Fixed JavaDoc due to incompatibilities with HTML5.

src/main/java/org/orekit/bodies/OneAxisEllipsoid.java

@@ -82,22 +82,22 @@ 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;" summary="">
+     * <table border="1" style="background-color:#f5f5dc;">
      * <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>
+     * <tr><td style="background-color:#c9d5c9; padding:5px">GRS 80</td>
      *     <td>{@link org.orekit.utils.Constants#GRS80_EARTH_EQUATORIAL_RADIUS Constants.GRS80_EARTH_EQUATORIAL_RADIUS}</td>
      *     <td>{@link org.orekit.utils.Constants#GRS80_EARTH_FLATTENING Constants.GRS80_EARTH_FLATTENING}</td></tr>
-     * <tr><td style="background-color:#c9d5c9;">WGS84</td>
+     * <tr><td style="background-color:#c9d5c9; padding:5px">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>
-     * <tr><td style="background-color:#c9d5c9;">IERS96</td>
+     * <tr><td style="background-color:#c9d5c9; padding:5px">IERS96</td>
      *     <td>{@link org.orekit.utils.Constants#IERS96_EARTH_EQUATORIAL_RADIUS Constants.IERS96_EARTH_EQUATORIAL_RADIUS}</td>
      *     <td>{@link org.orekit.utils.Constants#IERS96_EARTH_FLATTENING Constants.IERS96_EARTH_FLATTENING}</td></tr>
-     * <tr><td style="background-color:#c9d5c9;">IERS2003</td>
+     * <tr><td style="background-color:#c9d5c9; padding:5px">IERS2003</td>
      *     <td>{@link org.orekit.utils.Constants#IERS2003_EARTH_EQUATORIAL_RADIUS Constants.IERS2003_EARTH_EQUATORIAL_RADIUS}</td>
      *     <td>{@link org.orekit.utils.Constants#IERS2003_EARTH_FLATTENING Constants.IERS2003_EARTH_FLATTENING}</td></tr>
-     * <tr><td style="background-color:#c9d5c9;">IERS2010</td>
+     * <tr><td style="background-color:#c9d5c9; padding:5px">IERS2010</td>
      *     <td>{@link org.orekit.utils.Constants#IERS2010_EARTH_EQUATORIAL_RADIUS Constants.IERS2010_EARTH_EQUATORIAL_RADIUS}</td>
      *     <td>{@link org.orekit.utils.Constants#IERS2010_EARTH_FLATTENING Constants.IERS2010_EARTH_FLATTENING}</td></tr>
      * </table>

src/main/java/org/orekit/files/ccsds/StreamingAemWriter.java

@@ -44,7 +44,7 @@ import org.orekit.utils.TimeStampedAngularCoordinates;
  *
  * <p> Each instance corresponds to a single AEM file.
  *
- * <h3> Metadata </h3>
+ * <h2> Metadata </h2>
  *
  * <p> The AEM metadata used by this writer is described in the following table. Many
  * metadata items are optional or have default values so they do not need to be specified.
@@ -56,7 +56,8 @@ import org.orekit.utils.TimeStampedAngularCoordinates;
  * <p> The AEM metadata for the whole AEM file is set in the {@link
  * #StreamingAemWriter(Appendable, TimeScale, Map) constructor}.
  *
- * <table summary="AEM metada">
+ * <table>
+ * <caption>AEM metadata</caption>
  *     <thead>
  *         <tr>
  *             <th>Keyword

src/main/java/org/orekit/files/ccsds/StreamingOemWriter.java

@@ -56,7 +56,7 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  * <p> Each instance corresponds to a single OEM file. A new OEM ephemeris segment is
  * started by calling {@link #newSegment(Frame, Map)}.
  *
- * <h3> Metadata </h3>
+ * <h2> Metadata </h2>
  *
  * <p> The OEM metadata used by this writer is described in the following table. Many
  * metadata items are optional or have default values so they do not need to be specified.
@@ -70,7 +70,8 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  * be overridden for a particular segment using the {@code metadata} argument to {@link
  * #newSegment(Frame, Map)}.
  *
- * <table summary="OEM metada">
+ * <table>
+ * <caption>OEM metadata</caption>
  *     <thead>
  *         <tr>
  *             <th>Keyword
@@ -170,7 +171,7 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  *        <tr>
  *            <td>{@link Keyword#INTERPOLATION}
  *            <td>Segment
- *            <td>No
+ *            <td>Noupday
  *            <td>
  *            <td>Table 5-3
  *        <tr>
@@ -193,7 +194,7 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  * are EME2000, GCRF, GRC, ICRF, ITRF2000, ITRF-93, ITRF-97, MCI, TDR, TEME, and TOD.
  * Additionally ITRF followed by a four digit year may be used.
  *
- * <h3> Examples </h3>
+ * <h2> Examples </h2>
  *
  * <p> This class can be used as a step handler for a {@link Propagator}, or on its own.
  * Either way the object name and ID must be specified. The following example shows its

