diff --git a/pom.xml b/pom.xml
index b14e947d7ad6ec1dcac6edb25274e5c3ecb82347..d2fd4ae8341668878529a723be7a884bf3a9ab3b 100644
--- a/pom.xml
+++ b/pom.xml
@@ -416,6 +416,15 @@
<groupId>org.apache.maven.plugins</groupId>
<artifactId>maven-javadoc-plugin</artifactId>
<version>${orekit.maven-javadoc-plugin.version}</version>
+ <configuration>
+ <overview>${basedir}/src/main/java/org/orekit/overview.html</overview>
+ <bottom><![CDATA[Copyright © ${project.inceptionYear}-{currentYear} <a href="http://www.c-s.fr">CS Systèmes d'information</a>. All rights reserved.]]></bottom>
+ <links>
+ <link>http://docs.oracle.com/javase/8/docs/api/</link>
+ <link>https://www.hipparchus.org/apidocs/</link>
+ </links>
+ <source>${orekit.compiler.source}</source>
+ </configuration>
</plugin>
<plugin>
<groupId>org.jacoco</groupId>
@@ -648,6 +657,7 @@
<link>http://docs.oracle.com/javase/8/docs/api/</link>
<link>https://www.hipparchus.org/apidocs/</link>
</links>
+ <source>${orekit.compiler.source}</source>
</configuration>
<reportSets>
<reportSet>
diff --git a/src/main/java/org/orekit/bodies/OneAxisEllipsoid.java b/src/main/java/org/orekit/bodies/OneAxisEllipsoid.java
index 85487a892927b39c9e87c68896a47a38b9ffa785..e1bfefe180cc07e82bab226c63ba8cd9469ee172 100644
--- a/src/main/java/org/orekit/bodies/OneAxisEllipsoid.java
+++ b/src/main/java/org/orekit/bodies/OneAxisEllipsoid.java
@@ -79,7 +79,7 @@ public class OneAxisEllipsoid extends Ellipsoid implements BodyShape {
/** Simple constructor.
* <p>Standard values for Earth models can be found in the {@link org.orekit.utils.Constants Constants} class:</p>
- * <table border="1" cellpadding="5" style="background-color:#f5f5dc;">
+ * <table border="1" cellpadding="5" style="background-color:#f5f5dc;" summary="">
* <caption>Ellipsoid Models</caption>
* <tr style="background-color:#c9d5c9;"><th>model</th><th>a<sub>e</sub> (m)</th> <th>f</th></tr>
* <tr><td style="background-color:#c9d5c9;">GRS 80</td>
@@ -88,7 +88,7 @@ public class OneAxisEllipsoid extends Ellipsoid implements BodyShape {
* <tr><td style="background-color:#c9d5c9;">WGS84</td>
* <td>{@link org.orekit.utils.Constants#WGS84_EARTH_EQUATORIAL_RADIUS Constants.WGS84_EARTH_EQUATORIAL_RADIUS}</td>
* <td>{@link org.orekit.utils.Constants#WGS84_EARTH_FLATTENING Constants.WGS84_EARTH_FLATTENING}</td></tr>
- * </table summary="">
+ * </table>
* @param ae equatorial radius
* @param f the flattening (f = (a-b)/a)
* @param bodyFrame body frame related to body shape
@@ -215,7 +215,21 @@ public class OneAxisEllipsoid extends Ellipsoid implements BodyShape {
}
- /** {@inheritDoc} */
+ /** Get the intersection point of a line with the surface of the body.
+ * <p>A line may have several intersection points with a closed
+ * surface (we consider the one point case as a degenerated two
+ * points case). The close parameter is used to select which of
+ * these points should be returned. The selected point is the one
+ * that is closest to the close point.</p>
+ * @param line test line (may intersect the body or not)
+ * @param close point used for intersections selection
+ * @param frame frame in which line is expressed
+ * @param date date of the line in given frame
+ * @param <T> type of the field elements
+ * @return intersection point at altitude zero or null if the line does
+ * not intersect the surface
+ * @since 9.3
+ */
public <T extends RealFieldElement<T>> FieldVector3D<T> getCartesianIntersectionPoint(final FieldLine<T> line,
final FieldVector3D<T> close,
final Frame frame,
diff --git a/src/main/java/org/orekit/estimation/measurements/AngularAzEl.java b/src/main/java/org/orekit/estimation/measurements/AngularAzEl.java
index 119742699ac9adb14243c6b7aad9aeb20ad17961..320db24dcbd7d4f929dd4b17301db91f11b21ffc 100644
--- a/src/main/java/org/orekit/estimation/measurements/AngularAzEl.java
+++ b/src/main/java/org/orekit/estimation/measurements/AngularAzEl.java
@@ -57,7 +57,7 @@ public class AngularAzEl extends AbstractMeasurement<AngularAzEl> {
* @param angular observed value
* @param sigma theoretical standard deviation
* @param baseWeight base weight
- * @deprecated since 9.3, replaced by {@#AngularAzEl(GroundStation, AbsoluteDate,
+ * @deprecated since 9.3, replaced by {@link #AngularAzEl(GroundStation, AbsoluteDate,
* double[], double[], double[], ObservableSatellite)}
*/
@Deprecated
@@ -74,7 +74,7 @@ public class AngularAzEl extends AbstractMeasurement<AngularAzEl> {
* @param baseWeight base weight
* @param propagatorIndex index of the propagator related to this measurement
* @since 9.0
- * @deprecated since 9.3, replaced by {@#AngularAzEl(GroundStation, AbsoluteDate,
+ * @deprecated since 9.3, replaced by {@link #AngularAzEl(GroundStation, AbsoluteDate,
* double[], double[], double[], ObservableSatellite)}
*/
@Deprecated
diff --git a/src/main/java/org/orekit/estimation/measurements/AngularRaDec.java b/src/main/java/org/orekit/estimation/measurements/AngularRaDec.java
index fd5860b191f48f4f0910cf3cf8f28a2e4dfa4bcf..5c07faac59134d63ebffbc6824d333d27f517abc 100644
--- a/src/main/java/org/orekit/estimation/measurements/AngularRaDec.java
