Fixed JavaDoc warnings.

src/main/java/org/orekit/estimation/measurements/gnss/GRAPHICCombination.java

@@ -25,14 +25,14 @@ import org.orekit.gnss.SatelliteSystem;
  * combination of measurements.
  * </p>
  * <pre>
- *    m<sub>f</sub> =  0.5 * (Φ<sub>f</sub> + R<sub>f</sub>)
+ *    mf =  0.5 * (Φf + Rf)
  * </pre>
  * With:
  * <ul>
- * <li>m<sub>f</sub> : GRAPHIC measurement.</li>
- * <li>Φ<sub>f</sub> : Phase measurement.</li>
- * <li>R<sub>f</sub> : Code measurement.</li>
- * <li>f             : Frequency.</li>
+ * <li>mf : GRAPHIC measurement.</li>
+ * <li>Φf : Phase measurement.</li>
+ * <li>Rf : Code measurement.</li>
+ * <li>f  : Frequency.</li>
  * </ul>
  * @author Bryan Cazabonne
  * @since 10.1

src/main/java/org/orekit/estimation/measurements/gnss/MelbourneWubbenaCombination.java

@@ -35,18 +35,18 @@ import org.orekit.gnss.SatelliteSystem;
  * narrow-lane combination of code measurements.
  * </p>
  * <pre>
- *    m<sub>MW</sub> =  Φ<sub>WL</sub> - R<sub>NL</sub>
- *    m<sub>MW</sub> =  λ<sub>WL</sub> * N<sub>WL</sub> + b + ε
+ *    mMW =  ΦWL- RNL
+ *    mMW =  λWL * NWL+ b + ε
  * </pre>
  * With:
  * <ul>
- * <li>m<sub>MW</sub> : Melbourne-Wübbena measurement.</li>
- * <li>Φ<sub>WL</sub> : Wide-Lane phase measurement.</li>
- * <li>R<sub>NL</sub> : Narrow-Lane code measurement.</li>
- * <li>λ<sub>WL</sub> : Wide-Lane wavelength.</li>
- * <li>N<sub>WL</sub> : Wide-Lane ambiguity (N<sub>f1</sub> - N<sub>f2</sub>).</li>
- * <li>b              : Satellite and receiver instrumental delays.</li>
- * <li>ε              : Measurement noise.</li>
+ * <li>mMW : Melbourne-Wübbena measurement.</li>
+ * <li>ΦWL : Wide-Lane phase measurement.</li>
+ * <li>RNL : Narrow-Lane code measurement.</li>
+ * <li>λWL : Wide-Lane wavelength.</li>
+ * <li>NWL : Wide-Lane ambiguity (Nf1 - Nf2).</li>
+ * <li>b   : Satellite and receiver instrumental delays.</li>
+ * <li>ε   : Measurement noise.</li>
  * </ul>
  * <p>
  * {@link NarrowLaneCombination Narrow-Lane} and {@link WideLaneCombination Wide-Lane}

src/main/java/org/orekit/estimation/measurements/gnss/PhaseMinusCodeCombination.java

@@ -25,14 +25,14 @@ import org.orekit.gnss.SatelliteSystem;
  * measurements that can be used for cycle-slip detection.
  * </p>
  * <pre>
- *    m<sub>f</sub> =  Φ<sub>f</sub> - R<sub>f</sub>
+ *    mf =  Φf - Rf
  * </pre>
  * With:
  * <ul>
- * <li>m<sub>f</sub> : Phase minus Code measurement.</li>
- * <li>Φ<sub>f</sub> : Phase measurement.</li>
- * <li>R<sub>f</sub> : Code measurement.</li>
- * <li>f             : Frequency.</li>
+ * <li>mf : Phase minus Code measurement.</li>
+ * <li>Φf : Phase measurement.</li>
+ * <li>Rf : Code measurement.</li>
+ * <li>f  : Frequency.</li>
  * </ul>
  * @author Bryan Cazabonne
  * @since 10.1

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

@@ -507,13 +507,13 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
      * </p>
      * <table border="1" cellpadding="5">
      * <caption>Extrapolation Error</caption>
-     * <tr bgcolor="#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 bgcolor="#eeeeff"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td bgcolor="#eeeeff">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td bgcolor="#eeeeff">900</td><td>3141</td><td>3307</td></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>
      * </table>
      * @param dt time shift in seconds
      * @return a new state, shifted with respect to the instance (which is immutable)
@@ -548,13 +548,13 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
      * </p>
      * <table border="1" cellpadding="5">
      * <caption>Extrapolation Error</caption>
-     * <tr bgcolor="#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 bgcolor="#eeeeff"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td bgcolor="#eeeeff">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td bgcolor="#eeeeff">900</td><td>3141</td><td>3307</td></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>
      * </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

@@ -423,13 +423,13 @@ public class SpacecraftState
      * </p>
      * <table border="1" cellpadding="5">
      * <caption>Extrapolation Error</caption>
-     * <tr bgcolor="#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 bgcolor="#eeeeff"> 60</td><td>  18</td><td> 1.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">120</td><td>  72</td><td> 9.1</td></tr>
-     * <tr><td bgcolor="#eeeeff">300</td><td> 447</td><td> 140</td></tr>
-     * <tr><td bgcolor="#eeeeff">600</td><td>1601</td><td>1067</td></tr>
-     * <tr><td bgcolor="#eeeeff">900</td><td>3141</td><td>3307</td></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>
      * </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/analytical/gnss/BeidouPropagator.java