src/main/java/org/orekit/files/ilrs/CPFFile.java

@@ -117,7 +117,7 @@ public class CPFFile implements EphemerisFile {
 
     /**
      * Set the interpolation sample.
-     * @param interpolationSample
+     * @param interpolationSample interpolation sample
      */
     public void setInterpolationSample(final int interpolationSample) {
         this.interpolationSample = interpolationSample;

src/main/java/org/orekit/files/ilrs/CRDFile.java

@@ -360,7 +360,7 @@ public class CRDFile {
         /** Elevation [rad]. */
         private final double elevation;
 
-        /** Direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive). */
+        /** Direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive). */
         private final int directionFlag;
 
         /** Angle origin indicator.
@@ -423,7 +423,7 @@ public class CRDFile {
         }
 
         /**
-         * Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
+         * Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
          * @return the direction flag
          */
         public int getDirectionFlag() {

src/main/java/org/orekit/frames/FieldTransform.java

@@ -57,9 +57,9 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  *
  * <p>Instances of this class are guaranteed to be immutable.</p>
  *
- * <h1> Examples </h1>
+ * <h2> Examples </h2>
  *
- * <h2> Example of translation from R<sub>A</sub> to R<sub>B</sub> </h2>
+ * <h3> Example of translation from R<sub>A</sub> to R<sub>B</sub> </h3>
  *
  * <p> We want to transform the {@link FieldPVCoordinates} PV<sub>A</sub> to
  * PV<sub>B</sub> with :
@@ -78,7 +78,7 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  * PVB = R1toR2.transformPVCoordinate(PVA);
  * </pre>
  *
- * <h2> Example of rotation from R<sub>A</sub> to R<sub>B</sub> </h2>
+ * <h3> Example of rotation from R<sub>A</sub> to R<sub>B</sub> </h3>
  * <p> We want to transform the {@link FieldPVCoordinates} PV<sub>A</sub> to
  * PV<sub>B</sub> with
  *

src/main/java/org/orekit/frames/Frame.java

@@ -27,7 +27,7 @@ import org.orekit.time.FieldAbsoluteDate;
 
 /** Tridimensional references frames class.
  *
- * <h1> Frame Presentation </h1>
+ * <h2> Frame Presentation </h2>
  * <p>This class is the base class for all frames in OREKIT. The frames are
  * linked together in a tree with some specific frame chosen as the root of the tree.
  * Each frame is defined by {@link Transform transforms} combining any number

src/main/java/org/orekit/frames/FramesFactory.java

@@ -26,7 +26,7 @@ import org.orekit.utils.IERSConventions;
 
 /** Factory for predefined reference frames.
  *
- * <h1> FramesFactory Presentation </h1>
+ * <h2> FramesFactory Presentation </h2>
  * <p>
  * Several predefined reference {@link Frame frames} are implemented in OREKIT.
  * They are linked together in a tree with the <i>Geocentric

src/main/java/org/orekit/frames/Transform.java

@@ -58,9 +58,9 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  *
  * <p>Instances of this class are guaranteed to be immutable.</p>
  *
- * <h1> Examples </h1>
+ * <h2> Examples </h2>
  *
- * <h2> Example of translation from R<sub>A</sub> to R<sub>B</sub> </h2>
+ * <h3> Example of translation from R<sub>A</sub> to R<sub>B</sub> </h3>
  *
  * <p> We want to transform the {@link PVCoordinates} PV<sub>A</sub> to
  * PV<sub>B</sub> with :
@@ -79,7 +79,7 @@ import org.orekit.utils.TimeStampedPVCoordinates;
  * PVB = R1toR2.transformPVCoordinates(PVA);
  * </code></pre>
  *
- * <h2> Example of rotation from R<sub>A</sub> to R<sub>B</sub> </h2>
+ * <h3> Example of rotation from R<sub>A</sub> to R<sub>B</sub> </h3>
  * <p> We want to transform the {@link PVCoordinates} PV<sub>A</sub> to
  * PV<sub>B</sub> with
  *