+++ b/src/main/java/org/orekit/estimation/measurements/AngularRaDec.java
@@ -64,7 +64,7 @@ public class AngularRaDec extends AbstractMeasurement<AngularRaDec> {
* @param angular observed value
* @param sigma theoretical standard deviation
* @param baseWeight base weight
- * @deprecated since 9.3, replaced by {@#AngularRaDec(GroundStation, AbsoluteDate,
+ * @deprecated since 9.3, replaced by {@link #AngularRaDec(GroundStation, Frame, AbsoluteDate,
* double[], double[], double[], ObservableSatellite)}
*/
@Deprecated
@@ -82,7 +82,7 @@ public class AngularRaDec extends AbstractMeasurement<AngularRaDec> {
* @param baseWeight base weight
* @param propagatorIndex index of the propagator related to this measurement
* @since 9.0
- * @deprecated since 9.3, replaced by {@#AngularRaDec(GroundStation, AbsoluteDate,
+ * @deprecated since 9.3, replaced by {@link #AngularRaDec(GroundStation, Frame, AbsoluteDate,
* double[], double[], double[], ObservableSatellite)}
*/
@Deprecated
diff --git a/src/main/java/org/orekit/estimation/measurements/ComparableMeasurement.java b/src/main/java/org/orekit/estimation/measurements/ComparableMeasurement.java
index 533ef3c1788e75c77a662bd4a28a877962869116..5539e04fe80aefccca7d4896528bf18cc5f89850 100644
--- a/src/main/java/org/orekit/estimation/measurements/ComparableMeasurement.java
+++ b/src/main/java/org/orekit/estimation/measurements/ComparableMeasurement.java
@@ -29,7 +29,7 @@ public interface ComparableMeasurement extends TimeStamped, Comparable<Comparabl
* <p>
* The observed value is the value that was measured by the instrument.
* </p>
- * @return observed value (array of size {@link #getDimension()}
+ * @return observed value
*/
double[] getObservedValue();
diff --git a/src/main/java/org/orekit/estimation/measurements/PV.java b/src/main/java/org/orekit/estimation/measurements/PV.java
index cb0215514d7400dfe148d6f8e34ef63ca36d3ce8..3b18663416d7ff7e3ef6c5a47c4bfff4ca16f401 100644
--- a/src/main/java/org/orekit/estimation/measurements/PV.java
+++ b/src/main/java/org/orekit/estimation/measurements/PV.java
@@ -345,7 +345,7 @@ public class PV extends AbstractMeasurement<PV> {
* @param baseWeight base weight
* @since 9.2
* @deprecated as of 9.3, replaced by {@link #PV(AbsoluteDate, Vector3D, Vector3D,
- * double[][], double, ObservableSatellite))}
+ * double[][], double, ObservableSatellite)}
*/
@Deprecated
public PV(final AbsoluteDate date, final Vector3D position, final Vector3D velocity,
@@ -364,7 +364,7 @@ public class PV extends AbstractMeasurement<PV> {
* @param propagatorIndex index of the propagator related to this measurement
* @since 9.2
* @deprecated as of 9.3, replaced by {@link #PV(AbsoluteDate, Vector3D, Vector3D,
- * double[][], double, ObservableSatellite))}
+ * double[][], double, ObservableSatellite)}
*/
@Deprecated
public PV(final AbsoluteDate date, final Vector3D position, final Vector3D velocity,
diff --git a/src/main/java/org/orekit/estimation/measurements/generation/Generator.java b/src/main/java/org/orekit/estimation/measurements/generation/Generator.java
index 3071dcadf3b3a86e3b7d3cff396e6f2c7ce11fc6..a927009f13bca99cc2c39f8e067d1651ee1f5442 100644
--- a/src/main/java/org/orekit/estimation/measurements/generation/Generator.java
+++ b/src/main/java/org/orekit/estimation/measurements/generation/Generator.java
@@ -31,7 +31,7 @@ import org.orekit.propagation.sampling.OrekitStepInterpolator;
import org.orekit.time.AbsoluteDate;
-/** Main generator for {@link ObservedMeasurements observed measurements}.
+/** Main generator for {@link ObservedMeasurement observed measurements}.
* @author Luc Maisonobe
* @since 9.3
*/
diff --git a/src/main/java/org/orekit/estimation/measurements/generation/MeasurementBuilder.java b/src/main/java/org/orekit/estimation/measurements/generation/MeasurementBuilder.java
index c4c619f884ebca5fac5b479e36cc228302c4b02a..2713ae2bef27fac457b5678ee21ac0c046cffdec 100644
--- a/src/main/java/org/orekit/estimation/measurements/generation/MeasurementBuilder.java
+++ b/src/main/java/org/orekit/estimation/measurements/generation/MeasurementBuilder.java
@@ -24,7 +24,7 @@ import org.orekit.propagation.SpacecraftState;
import org.orekit.time.AbsoluteDate;
-/** Interface for generating individual {@link ObservedMeasurements measurements}.
+/** Interface for generating individual {@link ObservedMeasurement measurements}.
* @param <T> the type of the measurement
* @author Luc Maisonobe
* @since 9.3
diff --git a/src/main/java/org/orekit/estimation/measurements/generation/Scheduler.java b/src/main/java/org/orekit/estimation/measurements/generation/Scheduler.java
index a81f1dd3742a8f75ba39f934536f5991a89ac0eb..280760af7197436a9c27835fb39a929d4bb707d4 100644
--- a/src/main/java/org/orekit/estimation/measurements/generation/Scheduler.java
+++ b/src/main/java/org/orekit/estimation/measurements/generation/Scheduler.java
@@ -24,7 +24,7 @@ import org.orekit.propagation.sampling.OrekitStepInterpolator;
import org.orekit.time.AbsoluteDate;
-/** Interface for generating {@link ObservedMeasurements measurements} sequences.
+/** Interface for generating {@link ObservedMeasurement measurements} sequences.
