Commit 61e094d5 authored by iSergio's avatar iSergio
Browse files

Added Transforms.computeIcrfToMoonFixedMatrix and... 

Added Transforms.computeIcrfToMoonFixedMatrix and Transforms.computeMoonFixedToIcrfMatrix to compute the transformations between the Moon's fixed frame and ICRF at a given time.
parent b3695ef8

cesiumjs4gwt-main/src/main/java/org/cesiumjs/cs/core/Transforms.java

+38 −0
Original line number Diff line number Diff line
@@ -104,6 +104,44 @@ public class Transforms { 
    @JsMethod

    public static native Matrix3 computeIcrfToFixedMatrix(JulianDate date, Matrix3 result);



    /**

     * Computes a rotation matrix to transform a point or vector from the International Celestial Reference

     * Frame (GCRF/ICRF) inertial frame axes to the Moon-Fixed frame axes at a given time.

     * @param date The time at which to compute the rotation matrix.

     * @return The rotation matrix.

     */

    @JsMethod

    public static native Matrix3 computeIcrfToMoonFixedMatrix(JulianDate date);



    /**

     * Computes a rotation matrix to transform a point or vector from the International Celestial Reference

     * Frame (GCRF/ICRF) inertial frame axes to the Moon-Fixed frame axes at a given time.

     * @param date The time at which to compute the rotation matrix.

     * @param result The object onto which to store the result. If this parameter is not specified, a new instance is created and returned.

     * @return The rotation matrix.

     */

    @JsMethod

    public static native Matrix3 computeIcrfToMoonFixedMatrix(JulianDate date, Matrix3 result);



    /**

     * Computes a rotation matrix to transform a point or vector from the Moon-Fixed frame axes to the International

     * Celestial Reference Frame (GCRF/ICRF) inertial frame axes at a given time.

     * @param date The time at which to compute the rotation matrix.

     * @return The rotation matrix.

     */

    @JsMethod

    public static native Matrix3 computeMoonFixedToIcrfMatrix(JulianDate date);



    /**

     * Computes a rotation matrix to transform a point or vector from the Moon-Fixed frame axes to the International

     * Celestial Reference Frame (GCRF/ICRF) inertial frame axes at a given time.

     * @param date The time at which to compute the rotation matrix.

     * @param result The object onto which to store the result. If this parameter is not specified, a new instance is created and returned.

     * @return The rotation matrix.

     */

    @JsMethod

    public static native Matrix3 computeMoonFixedToIcrfMatrix(JulianDate date, Matrix3 result);



    // TODO: Example



    /**