src/main/java/org/orekit/orbits/package-info.java

@@ -28,7 +28,7 @@
  * org.orekit.orbits.CartesianOrbit Cartesian} representations are supported.
  * </p>
  *
- * <h3>Design History</h3>
+ * <h2>Design History</h2>
  * <p>
  * Early designs for the orbit package were much more complex than the current design.
  * Looking back at these designs, they tried to do far too much in a single class and
@@ -58,7 +58,7 @@
  * easy to maintain and reusable.
  * </p>
  *
- * <h3>Current state versus evolving state</h3>
+ * <h2>Current state versus evolving state</h2>
  * <p>
  * From the early design, the various orbit classes retained only the kinematical
  * notions at a single time. They basically represent the current state, and
@@ -93,7 +93,7 @@
  * conversions to other frames without having to externally preserve a mapping
  * between orbits and their frame: it is already done. As an example, getting
  * the position and velocity of a satellite given by a circular orbit in a ground
- * station frame is simply a matter of calling <tt>orbit.getPVCoordinates(stationFrame)</tt>,
+ * station frame is simply a matter of calling <code>orbit.getPVCoordinates(stationFrame)</code>,
  * regardless of the frame in which the orbit is defined (GCRF, EME2000, ...).
  * </p>
  *
@@ -114,7 +114,7 @@
  * interface.
  * </p>
  *
- * <h3>Representations Conversions</h3>
+ * <h2>Representations Conversions</h2>
  * <p>
  * All representations can be converted into all other ones. No error is triggered
  * if some conversion is ambiguous (like converting a perfectly circular orbit from

src/main/java/org/orekit/overview.html

 <html>
 OREKIT
 <body>
-<h2>1. Purpose</h2>
+<h1>1. Purpose</h1>
 <p> 
   OREKIT library is a low-level library for space mechanics projects. It is 
 implemented in the JAVA language. 
@@ -25,7 +25,7 @@ implemented in the JAVA language.
       filesystem layout ...)</li>
 </ul>
 
-<h2>2. Features</h2>
+<h1>2. Features</h1>
 <p>
 Orekit can be used for many purposes, from simple geometrical or orbital tools 
 up to complex orbits propagators with several perturbing forces, maneuvers and
@@ -303,7 +303,7 @@ discrete events. Here is a short list of the features offered by the library:</p
   </li>
 </ul>
 
-<h2>3. Dependency</h2>
+<h1>3. Dependency</h1>
 <p>
 OREKIT has only one dependency: the <a href="https://hipparchus.org/">Hipparchus</a>
 open-source library. This library provides mathematical tools for many purposes: geometry,

src/main/java/org/orekit/propagation/FieldSpacecraftState.java

@@ -505,15 +505,15 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
      * Sun and Moon third bodies attractions, drag and solar radiation pressure.
      * Beware that these results will be different for other orbits.
      * </p>
-     * <table border="1" cellpadding="5">
+     * <table border="1">
      * <caption>Extrapolation Error</caption>
      * <tr style="background-color: #ccccff;"><th>interpolation time (s)</th>
      * <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
-     * <tr><td style="background-color: #eeeeff;"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td style="background-color: #eeeeff;">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td style="background-color: #eeeeff;">900</td><td>3141</td><td>3307</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px"> 60</td><td>  18</td><td> 1.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">120</td><td>  72</td><td> 9.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">300</td><td> 447</td><td> 140</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">600</td><td>1601</td><td>1067</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">900</td><td>3141</td><td>3307</td></tr>
      * </table>
      * @param dt time shift in seconds
      * @return a new state, shifted with respect to the instance (which is immutable)
@@ -546,15 +546,15 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
      * Sun and Moon third bodies attractions, drag and solar radiation pressure.
      * Beware that these results will be different for other orbits.
      * </p>
-     * <table border="1" cellpadding="5">
+     * <table border="1">
      * <caption>Extrapolation Error</caption>
      * <tr style="background-color: #ccccff;"><th>interpolation time (s)</th>
      * <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
-     * <tr><td style="background-color: #eeeeff;"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td style="background-color: #eeeeff;">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td style="background-color: #eeeeff;">900</td><td>3141</td><td>3307</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px"> 60</td><td>  18</td><td> 1.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">120</td><td>  72</td><td> 9.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">300</td><td> 447</td><td> 140</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">600</td><td>1601</td><td>1067</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">900</td><td>3141</td><td>3307</td></tr>
      * </table>
      * @param dt time shift in seconds
      * @return a new state, shifted with respect to the instance (which is immutable)

