Fixed issue #980

fe9c002d · Romain Serra · 4948fa11 · fe9c002d · fe9c002d · fe9c002d
Commit fe9c002d authored Dec 04, 2022 by Romain Serra
--- a/src/changes/changes.xml
+++ b/src/changes/changes.xml
@@ -20,6 +20,9 @@
    <title>Orekit Changes</title>
  </properties>
  <body>
+    <action dev="serrof" type="fix" issue="980">
+      Fixed wrong wrapper in deprecated KeplerianOrbit's and FieldKeplerianOrbit's methods for anomaly conversions.
+    </action>
    <release version="11.3" date="2022-10-25"
 			description="Version 11.3 is a minor release of Orekit.
            It includes both new features and bug fixes. New features introduced in 11.3 are:

--- a/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java
+++ b/src/main/java/org/orekit/orbits/FieldKeplerianOrbit.java
@@ -622,10 +622,10 @@ public class FieldKeplerianOrbit<T extends CalculusFieldElement<T>> extends Fiel
     * @param <T> type of the field elements
     * @return v the true anomaly
     * @deprecated As of 11.3, replaced by
-     * {@link FieldKeplerianAnomalyUtility#ellipticEccentricToMean(CalculusFieldElement, CalculusFieldElement)}.
+     * {@link FieldKeplerianAnomalyUtility#ellipticEccentricToTrue(CalculusFieldElement, CalculusFieldElement)}.
     */
    public static <T extends CalculusFieldElement<T>> T ellipticEccentricToTrue(final T E, final T e) {
-        return FieldKeplerianAnomalyUtility.ellipticEccentricToMean(e, E);
+        return FieldKeplerianAnomalyUtility.ellipticEccentricToTrue(e, E);
    }

    /** Computes the elliptic eccentric anomaly from the true anomaly.

--- a/src/main/java/org/orekit/orbits/KeplerianOrbit.java
+++ b/src/main/java/org/orekit/orbits/KeplerianOrbit.java
@@ -611,7 +611,7 @@ public class KeplerianOrbit extends Orbit {
     * @deprecated As of 11.3, replaced by {@link KeplerianAnomalyUtility#ellipticMeanToEccentric(double, double)}.
     */
    public static double meanToEllipticEccentric(final double M, final double e) {
-        return KeplerianAnomalyUtility.ellipticEccentricToMean(e, M);
+        return KeplerianAnomalyUtility.ellipticMeanToEccentric(e, M);
    }

    /** Computes the mean anomaly from the elliptic eccentric anomaly.