Fixed JavaDoc warnings.

src/main/java/org/orekit/forces/drag/AbstractDragForceModel.java

@@ -155,7 +155,7 @@ public abstract class AbstractDragForceModel extends AbstractForceModel {
      * as {@link Atmosphere#getDensity(FieldAbsoluteDate, FieldVector3D, Frame)} in the
      * specific case of {@link DerivativeStructure} with respect to state, so
      * it is less general. However, it is *much* faster in this important case.
-     * <p>
+     * </p>
      * <p>
      * The derivatives should be computed with respect to position. The input
      * parameters already take into account the free parameters (6, 7 or 8 depending
@@ -231,7 +231,7 @@ public abstract class AbstractDragForceModel extends AbstractForceModel {
      * as {@link Atmosphere#getDensity(FieldAbsoluteDate, FieldVector3D, Frame)} in the
      * specific case of {@link Gradient} with respect to state, so
      * it is less general. However, it is *much* faster in this important case.
-     * <p>
+     * </p>
      * <p>
      * The derivatives should be computed with respect to position. The input
      * parameters already take into account the free parameters (6, 7 or 8 depending

src/main/java/org/orekit/forces/maneuvers/trigger/EventBasedManeuverTriggers.java

@@ -132,7 +132,7 @@ public class EventBasedManeuverTriggers implements ManeuverTriggers, EventHandle
      * Method to set the firing state on initialization. can be overloaded by sub
      * classes.
      *
-     * @param initialState
+     * @param initialState initial spacecraft state
      */
     protected void checkInitialFiringState(final SpacecraftState initialState) {
         if (isFiringOnInitialState(initialState)) {
@@ -144,7 +144,7 @@ public class EventBasedManeuverTriggers implements ManeuverTriggers, EventHandle
      * Method to check if the thruster is firing on initialization. can be called by
      * sub classes
      *
-     * @param initialState
+     * @param initialState initial spacecraft state
      * @return true if firing
      */
     protected boolean isFiringOnInitialState(final SpacecraftState initialState) {

src/main/java/org/orekit/propagation/analytical/tle/TLE.java

@@ -258,7 +258,6 @@ public class TLE implements TimeStamped, Serializable {
      *     0 <= ω <= 2π
      *     0 <= meanAnomaly <= 2π
      * </pre>
-     * </p>
      *
      * @param satelliteNumber satellite number
      * @param classification classification (U for unclassified)
@@ -315,7 +314,6 @@ public class TLE implements TimeStamped, Serializable {
      *     0 &lt;= ω &lt;= 2π
      *     0 &lt;= meanAnomaly &lt;= 2π
      * </pre>
-     * </p>
      *
      * @param satelliteNumber satellite number
      * @param classification classification (U for unclassified)

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

@@ -99,8 +99,8 @@ public class FieldFunctionalDetector<T extends RealFieldElement<T>>
 
     /**
      * Create a new event detector with a new g function, keeping all other attributes the
-     * same. It is recommended to use {@link #withMaxCheck(T)} and {@link
-     * #withThreshold(T)} to set appropriate values for this g function.
+     * same. It is recommended to use {@link #withMaxCheck(RealFieldElement)} and {@link
+     * #withThreshold(RealFieldElement)} to set appropriate values for this g function.
      *
      * @param newGFunction the new g function.
      * @return a new detector with the new g function.

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

@@ -186,12 +186,12 @@ public class TimeComponents implements Serializable, Comparable<TimeComponents>
      * satisfy the following constraints. This first guarantees the hour and minute are
      * valid, the second guarantees the second is valid.
      *
-     * <code><pre>
-     *     0 <= secondInDayA + secondInDayB < 86400
-     *     0 <= (secondInDayA + secondInDayB) % 60 + leap < minuteDuration
-     *     0 <= leap <= minuteDuration - 60                        if minuteDuration >= 60
-     *     0 >= leap >= minuteDuration - 60                        if minuteDuration <  60
-     * </pre></code>
+     * <pre>
+     *     {@code 0 <= secondInDayA + secondInDayB < 86400}
+     *     {@code 0 <= (secondInDayA + secondInDayB) % 60 + leap < minuteDuration}
+     *     {@code 0 <= leap <= minuteDuration - 60                        if minuteDuration >= 60}
+     *     {@code 0 >= leap >= minuteDuration - 60                        if minuteDuration <  60}
+     * </pre>
      *
      * <p>If the seconds of minute ({@link #getSecond()}) computed from {@code
      * secondInDayA + secondInDayB + leap} is greater than or equal to {@code
@@ -284,12 +284,12 @@ public class TimeComponents implements Serializable, Comparable<TimeComponents>
      * satisfy the following constraints. This first guarantees the hour and minute are
      * valid, the second guarantees the second is valid.
      *
-     * <code><pre>
-     *     0 <= secondInDayA + secondInDayB < 86400
-     *     0 <= (secondInDayA + secondInDayB) % 60 + leap <= minuteDuration
-     *     0 <= leap <= minuteDuration - 60                        if minuteDuration >= 60
-     *     0 >= leap >= minuteDuration - 60                        if minuteDuration <  60
-     * </pre></code>
+     * <pre>
+     *     {@code 0 <= secondInDayA + secondInDayB < 86400}
+     *     {@code 0 <= (secondInDayA + secondInDayB) % 60 + leap <= minuteDuration}
+     *     {@code 0 <= leap <= minuteDuration - 60                        if minuteDuration >= 60}
+     *     {@code 0 >= leap >= minuteDuration - 60                        if minuteDuration <  60}
+     * </pre>
      *
      * <p>If the seconds of minute ({@link #getSecond()}) computed from {@code
      * secondInDayA + secondInDayB + leap} is greater than or equal to {@code 60 + leap}