src/main/java/org/orekit/propagation/SpacecraftState.java

@@ -421,15 +421,15 @@ public class SpacecraftState
      * Sun and Moon third bodies attractions, drag and solar radiation pressure.
      * Beware that these results will be different for other orbits.
      * </p>
-     * <table border="1" cellpadding="5">
+     * <table border="1">
      * <caption>Extrapolation Error</caption>
-     * <tr style="background-color: #ccccff;"><th>interpolation time (s)</th>
+     * <tr style="background-color: #ccccff"><th>interpolation time (s)</th>
      * <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
-     * <tr><td style="background-color: #eeeeff;"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td style="background-color: #eeeeff;">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td style="background-color: #eeeeff;">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td style="background-color: #eeeeff;">900</td><td>3141</td><td>3307</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px"> 60</td><td>  18</td><td> 1.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">120</td><td>  72</td><td> 9.1</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">300</td><td> 447</td><td> 140</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">600</td><td>1601</td><td>1067</td></tr>
+     * <tr><td style="background-color: #eeeeff; padding:5px">900</td><td>3141</td><td>3307</td></tr>
      * </table>
      * @param dt time shift in seconds
      * @return a new state, shifted with respect to the instance (which is immutable)

src/main/java/org/orekit/propagation/events/handlers/EventMultipleHandler.java

@@ -34,7 +34,7 @@ import org.orekit.time.AbsoluteDate;
  * the same event can lead to non-deterministic behaviour.
  * This handler manages several handlers. The action returned is based on a priority rule
  * (see {@link #eventOccurred}) :
- * {@link Action#STOP stop} > {@link Action#RESET_STATE resetState} > {@link Action#RESET_DERIVATIVES resetDerivatives} > {@link Action#RESET_EVENTS resetRevents} > {@link Action#CONTINUE continue}
+ * {@link Action#STOP stop} > {@link Action#RESET_STATE resetState} > {@link Action#RESET_DERIVATIVES resetDerivatives} > {@link Action#RESET_EVENTS resetRevents} > {@link Action#CONTINUE continue}
  *
  * @author Lara Hué
  *

src/main/java/org/orekit/propagation/package-info.java

@@ -15,7 +15,7 @@
  * limitations under the License.
  */
 /**
- * <h1> Propagation </h1>
+ * <h2> Propagation </h2>
  *
  * This package provides tools to propagate orbital states with different methods.
  *
@@ -33,7 +33,7 @@
  * the state.
  * </p>
  *
- * <h2> Keplerian propagation </h2>
+ * <h3> Keplerian propagation </h3>
  *
  * <p> The {@link org.orekit.propagation.analytical.KeplerianPropagator}
  * implements the {@link org.orekit.propagation.Propagator}
@@ -43,7 +43,7 @@
  * {@link org.orekit.orbits.EquinoctialOrbit}
  * representation: only the mean anomaly value changes.
  *
- * <h2> Eckstein-Hechler propagation </h2>
+ * <h3> Eckstein-Hechler propagation </h3>
  *
  * <p> This analytical model is suited for near circular orbits and inclination
  * neither equatorial nor critical. It considers J2 to J6 potential
@@ -51,7 +51,7 @@
  * position. As the Keplerian propagator, it implements the
  * {@link org.orekit.propagation.Propagator} interface.
  *
- * <h2> Numerical propagation </h2>
+ * <h3> Numerical propagation </h3>
  *
  * <p> It is the most important part of the OREKIT project. Based on Hipparchus
  * integrators, the {@link org.orekit.propagation.numerical.NumericalPropagator}

src/main/java/org/orekit/time/AGILeapSecondFilesLoader.java

@@ -53,7 +53,7 @@ public class AGILeapSecondFilesLoader extends AbstractSelfFeedingLoader
      * DataContext#getDefault() default data context}.
      *
      * @param supportedNames regular expression for supported files names
-     * @see #TAIUTCDatFilesLoader(String, DataProvidersManager)
+     * @see #AGILeapSecondFilesLoader(String, DataProvidersManager)
      */
     @DefaultDataContext
     public AGILeapSecondFilesLoader(final String supportedNames) {