EclipticProvider.java

  1. /* Contributed in the public domain.
  2.  * Licensed to CS GROUP (CS) under one or more
  3.  * contributor license agreements.  See the NOTICE file distributed with
  4.  * this work for additional information regarding copyright ownership.
  5.  * CS licenses this file to You under the Apache License, Version 2.0
  6.  * (the "License"); you may not use this file except in compliance with
  7.  * the License.  You may obtain a copy of the License at
  8.  *
  9.  *   http://www.apache.org/licenses/LICENSE-2.0
  10.  *
  11.  * Unless required by applicable law or agreed to in writing, software
  12.  * distributed under the License is distributed on an "AS IS" BASIS,
  13.  * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
  14.  * See the License for the specific language governing permissions and
  15.  * limitations under the License.
  16.  */
  17. package org.orekit.frames;

  18. import org.hipparchus.CalculusFieldElement;
  19. import org.hipparchus.geometry.euclidean.threed.FieldRotation;
  20. import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
  21. import org.hipparchus.geometry.euclidean.threed.Rotation;
  22. import org.hipparchus.geometry.euclidean.threed.RotationConvention;
  23. import org.hipparchus.geometry.euclidean.threed.Vector3D;
  24. import org.orekit.annotation.DefaultDataContext;
  25. import org.orekit.data.DataContext;
  26. import org.orekit.time.AbsoluteDate;
  27. import org.orekit.time.FieldAbsoluteDate;
  28. import org.orekit.time.TimeScalarFunction;
  29. import org.orekit.time.TimeScales;
  30. import org.orekit.utils.IERSConventions;

  31. /**
  32.  * An inertial frame aligned with the ecliptic.
  33.  * <p>
  34.  * The IAU defines the ecliptic as "the plane perpendicular to the mean heliocentric
  35.  * orbital angular momentum vector of the Earth-Moon barycentre in the BCRS (IAU 2006
  36.  * Resolution B1)." The +z axis is aligned with the angular momentum vector, and the +x
  37.  * axis is aligned with +x axis of {@link Frames#getMOD(IERSConventions) MOD}.
  38.  * </p>
  39.  *
  40.  * <p>
  41.  * This implementation agrees with the JPL 406 ephemerides to within 0.5 arc seconds.
  42.  * </p>
  43.  *
  44.  * @since 7.0
  45.  */
  46. public class EclipticProvider implements TransformProvider {

  47.     /** IERS conventions. */
  48.     private final IERSConventions conventions;

  49.     /** the obliquity of the ecliptic, in radians as a function of time. */
  50.     private final transient TimeScalarFunction obliquity;

  51.     /**
  52.      * Create a transform provider from MOD to an ecliptically aligned frame.
  53.      *
  54.      * <p>This constructor uses the {@link DataContext#getDefault() default data context}.
  55.      *
  56.      * @param conventions IERS conventions
  57.      * @see #EclipticProvider(IERSConventions, TimeScales)
  58.      */
  59.     @DefaultDataContext
  60.     public EclipticProvider(final IERSConventions conventions) {
  61.         this(conventions, DataContext.getDefault().getTimeScales());
  62.     }

  63.     /**
  64.      * Create a transform provider from MOD to an ecliptically aligned frame.
  65.      * @param conventions IERS conventions
  66.      * @param timeScales to use in computing the transformation.
  67.      * @since 10.1
  68.      */
  69.     public EclipticProvider(final IERSConventions conventions,
  70.                             final TimeScales timeScales) {
  71.         this.conventions = conventions;
  72.         this.obliquity   = conventions.getMeanObliquityFunction(timeScales);
  73.     }

  74.     @Override
  75.     public Transform getTransform(final AbsoluteDate date) {
  76.         //mean obliquity of date
  77.         final double epsA = obliquity.value(date);
  78.         return new Transform(date, new Rotation(Vector3D.MINUS_I, epsA, RotationConvention.VECTOR_OPERATOR));
  79.     }

  80.     @Override
  81.     public <T extends CalculusFieldElement<T>> FieldTransform<T> getTransform(final FieldAbsoluteDate<T> date) {
  82.         //mean obliquity of date
  83.         final T epsA = obliquity.value(date);
  84.         return new FieldTransform<>(date, new FieldRotation<>(FieldVector3D.getMinusI(date.getField()),
  85.                                                               epsA,
  86.                                                               RotationConvention.VECTOR_OPERATOR));
  87.     }

  88. }