* @param <T> the type of the measurement
* @author Luc Maisonobe
* @since 9.3
diff --git a/src/main/java/org/orekit/estimation/sequential/KalmanEstimatorBuilder.java b/src/main/java/org/orekit/estimation/sequential/KalmanEstimatorBuilder.java
index fef334b8212b6a76c5db6b3cf4ed9a805096c1fa..ac449bf9e16f86b31ea547b94cdcac856658b92c 100644
--- a/src/main/java/org/orekit/estimation/sequential/KalmanEstimatorBuilder.java
+++ b/src/main/java/org/orekit/estimation/sequential/KalmanEstimatorBuilder.java
@@ -21,7 +21,6 @@ import java.util.List;
import org.hipparchus.linear.MatrixDecomposer;
import org.hipparchus.linear.QRDecomposer;
-import org.hipparchus.linear.RealMatrix;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitMessages;
import org.orekit.propagation.conversion.NumericalPropagatorBuilder;
@@ -56,15 +55,13 @@ public class KalmanEstimatorBuilder {
this.processNoiseMatricesProviders = new ArrayList<>();
}
- /** Construct a {@link KalmanEstimatorReal} from the data in this builder.
+ /** Construct a {@link KalmanEstimator} from the data in this builder.
* <p>
* Before this method is called, {@link #addPropagationConfiguration(NumericalPropagatorBuilder,
- * ProcessNoiseMatrixProvider)addPropagationConfiguration()} must have been called
- * at least once and {@link #initialCovarianceMatrix(RealMatrix) initialCovarianceMatrix()}
- * must have been called, otherwise configuration is incomplete and an exception
- * will be raised.
+ * CovarianceMatrixProvider) addPropagationConfiguration()} must have been called
+ * at least once, otherwise configuration is incomplete and an exception will be raised.
* </p>
- * @return a new {@link KalmanEstimatorReal}.
+ * @return a new {@link KalmanEstimator}.
*/
public KalmanEstimator build() {
final int n = propagatorBuilders.size();
@@ -92,7 +89,7 @@ public class KalmanEstimatorBuilder {
* </p>
* <p>
* The {@code provider} should return a matrix with dimensions and ordering
- * consistent with the {@link builder} configuration. The first 6 rows/columns
+ * consistent with the {@code builder} configuration. The first 6 rows/columns
* correspond to the 6 orbital parameters which must all be present, regardless
* of the fact they are estimated or not. The remaining elements correspond
* to the subset of propagation parameters that are estimated, in the
diff --git a/src/main/java/org/orekit/estimation/sequential/UnivariateProcessNoise.java b/src/main/java/org/orekit/estimation/sequential/UnivariateProcessNoise.java
index 43cb50f03d10741f10d60e3b119743441b261235..8ffa4f0e15552d65584c08c28092b4c10c2c79e7 100644
--- a/src/main/java/org/orekit/estimation/sequential/UnivariateProcessNoise.java
+++ b/src/main/java/org/orekit/estimation/sequential/UnivariateProcessNoise.java
@@ -34,7 +34,7 @@ import org.orekit.propagation.SpacecraftState;
* The method {@link #getProcessNoiseMatrix} then square the values so that they are consistent with a covariance matrix.
* <p>
* The orbital parameters evolutions are provided in LOF frame and Cartesian (PV);
- * then converted in inertial frame and current {@link OrbitType} and {@link PositionAngle}
+ * then converted in inertial frame and current {@link org.orekit.orbits.OrbitType} and {@link PositionAngle}
* when method {@link #getProcessNoiseMatrix} is called.
* </p>
* <p>
diff --git a/src/main/java/org/orekit/files/ccsds/Keyword.java b/src/main/java/org/orekit/files/ccsds/Keyword.java
index ee7a2bfc03d3f31db8101708107a73719e188df0..80032698fe8d8535dc202bd1a6946cc8b084ee25 100644
--- a/src/main/java/org/orekit/files/ccsds/Keyword.java
+++ b/src/main/java/org/orekit/files/ccsds/Keyword.java
@@ -504,7 +504,7 @@ public enum Keyword {
/** Data: ANGLE_1 in degrees and in [-180, +360[ [deg].<p>
* The value assigned to the ANGLE_1 keyword represents the azimuth, right ascension, or ‘X’
* angle of the measurement, depending on the value of the ANGLE_TYPE keyword.<p>
- * The angle measurement shall be a double precision value as follows: -180.0 <= ANGLE_1 < 360.0<p>
+ * The angle measurement shall be a double precision value as follows: -180.0 ≤ ANGLE_1 < 360.0<p>
* Units shall be degrees.<p>
* See meta-data keyword ANGLE_TYPE for the definition of the angles.
*/
@@ -512,7 +512,7 @@ public enum Keyword {
/** Data: ANGLE_2 in degrees and in [-180, +360[ [deg].<p>
* The value assigned to the ANGLE_2 keyword represents the elevation, declination, or ‘Y’
* angle of the measurement, depending on the value of the ANGLE_TYPE keyword.<p>
- * The angle measurement shall be a double precision value as follows: -180.0 <= ANGLE_2 < 360.0.<p>
+ * The angle measurement shall be a double precision value as follows: -180.0 ≤ ANGLE_2 < 360.0.<p>
* Units shall be degrees.<p>
* See meta-data keyword ANGLE_TYPE for the definition of the angles.