@@ -84,13 +84,14 @@ public class BeidouPropagator extends AbstractGNSSPropagator {
          * </p>
          *
          * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
+         * Another data context can be set using
+         * {@code Builder(final BeidouOrbitalElements gpsOrbElt, final Frames frames)}</p>
          *
          * @param bdsOrbElt the Beidou orbital elements to be used by the Beidou propagator.
          * @see #attitudeProvider(AttitudeProvider provider)
          * @see #mass(double mass)
          * @see #eci(Frame inertial)
          * @see #ecef(Frame bodyFixed)
-         * @see #BeidouPropagator.Builder(BeidouOrbitalElements bdsOrbElt, Frames frames)
          */
         @DefaultDataContext
         public Builder(final BeidouOrbitalElements bdsOrbElt) {

src/main/java/org/orekit/propagation/analytical/gnss/GLONASSAnalyticalPropagator.java

@@ -156,13 +156,14 @@ public class GLONASSAnalyticalPropagator extends AbstractAnalyticalPropagator {
          * </p>
          *
          * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
+         * Another data context can be set using
+         * {@code Builder(final GLONASSOrbitalElements gpsOrbElt, final DataContext dataContext)}</p>
          *
          * @param glonassOrbElt the GLONASS orbital elements to be used by the GLONASS propagator.
          * @see #attitudeProvider(AttitudeProvider provider)
          * @see #mass(double mass)
          * @see #eci(Frame inertial)
          * @see #ecef(Frame bodyFixed)
-         * @see #GLONASSAnalyticalPropagator.Builder(GLONASSOrbitalElements glonassOrbElt, DataContext dataContext)
          */
         @DefaultDataContext
         public Builder(final GLONASSOrbitalElements glonassOrbElt) {

src/main/java/org/orekit/propagation/analytical/gnss/GPSPropagator.java

@@ -82,13 +82,14 @@ public class GPSPropagator extends AbstractGNSSPropagator {
          * </p>
          *
          * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
+         * Another data context can be set using
+         * {@code Builder(final GPSOrbitalElements gpsOrbElt, final Frames frames)}</p>
          *
          * @param gpsOrbElt the GPS orbital elements to be used by the GPSpropagator.
          * @see #attitudeProvider(AttitudeProvider provider)
          * @see #mass(double mass)
          * @see #eci(Frame inertial)
          * @see #ecef(Frame bodyFixed)
-         * @see #GPSPropagator.Builder(GPSOrbitalElements gpsOrbElt, Frames frames)
          */
         @DefaultDataContext
         public Builder(final GPSOrbitalElements gpsOrbElt) {

src/main/java/org/orekit/propagation/analytical/gnss/GalileoPropagator.java

@@ -83,13 +83,14 @@ public class GalileoPropagator extends AbstractGNSSPropagator {
          * </p>
          *
          * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
+         * Another data context can be set using
+         * {@code Builder(final GalileoOrbitalElements gpsOrbElt, final Frames frames)}</p>
          *
          * @param galileoOrbElt the Galileo orbital elements to be used by the Galileo propagator.
          * @see #attitudeProvider(AttitudeProvider provider)
          * @see #mass(double mass)
          * @see #eci(Frame inertial)
          * @see #ecef(Frame bodyFixed)
-         * @see #GalileoPropagator.Builder(GalileoOrbitalElements galileoOrbElt, Frames frames)
          */
         @DefaultDataContext
         public Builder(final GalileoOrbitalElements galileoOrbElt) {

src/main/java/org/orekit/propagation/analytical/gnss/QZSSPropagator.java

@@ -85,13 +85,14 @@ public class QZSSPropagator extends AbstractGNSSPropagator {
          * </p>
          *
          * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
+         * Another data context can be set using
+         * {@code Builder(final QZSSOrbitalElements gpsOrbElt, final Frames frames)}</p>
          *
          * @param qzssOrbElt the QZSS orbital elements to be used by the QZSSpropagator.
          * @see #attitudeProvider(AttitudeProvider provider)
          * @see #mass(double mass)
          * @see #eci(Frame inertial)
          * @see #ecef(Frame bodyFixed)
-         * @see #QZSSPropagator.Builder(QZSSOrbitalElements qzssOrbElt, Frames frames)
          */
         @DefaultDataContext
         public Builder(final QZSSOrbitalElements qzssOrbElt) {

src/main/java/org/orekit/propagation/events/AbstractDetector.java

@@ -33,7 +33,7 @@ public abstract class AbstractDetector<T extends AbstractDetector<T>> implements
     /** Default convergence threshold (s). */
     public static final double DEFAULT_THRESHOLD = 1.e-6;
 
-    /** Default cmaximum number of iterations in the event time search. */
+    /** Default maximum number of iterations in the event time search. */
     public static final int DEFAULT_MAX_ITER = 100;
 
     /** Max check interval. */