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desruisseaux pushed a commit to branch geoapi-4.0
in repository https://gitbox.apache.org/repos/asf/sis.git

commit c9746c3198d9cefcde6394e4089cfa5ac506e2b3
Author: Matthieu_Bastianelli <matthieu.bastiane...@geomatys.com>
AuthorDate: Tue Jul 23 12:52:07 2019 +0200

    feat (sis-referencing & internal) : add test for cylindrical 
satellite-tracking projection and refactor of the ConicSatelliteTracking classe 
to use methods instead of lambda expressions
---
 .../referencing/provider/SatelliteTracking.java    |   3 -
 .../projection/ConicSatelliteTracking.java         | 110 +++++++++++++--------
 .../projection/CylindricalSatelliteTracking.java   |   2 +-
 .../projection/ConicSatelliteTrackingTest.java     |  59 ++++++++++-
 .../CylindricalSatelliteTrackingTest.java          | 103 +++++++++++++++++--
 5 files changed, 223 insertions(+), 54 deletions(-)

diff --git 
a/core/sis-referencing/src/main/java/org/apache/sis/internal/referencing/provider/SatelliteTracking.java
 
b/core/sis-referencing/src/main/java/org/apache/sis/internal/referencing/provider/SatelliteTracking.java
index 3e9382d..6784123 100644
--- 
a/core/sis-referencing/src/main/java/org/apache/sis/internal/referencing/provider/SatelliteTracking.java
+++ 
b/core/sis-referencing/src/main/java/org/apache/sis/internal/referencing/provider/SatelliteTracking.java
@@ -19,10 +19,7 @@
 package org.apache.sis.internal.referencing.provider;
 
 import javax.xml.bind.annotation.XmlTransient;
-import static 
org.apache.sis.internal.referencing.provider.AbstractProvider.createZeroConstant;
-import static 
org.apache.sis.internal.referencing.provider.Mercator1SP.LATITUDE_OF_ORIGIN;
 import org.apache.sis.measure.Units;
-import org.apache.sis.metadata.iso.citation.Citations;
 import org.apache.sis.parameter.ParameterBuilder;
 import org.apache.sis.parameter.Parameters;
 import org.apache.sis.referencing.operation.projection.ConicSatelliteTracking;
diff --git 
a/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTracking.java
 
b/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTracking.java
index 3c8d556..f7247df 100644
--- 
a/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTracking.java
+++ 
b/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTracking.java
@@ -27,7 +27,6 @@ import org.opengis.referencing.operation.Matrix;
 import org.opengis.referencing.operation.OperationMethod;
 
 import static java.lang.Math.*;
-import java.util.function.DoubleUnaryOperator;
 import org.apache.sis.internal.referencing.Resources;
 import static org.apache.sis.internal.referencing.provider.SatelliteTracking.*;
 import org.apache.sis.referencing.operation.matrix.MatrixSIS;
@@ -100,11 +99,14 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
      * Projection Cone's constant.
      */
     private final double n;
+    
     /**
-     * Approximation of the limiting lattitude to which the {@code L 
coefficient}
+     * Approximation of the Minimum latitude at infinite radius. 
+     * 
+     * Limiting latitude to which the {@code L coefficient}
      * is associated with a particular case {@code L equals -s0/n}.
      */
-    private final double lattitudeLimit;
+    private final double latitudeLimit;
     /**
      * Boolean attribute indicating if the projection cone's constant is 
positive.
      * */
@@ -174,31 +176,29 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
             final double sin_φ0 = sin(φ0);
             final double φ2 = 
toRadians(initializer.getAndStore(STANDARD_PARALLEL_2));   //appropriated use 
of toRadians??
 