*/
diff --git a/src/main/java/org/orekit/forces/drag/atmosphere/JB2008.java b/src/main/java/org/orekit/forces/drag/atmosphere/JB2008.java
index 81e92fa1bafdb83f56aa4b270d11df9b9f79aed4..0d9e2985981a7a0e2a46acaf4bf23a91488d530e 100644
--- a/src/main/java/org/orekit/forces/drag/atmosphere/JB2008.java
+++ b/src/main/java/org/orekit/forces/drag/atmosphere/JB2008.java
@@ -39,7 +39,7 @@ import org.orekit.utils.PVCoordinatesProvider;
* It is described in the paper:<br>
* <a href="http://sol.spacenvironment.net/~JB2008/pubs/AIAA_2008-6438_JB2008_Model.pdf">A
* New Empirical Thermospheric Density Model JB2008 Using New Solar Indices</a><br>
- * <i>Bruce R. Bowman & al.</i><br>
+ * <i>Bruce R. Bowman & al.</i><br>
* AIAA 2008-6438<br>
* </p>
* <p>
@@ -209,9 +209,9 @@ public class JB2008 implements Atmosphere {
* (Tabular time 2.0 days earlier)
* @param xm10B MG2 81-day ave. centered index<br>
* (Tabular time 2.0 days earlier)
- * @param y10 Solar X-Ray & Lya index scaled to F10<br>
+ * @param y10 Solar X-Ray & Lya index scaled to F10<br>
* (Tabular time 5.0 days earlier)
- * @param y10B Solar X-Ray & Lya 81-day ave. centered index<br>
+ * @param y10B Solar X-Ray & Lya 81-day ave. centered index<br>
* (Tabular time 5.0 days earlier)
* @param dstdtc Temperature change computed from Dst index
* @return total mass-Density at input position (kg/m³)
@@ -469,9 +469,9 @@ public class JB2008 implements Atmosphere {
* (Tabular time 2.0 days earlier)
* @param xm10B MG2 81-day ave. centered index<br>
* (Tabular time 2.0 days earlier)
- * @param y10 Solar X-Ray & Lya index scaled to F10<br>
+ * @param y10 Solar X-Ray & Lya index scaled to F10<br>
* (Tabular time 5.0 days earlier)
- * @param y10B Solar X-Ray & Lya 81-day ave. centered index<br>
+ * @param y10B Solar X-Ray & Lya 81-day ave. centered index<br>
* (Tabular time 5.0 days earlier)
* @param dstdtc Temperature change computed from Dst index
* @param <T> type fo the field elements
diff --git a/src/main/java/org/orekit/forces/drag/atmosphere/JB2008InputParameters.java b/src/main/java/org/orekit/forces/drag/atmosphere/JB2008InputParameters.java
index 5cd28bb9966f1915e88f84806ab06de9fb9e4bcc..89bda5a2332f774a81cda84e764ec0212d90936b 100644
--- a/src/main/java/org/orekit/forces/drag/atmosphere/JB2008InputParameters.java
+++ b/src/main/java/org/orekit/forces/drag/atmosphere/JB2008InputParameters.java
@@ -81,17 +81,17 @@ public interface JB2008InputParameters extends Serializable {
*/
double getXM10B(AbsoluteDate date);
- /** Get the Solar X-Ray & Lya index scaled to F10.
+ /** Get the Solar X-Ray & Lya index scaled to F10.
* <p>Tabular time 5.0 days earlier.</p>
* @param date the current date
- * @return the Solar X-Ray & Lya index scaled to F10
+ * @return the Solar X-Ray & Lya index scaled to F10
*/
double getY10(AbsoluteDate date);
- /** Get the Solar X-Ray & Lya 81-day ave. centered index.
+ /** Get the Solar X-Ray & Lya 81-day ave. centered index.
* <p>Tabular time 5.0 days earlier.</p>
* @param date the current date
- * @return the Solar X-Ray & Lya 81-day ave. centered index
+ * @return the Solar X-Ray & Lya 81-day ave. centered index
*/
double getY10B(AbsoluteDate date);
diff --git a/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00.java b/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00.java
index 8b1725e796d878bdc051c2b266fdc3397eb854b0..8d27ea7bcff3b1bfec6d135f17c16be5432cbc6d 100644
--- a/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00.java
+++ b/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00.java
@@ -121,7 +121,7 @@ import org.orekit.utils.PVCoordinatesProvider;
* Instances of this class are immutable.
* </p>
*
- * @author Mike Picone & al (Naval Research Laboratory), 2001: FORTRAN routine
+ * @author Mike Picone & al (Naval Research Laboratory), 2001: FORTRAN routine
* @author Dominik Brodowski, 2004: C routine
* @author Pascal Parraud, 2016: Java translation
* @since 8.1
diff --git a/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00InputParameters.java b/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00InputParameters.java
index bd0da50e2200f9516c83a018abba195237279a51..ba021b6e9646b5c61fb8965e25c90b75da9734e3 100644
--- a/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00InputParameters.java
+++ b/src/main/java/org/orekit/forces/drag/atmosphere/NRLMSISE00InputParameters.java
@@ -57,14 +57,14 @@ public interface NRLMSISE00InputParameters extends Serializable {
* <p>
* A<sub>p</sub> indices are provided as an array such as:
* <ul>
- * <li>0 -> daily A<sub>p</sub></li>
- * <li>1 -> 3 hr A<sub>p</sub> index for current time</li>
- * <li>2 -> 3 hr A<sub>p</sub> index for 3 hrs before current time</li>
- * <li>3 -> 3 hr A<sub>p</sub> index for 6 hrs before current time</li>
- * <li>4 -> 3 hr A<sub>p</sub> index for 9 hrs before current time</li>
- * <li>5 -> Average of eight 3 hr A<sub>p</sub> indices from 12 to 33 hrs
+ * <li>0 → daily A<sub>p</sub></li>
+ * <li>1 → 3 hr A<sub>p</sub> index for current time</li>
+ * <li>2 → 3 hr A<sub>p</sub> index for 3 hrs before current time</li>
+ * <li>3 → 3 hr A<sub>p</sub> index for 6 hrs before current time</li>
+ * <li>4 → 3 hr A<sub>p</sub> index for 9 hrs before current time</li>
+ * <li>5 → Average of eight 3 hr A<sub>p</sub> indices from 12 to 33 hrs
* prior to current time</li>
- * <li>6 -> Average of eight 3 hr A<sub>p</sub> indices from 36 to 57 hrs
+ * <li>6 → Average of eight 3 hr A<sub>p</sub> indices from 36 to 57 hrs
* prior to current time</li>
* </ul>
* </p>
diff --git a/src/main/java/org/orekit/models/earth/DiscreteTroposphericModel.java b/src/main/java/org/orekit/models/earth/DiscreteTroposphericModel.java
index 99a8f387bb4464aabff22b11e22bd3a829820396..77b7af9c58434706a8e1860ce748eebabfd6cd02 100644
--- a/src/main/java/org/orekit/models/earth/DiscreteTroposphericModel.java
+++ b/src/main/java/org/orekit/models/earth/DiscreteTroposphericModel.java
@@ -64,8 +64,8 @@ public interface DiscreteTroposphericModel extends MappingFunction {
/** This method allows the computation of the zenith hydrostatic and
* zenith wet delay. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>wz</sub> -> zenith wet delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>wz</sub> → zenith wet delay
* </ul>
* @param height the height of the station in m above sea level.
