 + (int) FastMath.rint(maxDate.durationFrom(minDate) / tStep);
writer.format(Locale.US,
"spacecraft to observed body: min date = %s max date = %s tStep = %22.15e inertial frame = %s body frame = %s%n",
- highAccuracyDate(minDate), highAccuracyDate(maxDate), tStep,
+ convertDate(minDate), convertDate(maxDate), tStep,
scToBody.getInertialFrameName(), scToBody.getBodyFrameName());
tranformsDumped = new boolean[n];
}
if (!tranformsDumped[index]) {
writer.format(Locale.US,
- "transform: index = %d r = %22.15e %22.15e %22.15e %22.15e Ω = %22.15e %22.15e %22.15e ΩDot = %22.15e %22.15e %22.15e%n",
+ "transform: index = %d body %s spacecraft %s %s%n",
index,
- transform.getRotation().getQ0(), transform.getRotation().getQ1(),
- transform.getRotation().getQ2(), transform.getRotation().getQ3(),
- transform.getRotationRate().getX(), transform.getRotationRate().getY(), transform.getRotationRate().getZ(),
- transform.getRotationAcceleration().getX(), transform.getRotationAcceleration().getY(), transform.getRotationAcceleration().getZ());
+ convertRotation(bodyToInertial.getRotation(), bodyToInertial.getRotationRate(), bodyToInertial.getRotationAcceleration()),
+ convertTranslation(scToInertial.getTranslation(), scToInertial.getVelocity(), scToInertial.getAcceleration()),
+ convertRotation(scToInertial.getRotation(), scToInertial.getRotationRate(), scToInertial.getRotationAcceleration()));
tranformsDumped[index] = true;
}
}
@@ -206,7 +207,7 @@ class Dump {
* @return converted date
* @exception RuggedException if date cannot be converted to UTC
*/
- private String highAccuracyDate(final AbsoluteDate date)
+ private String convertDate(final AbsoluteDate date)
throws RuggedException {
try {
final DateTimeComponents dt = date.getComponents(TimeScalesFactory.getUTC());
@@ -218,6 +219,34 @@ class Dump {
}
}
+ /** Convert a translation to string.
+ * @param translation translation
+ * @param velocity linear velocity
+ * @param acceleration linear acceleration
+ * @return converted rotation
+ */
+ private String convertTranslation(final Vector3D translation, final Vector3D velocity, final Vector3D acceleration) {
+ return String.format(Locale.US,
+ "p = %22.15e %22.15e %22.15e v = %22.15e %22.15e %22.15e a = %22.15e %22.15e %22.15e",
+ translation.getX(), translation.getY(), translation.getZ(),
+ velocity.getX(), velocity.getY(), velocity.getZ(),
+ acceleration.getX(), acceleration.getY(), acceleration.getZ());
+ }
+
+ /** Convert a rotation to string.
+ * @param rotation rotation
+ * @param rate rate of the rotation
+ * @param acceleration angular acceleration
+ * @return converted rotation
+ */
+ private String convertRotation(final Rotation rotation, final Vector3D rate, final Vector3D acceleration) {
+ return String.format(Locale.US,
+ "r = %22.15e %22.15e %22.15e %22.15e Ω = %22.15e %22.15e %22.15e ΩDot = %22.15e %22.15e %22.15e",
+ rotation.getQ0(), rotation.getQ1(), rotation.getQ2(), rotation.getQ3(),
+ rate.getX(), rate.getY(), rate.getZ(),
+ acceleration.getX(), acceleration.getY(), acceleration.getZ());
+ }
+
/** Deactivate dump.
*/
public void deactivate() {
diff --git a/src/main/java/org/orekit/rugged/errors/DumpManager.java b/src/main/java/org/orekit/rugged/errors/DumpManager.java
index b0937b8b0e996ecf1cd7585582e3ac75ff4e4a96..ea9a9dda9bcde44dbb81a122678a3210c2741f77 100644
--- a/src/main/java/org/orekit/rugged/errors/DumpManager.java
+++ b/src/main/java/org/orekit/rugged/errors/DumpManager.java
@@ -149,14 +149,15 @@ public class DumpManager {
/** Dump an observation transform transform.
* @param scToBody provider for observation
* @param index index of the transform
- * @param transform transform
+ * @param bodyToInertial transform from body frame to inertial frame
+ * @param scToInertial transfrom from spacecraft frame to inertial frame
* @exception RuggedException if reference date cannot be converted to UTC
*/
- public static void dumpTransform(final SpacecraftToObservedBody scToBody,
- final int index, final Transform transform)
+ public static void dumpTransform(final SpacecraftToObservedBody scToBody, final int index,
+ final Transform bodyToInertial, final Transform scToInertial)
throws RuggedException {
if (isActive()) {
- DUMP.get().dumpTransform(scToBody, index, transform);
+ DUMP.get().dumpTransform(scToBody, index, bodyToInertial, scToInertial);
}
}
diff --git a/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java b/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
index e6006dd62a472e5ae214bb19ca826e07db87b05a..bd80455852585759c68e54a3cd741dfe4ebde7e8 100644
--- a/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
+++ b/src/main/java/org/orekit/rugged/utils/SpacecraftToObservedBody.java
@@ -272,8 +272,7 @@ public class SpacecraftToObservedBody implements Serializable {
final double s = date.durationFrom(list.get(0).getDate()) / tStep;
final int index = FastMath.max(0, FastMath.min(list.size() - 1, (int) FastMath.rint(s)));
- // we always dump the body to inertial transform, regardless of the one really asked for
- DumpManager.dumpTransform(this, index, bodyToInertial.get(index));
+ DumpManager.dumpTransform(this, index, bodyToInertial.get(index), scToInertial.get(index));
final Transform close = list.get(index);
return close.shiftedBy(date.durationFrom(close.getDate()));