-//        final double F0 = atan( (p2_on_p1*cos2_φ0 - cos_i)/sqrt(cos2_φ0 - 
cos2_i) );
-//        final double F1 = atan( (p2_on_p1*cos2_φ1 - cos_i)/sqrt(cos2_φ1 - 
cos2_i) );
-//        final double F2 = atan( (p2_on_p1*cos2_φ2 - cos_i)/sqrt(cos2_φ2 - 
cos2_i) );
-//        final double dλ0 = -asin(sin_φ0/sin_i);
-//        final double dλ1 = -asin(sin_φ1/sin_i);
-//        final double dλ2 = -asin(sin_φ2/sin_i);   
-//        final double λt0 = atan( tan(dλ0) * cos_i );
-//        final double λt1 = atan( tan(dλ1) * cos_i );
-//        final double λt2 = atan( tan(dλ2) * cos_i );
-            final DoubleUnaryOperator computeFn = (cos2_φn) -> atan((p2_on_p1 
* cos2_φn - cos_i) / sqrt(cos2_φn - cos2_i)); // eq.28-9 in Snyder 
-            final double F0 = computeFn.applyAsDouble(cos2_φ0);
+//            final DoubleUnaryOperator computeFn = (cos2_φn) -> 
atan((p2_on_p1 * cos2_φn - cos_i) / sqrt(cos2_φn - cos2_i)); // eq.28-9 in 
Snyder 
+//            final double F0 = computeFn.applyAsDouble(cos2_φ0);
+//            final double F1 = computeFn.applyAsDouble(cos2_φ1);
+//            final DoubleUnaryOperator computedλn = (sin_φn) -> -asin(sin_φn 
/ sin_i); // eq.28-2a in Snyder 
+//            final double dλ0 = computedλn.applyAsDouble(sin_φ0);
+//            final double dλ1 = computedλn.applyAsDouble(sin_φ1);
+//            final DoubleUnaryOperator computeλtn = (dλn) -> atan(tan(dλn) * 
cos_i); // eq.28-3a in Snyder 
+//            final double λt0 = computeλtn.applyAsDouble(dλ0);
+//            final double λt1 = computeλtn.applyAsDouble(dλ1);
+
+            final double F0 = computeFn(cos2_φ0);
             /*
-         *Inclination of the groundtrack to the meridian at latitude φ1
+             * Inclination of the groundtrack to the meridian at latitude φ1
              */
-            final double F1 = computeFn.applyAsDouble(cos2_φ1);
+            final double F1 = computeFn(cos2_φ1);
 
             cos_φ1xsin_F1 = cos_φ1 * sin(F1);
 
-            final DoubleUnaryOperator computedλn = (sin_φn) -> -asin(sin_φn / 
sin_i); // eq.28-2a in Snyder 
-            final double dλ0 = computedλn.applyAsDouble(sin_φ0);
-            final double dλ1 = computedλn.applyAsDouble(sin_φ1);
+            final double dλ0 = computedλn(sin_φ0);
+            final double dλ1 = computedλn(sin_φ1);
 
-            final DoubleUnaryOperator computeλtn = (dλn) -> atan(tan(dλn) * 
cos_i); // eq.28-3a in Snyder 
-            final double λt0 = computeλtn.applyAsDouble(dλ0);
-            final double λt1 = computeλtn.applyAsDouble(dλ1);
+            final double λt0 = computeλtn(dλ0);
+            final double λt1 = computeλtn(dλ1);
 
             final double L0 = λt0 - p2_on_p1 * dλ0;
             final double L1 = λt1 - p2_on_p1 * dλ1;
@@ -211,10 +211,12 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
                 final double cos_φ2 = cos(φ2);
                 final double cos2_φ2 = cos_φ2 * cos_φ2;
                 final double sin_φ2 = sin(φ2);
-                final double dλ2 = computedλn.applyAsDouble(sin_φ2);
-                final double λt2 = computeλtn.applyAsDouble(dλ2);
+//                final double dλ2 = computedλn.applyAsDouble(sin_φ2);
+                final double dλ2 = computedλn(sin_φ2);
+                final double λt2 = computeλtn(dλ2);
                 final double L2 = λt2 - p2_on_p1 * dλ2;
-                final double F2 = computeFn.applyAsDouble(cos2_φ2);
+//                final double F2 = computeFn.applyAsDouble(cos2_φ2);
+                final double F2 = computeFn(cos2_φ2);
                 n = (F2 - F1) / (L2 - L1);
             } else {
                 n = sin_φ1 * (p2_on_p1 * (2 * cos2_i - cos2_φ1) - cos_i) / 
(p2_on_p1 * cos2_φ1 - cos_i); //eq. 28-17 in Snyder 
@@ -223,28 +225,24 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
             ρ0 = cos_φ1xsin_F1 / (n * sin(n * L0 + s0)); // *R in eq.28-12 in 
Snyder 
 
             //======================== Unsure 
======================================
-            // Aim to assess the limit lattitude associated with -s0/n L-value.
+            // Aim to assess the limit latitude associated with -s0/n L-value.
             //
-            lattitudeLimit = lattitudeFromNewtonMethod(-s0 / n);
+            latitudeLimit = latitudeFromNewtonMethod(-s0 / n);
             positiveN = (n >= 0);
             
//======================================================================
 
 //            //Additionally we can compute the radius of the circle to which 
groundtracks
 //            //are tangent on the map :
 //            ρs = cos_φ1xsin_F1 / n; //*R
-
             