* @param parameters tropospheric model parameters.
@@ -77,8 +77,8 @@ public interface DiscreteTroposphericModel extends MappingFunction {
/** This method allows the computation of the zenith hydrostatic and
* zenith wet delay. The resulting element is an array having the following form:
* <ul>
- * <li>T[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>T[1] = D<sub>wz</sub> -> zenith wet delay
+ * <li>T[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>T[1] = D<sub>wz</sub> → zenith wet delay
* </ul>
* @param <T> type of the elements
* @param height the height of the station in m above sea level.
diff --git a/src/main/java/org/orekit/models/earth/EstimatedTroposphericModel.java b/src/main/java/org/orekit/models/earth/EstimatedTroposphericModel.java
index 6860d35937842fc017b2fa15c95a8683845cd2f4..14dbef7e35790287938b8318a6ac58ea881f7376 100644
--- a/src/main/java/org/orekit/models/earth/EstimatedTroposphericModel.java
+++ b/src/main/java/org/orekit/models/earth/EstimatedTroposphericModel.java
@@ -141,8 +141,8 @@ public class EstimatedTroposphericModel implements DiscreteTroposphericModel {
/** This method allows the computation of the zenith hydrostatic and zenith total delays.
* The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>tz</sub> -> zenith total delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>tz</sub> → zenith total delay
* </ul>
* <p>
* The user have to be careful because the others tropospheric models in Orekit
@@ -172,8 +172,8 @@ public class EstimatedTroposphericModel implements DiscreteTroposphericModel {
/** This method allows the computation of the zenith hydrostatic and zenith total delays.
* The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>tz</sub> -> zenith total delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>tz</sub> → zenith total delay
* </ul>
* <p>
* The user have to be careful because the others tropospheric models in Orekit
diff --git a/src/main/java/org/orekit/models/earth/GlobalPressureTemperatureModel.java b/src/main/java/org/orekit/models/earth/GlobalPressureTemperatureModel.java
index 63aa5e4796d8b1772dfc3a0ade32bca426f585a4..53d0a85f3087c4c141eba5f049467845144e1193 100644
--- a/src/main/java/org/orekit/models/earth/GlobalPressureTemperatureModel.java
+++ b/src/main/java/org/orekit/models/earth/GlobalPressureTemperatureModel.java
@@ -64,7 +64,7 @@ public class GlobalPressureTemperatureModel implements WeatherModel {
/** Build a new instance.
* <p>
* At the initialization the values of the pressure and the temperature are set to NaN.
- * The user has to call {@link #computeTemperatureAndPressure} method before using
+ * The user has to call {@link #weatherParameters(double, AbsoluteDate)} method before using
* the values of the pressure and the temperature.
* </p>
* @param latitude geodetic latitude, in radians
diff --git a/src/main/java/org/orekit/models/earth/MappingFunction.java b/src/main/java/org/orekit/models/earth/MappingFunction.java
index 9e765f9c35e24035df0d8fe36d67d048cbed4ab3..5975bef91d768aab73feb91a748e9946513209fb 100644
--- a/src/main/java/org/orekit/models/earth/MappingFunction.java
+++ b/src/main/java/org/orekit/models/earth/MappingFunction.java
@@ -34,8 +34,8 @@ public interface MappingFunction extends Serializable {
/** This method allows the computation of the hydrostatic and
* wet mapping functions. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = m<sub>h</sub>(e) -> hydrostatic mapping function
- * <li>double[1] = m<sub>w</sub>(e) -> wet mapping function
+ * <li>double[0] = m<sub>h</sub>(e) → hydrostatic mapping function
+ * <li>double[1] = m<sub>w</sub>(e) → wet mapping function
* </ul>
* @param elevation the elevation of the satellite, in radians.
* @param height the height of the station in m above sea level.
@@ -48,8 +48,8 @@ public interface MappingFunction extends Serializable {
/** This method allows the computation of the hydrostatic and
* wet mapping functions. The resulting element is an array having the following form:
* <ul>
- * <li>T[0] = m<sub>h</sub>(e) -> hydrostatic mapping function
- * <li>T[1] = m<sub>w</sub>(e) -> wet mapping function
+ * <li>T[0] = m<sub>h</sub>(e) → hydrostatic mapping function
+ * <li>T[1] = m<sub>w</sub>(e) → wet mapping function
* </ul>
* @param elevation the elevation of the satellite, in radians.
* @param height the height of the station in m above sea level.
diff --git a/src/main/java/org/orekit/models/earth/MendesPavlisModel.java b/src/main/java/org/orekit/models/earth/MendesPavlisModel.java
index ff29a266fb1f98639a10a1834f381b323c5a0923..d44841a2092df6e9566dc3aa9c24589a4e82e946 100644
--- a/src/main/java/org/orekit/models/earth/MendesPavlisModel.java
+++ b/src/main/java/org/orekit/models/earth/MendesPavlisModel.java
@@ -83,7 +83,7 @@ public class MendesPavlisModel implements DiscreteTroposphericModel {
* thanks to the values of the pressure, the temperature and the humidity
* @param t0 the temperature at the station, K
* @param p0 the atmospheric pressure at the station, hPa
- * @param rh the humidity at the station, percent (50% -> 0.5)
+ * @param rh the humidity at the station, percent (50% → 0.5)
* @param latitude geodetic latitude of the station, radians
* @param lambda laser wavelength, µm
* */
@@ -225,8 +225,8 @@ public class MendesPavlisModel implements DiscreteTroposphericModel {
* Therefore, the two components of the resulting array are
* equals.
* <ul>
- * <li>double[0] = m(e) -> total mapping function
- * <li>double[1] = m(e) -> total mapping function
+ * <li>double[0] = m(e) → total mapping function
+ * <li>double[1] = m(e) → total mapping function
* </ul>
* </p><p>
* The total delay will thus be computed as this:
@@ -365,7 +365,7 @@ public class MendesPavlisModel implements DiscreteTroposphericModel {
*
* See: Giacomo, P., Equation for the dertermination of the density of moist air, Metrologia, V. 18, 1982
*
- * @param rh relative humidity, in percent (50% -> 0.5).
+ * @param rh relative humidity, in percent (50% → 0.5).
* @return the water vapor, in mbar (1 mbar = 1 hPa).
*/
private double getWaterVapor(final double rh) {
diff --git a/src/main/java/org/orekit/models/earth/TroposphericModel.java b/src/main/java/org/orekit/models/earth/TroposphericModel.java
index 190e2828c82a705a9a3acfaf497632a3523a446e..119fcefc86b81ef91522afd9b1cd1c953c78580d 100644
--- a/src/main/java/org/orekit/models/earth/TroposphericModel.java
+++ b/src/main/java/org/orekit/models/earth/TroposphericModel.java
@@ -93,8 +93,8 @@ public interface TroposphericModel extends DiscreteTroposphericModel {
/** This method allows the computation of the zenith hydrostatic and
* zenith wet delay. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>wz</sub> -> zenith wet delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>wz</sub> → zenith wet delay
* </ul>
* @param height the height of the station in m above sea level.
* @param parameters tropospheric model parameters.
@@ -111,8 +111,8 @@ public interface TroposphericModel extends DiscreteTroposphericModel {
/** This method allows the computation of the zenith hydrostatic and
* zenith wet delay. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>wz</sub> -> zenith wet delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>wz</sub> → zenith wet delay
* </ul>
* @param <T> type of the elements
* @param height the height of the station in m above sea level.
@@ -132,8 +132,8 @@ public interface TroposphericModel extends DiscreteTroposphericModel {
/** This method allows the computation of the hydrostatic and
* wet mapping functions. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = m<sub>h</sub>(e) -> hydrostatic mapping function
- * <li>double[1] = m<sub>w</sub>(e) -> wet mapping function
+ * <li>double[0] = m<sub>h</sub>(e) → hydrostatic mapping function
+ * <li>double[1] = m<sub>w</sub>(e) → wet mapping function
* </ul>
* @param elevation the elevation of the satellite, in radians.
* @param height the height of the station in m above sea level.
@@ -151,8 +151,8 @@ public interface TroposphericModel extends DiscreteTroposphericModel {
/** This method allows the computation of the hydrostatic and
* wet mapping functions. The resulting element is an array having the following form:
* <ul>
- * <li>double[0] = m<sub>h</sub>(e) -> hydrostatic mapping function
- * <li>double[1] = m<sub>w</sub>(e) -> wet mapping function
+ * <li>double[0] = m<sub>h</sub>(e) → hydrostatic mapping function
+ * <li>double[1] = m<sub>w</sub>(e) → wet mapping function
* </ul>
* @param elevation the elevation of the satellite, in radians.
* @param height the height of the station in m above sea level.
diff --git a/src/main/java/org/orekit/models/earth/ViennaModelCoefficientsLoader.java b/src/main/java/org/orekit/models/earth/ViennaModelCoefficientsLoader.java
index 3bac36856b0b9e5437ddc01c52d2b7aa80f3463a..101ce77b76fb273df314ed15256a686f49c4d38d 100644
--- a/src/main/java/org/orekit/models/earth/ViennaModelCoefficientsLoader.java
+++ b/src/main/java/org/orekit/models/earth/ViennaModelCoefficientsLoader.java
@@ -142,8 +142,8 @@ public class ViennaModelCoefficientsLoader implements DataLoader {
/** Returns the zenith delay array.
* <ul>
- * <li>double[0] = D<sub>hz</sub> -> zenith hydrostatic delay
- * <li>double[1] = D<sub>wz</sub> -> zenith wet delay
+ * <li>double[0] = D<sub>hz</sub> → zenith hydrostatic delay
+ * <li>double[1] = D<sub>wz</sub> → zenith wet delay
* </ul>
* @return the zenith delay array
*/
diff --git a/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java b/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java
index 70c5ade2a96a6c956e5e25ce109b20f8fb1d6692..2129fe4b7b1c8927fa2b8fcb979a4801c171749b 100644
--- a/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java
+++ b/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java
@@ -875,7 +875,7 @@ public class FieldKeplerianOrbit<T extends RealFieldElement<T>> extends FieldOrb
* @return position vector
* @deprecated as of 9.3 replaced with {@link #FieldKeplerianOrbit(RealFieldElement, RealFieldElement,
* RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame,
- * FieldAbsoluteDate, double)} and {@#getPVCoordinates()}
+ * FieldAbsoluteDate, double)} and {@link #getPVCoordinates()}
*/
@Deprecated
public static <T extends RealFieldElement<T>> FieldVector3D<T> ellipticKeplerianToPosition(final T a, final T e, final T i,
@@ -925,7 +925,7 @@ public class FieldKeplerianOrbit<T extends RealFieldElement<T>> extends FieldOrb
* @return position vector
* @deprecated as of 9.3 replaced with {@link #FieldKeplerianOrbit(RealFieldElement, RealFieldElement,
* RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame,
- * FieldAbsoluteDate, double)} and {@#getPVCoordinates()}
+ * FieldAbsoluteDate, double)} and {@link #getPVCoordinates()}
*/
@Deprecated
public static <T extends RealFieldElement<T>> FieldVector3D<T> hyperbolicKeplerianToPosition(final T a, final T e, final T i,
diff --git a/src/main/java/org/orekit/propagation/PropagatorsParallelizer.java b/src/main/java/org/orekit/propagation/PropagatorsParallelizer.java
index 9e9d246e8d22a133bc5d0a8bb66eef7480e91311..c5ec321cc93628e2652c2f1886e5de44ba074197 100644
--- a/src/main/java/org/orekit/propagation/PropagatorsParallelizer.java
+++ b/src/main/java/org/orekit/propagation/PropagatorsParallelizer.java
@@ -64,15 +64,15 @@ import org.orekit.time.TimeStamped;
* simulation times flows from left to right:
* </p>
* <pre>
- * propagator 1 : -------------[++++current step++++]>
+ * propagator 1 : -------------[++++current step++++]>
* |
- * propagator 2 : ----[++++current step++++]--------->
+ * propagator 2 : ----[++++current step++++]--------->
* | |
* ... | |
- * propagator n : ---------[++++current step++++]---->
+ * propagator n : ---------[++++current step++++]---->
* | |
* V V
- * global handler : -------------[global step]--------->
+ * global handler : -------------[global step]--------->
* </pre>
* <p>
* The previous sketch shows that propagator 1 has already computed states
diff --git a/src/main/java/org/orekit/propagation/analytical/FieldEcksteinHechlerPropagator.java b/src/main/java/org/orekit/propagation/analytical/FieldEcksteinHechlerPropagator.java
index 20e4943ffa4ff36d26af045605d71094eb5aacab..f8f3c21e39828a3533c2c8177a01f991099c46c6 100644
--- a/src/main/java/org/orekit/propagation/analytical/FieldEcksteinHechlerPropagator.java
+++ b/src/main/java/org/orekit/propagation/analytical/FieldEcksteinHechlerPropagator.java
@@ -40,7 +40,7 @@ import org.orekit.utils.TimeStampedFieldPVCoordinates;
/** This class propagates a {@link org.orekit.propagation.FieldSpacecraftState}
* using the analytical Eckstein-Hechler model.
* <p>The Eckstein-Hechler model is suited for near circular orbits
- * (e < 0.1, with poor accuracy between 0.005 and 0.1) and inclination
+ * (e < 0.1, with poor accuracy between 0.005 and 0.1) and inclination
* neither equatorial (direct or retrograde) nor critical (direct or
* retrograde).</p>
* @see FieldOrbit
diff --git a/src/main/java/org/orekit/propagation/events/FunctionalDetector.java b/src/main/java/org/orekit/propagation/events/FunctionalDetector.java
index 94cf715ac5bc9411542a8424ff10e865e19f1b94..d7964412ade15c43c54f0d6ce497824d3e340b2b 100644
--- a/src/main/java/org/orekit/propagation/events/FunctionalDetector.java
+++ b/src/main/java/org/orekit/propagation/events/FunctionalDetector.java
@@ -30,7 +30,7 @@ import org.orekit.propagation.events.handlers.EventHandler;
*
* <code><pre>
* FunctionalDetector d = new FunctionalDetector()
- * .withGFunction((s)-> s.getDate().durationFrom(triggerDate))
+ * .withGFunction((s) -> s.getDate().durationFrom(triggerDate))
* .withMaxCheck(1e10);
* </pre></code>
*
diff --git a/src/main/java/org/orekit/propagation/integration/FieldAdditionalEquations.java b/src/main/java/org/orekit/propagation/integration/FieldAdditionalEquations.java
index 327eaec6b1d59818a46c33b31a4d0e13159abb6b..43b10bab1f66782aa0db9cf17b521fe6c7124451 100644
--- a/src/main/java/org/orekit/propagation/integration/FieldAdditionalEquations.java
+++ b/src/main/java/org/orekit/propagation/integration/FieldAdditionalEquations.java
@@ -18,8 +18,6 @@ package org.orekit.propagation.integration;
import org.hipparchus.RealFieldElement;
import org.orekit.propagation.FieldSpacecraftState;
-import org.orekit.propagation.SpacecraftState;
-import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
/** This interface allows users to add their own differential equations to a numerical propagator.
@@ -45,8 +43,8 @@ import org.orekit.time.FieldAbsoluteDate;
* the pDot array, which is the time-derivative of the p array. Since the additional parameters
* p may also have an influence on the equations of motion themselves that should be accumulated
* to the main state derivatives (for example an equation linked to a complex thrust model may
- * induce an acceleration and a mass change), the {@link #computeDerivatives(FieldSpacecraftState, RealFieldElement[])
- * computeDerivatives} method can return a double array that will be
+ * induce an acceleration and a mass change), the {@link #computeDerivatives(FieldSpacecraftState,
+ * RealFieldElement[]) computeDerivatives} method can return a double array that will be
* <em>added</em> to the main state derivatives. This means these equations can be used as an
* additional force model if needed. If the additional parameters have no influence at all on
* the main spacecraft state, a null reference may be returned.
@@ -73,7 +71,7 @@ public interface FieldAdditionalEquations<T extends RealFieldElement<T>> {
*
* <p>
* This method will be called once at propagation start,
- * before any calls to {@link #computeDerivatives(SpacecraftState , AbsoluteDate[])}.
+ * before any calls to {@link #computeDerivatives(FieldSpacecraftState , RealFieldElement[])}.