//======================================================================        
             /*
          * At this point, all parameters have been processed. Now process to 
their
          * validation and the initialization of (de)normalize affine 
transforms.
              */
-        final MatrixSIS normalize   = 
context.getMatrix(ContextualParameters.MatrixRole.NORMALIZATION);
-//        final MatrixSIS denormalize = 
context.getMatrix(ContextualParameters.MatrixRole.DENORMALIZATION);
-        normalize  .convertAfter (0, n, null);  //For conic tracking
-//        denormalize.convertBefore(0, 1/PI,     null);
-//        denormalize.convertBefore(1, , null);
+            final MatrixSIS normalize = 
context.getMatrix(ContextualParameters.MatrixRole.NORMALIZATION);
+            normalize.convertAfter(0, n, null);  //For conic tracking
         }else{
-            n = lattitudeLimit = cos_φ1xsin_F1 = s0 = ρ0 = NaN;
+            n = latitudeLimit = cos_φ1xsin_F1 = s0 = ρ0 = NaN;
             positiveN = false;
         }
     }
@@ -275,7 +273,7 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
         /*
          * According to the Snyder (page 236) in those cases cannot or should 
not be plotted.
          */
-        if( ((positiveN)&&(φ<=lattitudeLimit)) || 
((!positiveN)&&(φ>=lattitudeLimit)) ){
+        if( ((positiveN)&&(φ<=latitudeLimit)) || 
((!positiveN)&&(φ>=latitudeLimit)) ){
             throw new 
ProjectionException(Resources.format(Resources.Keys.CanNotTransformCoordinates_2));
         }
         
@@ -285,11 +283,11 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
         final double L      = λt - p2_on_p1 * dλ;
         
         /*
-         * As {@code lattitudeLimit} is an approximation we repeat the test 
here.
+         * As {@code latitudeLimit} is an approximation we repeat the test 
here.
          */
         if( ((positiveN)&&(L<=-s0/n)) || ((!positiveN)&&(L>=-s0/n)) ){
             //TODO if usefull, could we add :
-            // lattitudeLimit = φ;
+            // latitudeLimit = φ;
             throw new 
ProjectionException(Resources.format(Resources.Keys.CanNotTransformCoordinates_2));
         }
         
@@ -349,10 +347,10 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
         
         //TODO ensure that λ0 will be added. ;  In eq. Snyder 28-23 : λ0 + θ/n
         dstPts[dstOff  ] =  θ ;//λ 
-        dstPts[dstOff+1] = lattitudeFromNewtonMethod(L); //φ
+        dstPts[dstOff+1] = latitudeFromNewtonMethod(L); //φ
     }
     
-    protected final double lattitudeFromNewtonMethod(final double l){
+    protected final double latitudeFromNewtonMethod(final double l){
         double dλ = -PI/2;
         double dλn = Double.MIN_VALUE;
         double A, A2, Δdλ;
@@ -382,10 +380,40 @@ public class ConicSatelliteTracking extends 
NormalizedProjection{
     }
     
     
-    public double getLattitudeLimit(){
-        return lattitudeLimit;
+    public double getLatitudeLimit(){
+        return latitudeLimit;
     }
     
+    /**
+     * Method to compute the φn coefficient according to equation 28-9
+     * in Snyder's Map Projections manual.
+     * 
+     * @param cos2_φn : square of the φn 's cosinus.
+     * @return Fn  coefficient associated with the φn latittude.
+     */
+    private double computeFn(final double cos2_φn) {
+        return atan((p2_on_p1 * cos2_φn - cos_i) / sqrt(cos2_φn - cos2_i)); // 
eq.28-9 in Snyder 
+    }
+    /**
+     * Method to compute the φn coefficient according to equation 28-2a
+     * in Snyder's Map Projections manual.
+     * 
+     * @param sin_φn : φn 's sinus.
+     * @return dλn  coefficient associated with the φn latittude.
+     */
+    private double computedλn(final double sin_φn) {
+        return -asin(sin_φn / sin_i); // eq.28-2a in Snyder 
+    }
+    /**
+     * Method to compute the φn coefficient according to equation 28-3a
+     * in Snyder's Map Projections manual.
+     * 
+     * @param dλn  coefficient associated with the φn latittude.
+     * @return λtn  coefficient associated with the φn latittude.
+     */
+    private double computeλtn(final double dλn) {
+        return atan(tan(dλn) * cos_i); // eq.28-3a in Snyder 
+    }
 //    /**
 //     * Radius of the circle radius of the circle to which groundtracks
 //     * are tangent on the map.
diff --git 
a/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTracking.java
 
b/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTracking.java
index 70ea6fe..1284583 100644
--- 
a/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTracking.java
+++ 
b/core/sis-referencing/src/main/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTracking.java
@@ -191,7 +191,7 @@ public class CylindricalSatelliteTracking extends 
ConicSatelliteTracking {
         final double L   = y * dF1 / cos_φ1; // In eq. Snyder 28-19 : L = y * 
dF1 / R . cos_φ1
         
         dstPts[dstOff  ] =  x;
-        dstPts[dstOff+1] = lattitudeFromNewtonMethod(L); //φ
+        dstPts[dstOff+1] = latitudeFromNewtonMethod(L); //φ
     }
 