* </p>
*
* <p>
diff --git a/src/main/java/org/orekit/propagation/numerical/FieldNumericalPropagator.java b/src/main/java/org/orekit/propagation/numerical/FieldNumericalPropagator.java
index e489b0f8b64d38df715d7f381fa5b2c747d8cf5c..9552f089280663e1d199cfda98d8bdce5ce1e80b 100644
--- a/src/main/java/org/orekit/propagation/numerical/FieldNumericalPropagator.java
+++ b/src/main/java/org/orekit/propagation/numerical/FieldNumericalPropagator.java
@@ -119,9 +119,9 @@ import org.orekit.utils.TimeStampedFieldPVCoordinates;
* final T maxStep = zero.add(500);
* final T initStep = zero.add(60);
* final double[][] tolerance = FieldNumericalPropagator.tolerances(dP, orbit, OrbitType.EQUINOCTIAL);
- * AdaptiveStepsizeFieldIntegrator<T> integrator = new DormandPrince853FieldIntegrator<>(field, minStep, maxStep, tolerance[0], tolerance[1]);
+ * AdaptiveStepsizeFieldIntegrator<T> integrator = new DormandPrince853FieldIntegrator<>(field, minStep, maxStep, tolerance[0], tolerance[1]);
* integrator.setInitialStepSize(initStep);
- * propagator = new FieldNumericalPropagator<>(field, integrator);
+ * propagator = new FieldNumericalPropagator<>(field, integrator);
* </pre>
* <p>By default, at the end of the propagation, the propagator resets the initial state to the final state,
* thus allowing a new propagation to be started from there without recomputing the part already performed.
diff --git a/src/main/java/org/orekit/time/AbsoluteDate.java b/src/main/java/org/orekit/time/AbsoluteDate.java
index c458b6ea557c9fba1f0bc4ca5f6e99e6cf79bd23..5806a8b48468d4ab1a347c8ae71cbf9bfaa93d8e 100644
--- a/src/main/java/org/orekit/time/AbsoluteDate.java
+++ b/src/main/java/org/orekit/time/AbsoluteDate.java
@@ -702,7 +702,7 @@ public class AbsoluteDate
/** Build an instance corresponding to a Julian Epoch (JE).
* <p>According to Lieske paper: <a
- * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
+ * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
* Precession Matrix Based on IAU (1976) System of Astronomical Constants</a>, Astronomy and Astrophysics,
* vol. 73, no. 3, Mar. 1979, p. 282-284, Julian Epoch is related to Julian Ephemeris Date as:</p>
* <pre>
@@ -723,7 +723,7 @@ public class AbsoluteDate
/** Build an instance corresponding to a Besselian Epoch (BE).
* <p>According to Lieske paper: <a
- * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
+ * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
* Precession Matrix Based on IAU (1976) System of Astronomical Constants</a>, Astronomy and Astrophysics,
* vol. 73, no. 3, Mar. 1979, p. 282-284, Besselian Epoch is related to Julian Ephemeris Date as:</p>
* <pre>
diff --git a/src/main/java/org/orekit/time/FieldAbsoluteDate.java b/src/main/java/org/orekit/time/FieldAbsoluteDate.java
index 8dbf3b7b6dd6bd8a707b5aca06810eaba8c73567..25bcaedfad183550f29abf13450d88044a1f9705 100644
--- a/src/main/java/org/orekit/time/FieldAbsoluteDate.java
+++ b/src/main/java/org/orekit/time/FieldAbsoluteDate.java
@@ -45,7 +45,7 @@ import org.orekit.utils.Constants;
* in UTC and write it in another file in TAI. This can be done as follows:</p>
* <pre>
* DateTimeComponents utcComponents = readNextDate();
- * FieldAbsoluteDate<T> date = new FieldAbsoluteDate<>(utcComponents, TimeScalesFactory.getUTC());
+ * FieldAbsoluteDate<T> date = new FieldAbsoluteDate<>(utcComponents, TimeScalesFactory.getUTC());
* writeNextDate(date.getComponents(TimeScalesFactory.getTAI()));
* </pre>
*
@@ -669,7 +669,7 @@ public class FieldAbsoluteDate<T extends RealFieldElement<T>>
/** Build an instance corresponding to a Julian Epoch (JE).
* <p>According to Lieske paper: <a
- * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
+ * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
* Precession Matrix Based on IAU (1976) System of Astronomical Constants</a>, Astronomy and Astrophysics,
* vol. 73, no. 3, Mar. 1979, p. 282-284, Julian Epoch is related to Julian Ephemeris Date as:</p>
* <pre>
@@ -691,7 +691,7 @@ public class FieldAbsoluteDate<T extends RealFieldElement<T>>
/** Build an instance corresponding to a Besselian Epoch (BE).
* <p>According to Lieske paper: <a
- * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
+ * href="http://articles.adsabs.harvard.edu/cgi-bin/nph-iarticle_query?1979A%26A....73..282L&defaultprint=YES&filetype=.pdf.">
* Precession Matrix Based on IAU (1976) System of Astronomical Constants</a>, Astronomy and Astrophysics,
* vol. 73, no. 3, Mar. 1979, p. 282-284, Besselian Epoch is related to Julian Ephemeris Date as:</p>
* <pre>
@@ -814,7 +814,7 @@ public class FieldAbsoluteDate<T extends RealFieldElement<T>>
/** Get a time-shifted date.
* <p>
- * Calling this method is equivalent to call <code>new FieldAbsoluteDate<>(this, dt)</code>.
+ * Calling this method is equivalent to call {@code new FieldAbsoluteDate<>(this, dt)}.
* </p>
* @param dt time shift in seconds
* @return a new date, shifted with respect to instance (which is immutable)
diff --git a/src/main/java/org/orekit/time/FieldTimeStamped.java b/src/main/java/org/orekit/time/FieldTimeStamped.java
index 3982d0e9ff5a3a6ddc79b2d72a8883a1aa58656b..3f312bc2c54805ec184d4c1216763601b998c3bb 100644
--- a/src/main/java/org/orekit/time/FieldTimeStamped.java
+++ b/src/main/java/org/orekit/time/FieldTimeStamped.java
@@ -25,8 +25,8 @@ import org.hipparchus.RealFieldElement;
* underlying comparator. An example using for {@link org.orekit.orbits.Orbit
* Orbit} instances is given here:</p>
* <pre>
- * SortedSet<Orbit> sortedOrbits =
- * new TreeSet<Orbit>(new ChronologicalComparator());
+ * SortedSet<Orbit> sortedOrbits =
+ * new TreeSet<Orbit>(new ChronologicalComparator());
* sortedOrbits.add(orbit1);
* sortedOrbits.add(orbit2);
* ...