 }
diff --git 
a/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTrackingTest.java
 
b/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTrackingTest.java
index 28d83df..0b20c88 100644
--- 
a/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTrackingTest.java
+++ 
b/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/ConicSatelliteTrackingTest.java
@@ -18,8 +18,8 @@
  */
 package org.apache.sis.referencing.operation.projection;
 
-import static java.lang.Double.NaN;
 import java.util.Collections;
+import org.apache.sis.internal.referencing.Formulas;
 import org.apache.sis.internal.referencing.NilReferencingObject;
 import org.apache.sis.internal.referencing.provider.SatelliteTracking;
 import org.apache.sis.measure.Units;
@@ -57,7 +57,7 @@ public class ConicSatelliteTrackingTest extends 
MapProjectionTestCase {
      * @param λ0 : central meridian.
      * @param φ1 : first parallel of conformality, with true scale.
      * @param φ2 : second parallel of conformality, without true scale.
-     * @param φ0 : lattitude_of_origin : latitude Crossing the central meridian
+     * @param φ0 : latitude_of_origin : latitude Crossing the central meridian
      * at the desired origin of rectangular coordinates (null or NaN for
      * cylindrical satellite tracking projection.)
      * @return
@@ -98,6 +98,9 @@ public class ConicSatelliteTrackingTest extends 
MapProjectionTestCase {
     /**
      * Tests the projection of a few points on a sphere.
      *
+     * Test based on the numerical example given by Snyder p. 360 to 363 of 
+     * <cite> Map Projections - A working Manual</cite>
+     *
      * @throws FactoryException if an error occurred while creating the map
      * projection.
      * @throws TransformException if an error occurred while projecting a 
point.
@@ -112,7 +115,7 @@ public class ConicSatelliteTrackingTest extends 
MapProjectionTestCase {
                 -90,     //central_meridian
                 45,      //standard_parallel_1
                 70,      //standard_parallel_2
-                30       //lattitude_of_origin
+                30       //latitude_of_origin
         );
         assertTrue(isInverseTransformSupported);
         verifyTransform(
@@ -123,5 +126,55 @@ public class ConicSatelliteTrackingTest extends 
MapProjectionTestCase {
                     0.2001910, 0.2121685
                 });
     }
+    
+    /**
+     * Tests the projection of a few points on a sphere.
+     *
+     * Test based on the sample coordinates for several of the
+     * Satellite-Tracking Projections shown in table 39 from
+     * <cite> Map Projections - A working Manual</cite>
+     *
+     * @throws FactoryException if an error occurred while creating the map
+     * projection.
+     * @throws TransformException if an error occurred while projecting a 
point.
+     */
+    @Test
+    public void testSampleCoordinates() throws FactoryException, 
TransformException {
+        
+        //Following tests don't pass with the former tolerance.
+        tolerance = Formulas.LINEAR_TOLERANCE; 
+        
+        
//----------------------------------------------------------------------
+        // φ1 = 30° ; φ2 = 60°
+        //---------------------
+        createProjection(
+                99.092,  //satellite_orbit_inclination
+                103.267, //satellite_orbital_period
+                1440.0,  //ascending_node_period
+                -90,     //central_meridian
+                30,      //standard_parallel_1
+                60,      //standard_parallel_2
+                30       //latitude_of_origin
+        );
+//        double xConverterFactor=0.017453;
+//        verifyTransform(
+//                new double[]{ // (λ,φ) coordinates in degrees to project.
+//                      0,  0,
+////                     10,  0, 
+////                    -10, 10,
+////                     60, 40,
+////                     80, 70,
+////                    -120, 80.908  //Tracking limit
+//                },
+//                new double[]{ // Expected (x,y) results in metres.
+//                    0, 0,
+////                    xConverterFactor *   10,  0,
+////                    xConverterFactor *  -10,  0.17579,
+////                    xConverterFactor *   60,  0.79741,
+////                    xConverterFactor *   80,  2.34465,
+////                    xConverterFactor * -120,  7.23571 //Tracking limit
+//                });
+        
+    }
 
 }
diff --git 
a/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTrackingTest.java
 
b/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTrackingTest.java
index 0a86ba6..c207af3 100644
--- 
a/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTrackingTest.java
+++ 
b/core/sis-referencing/src/test/java/org/apache/sis/referencing/operation/projection/CylindricalSatelliteTrackingTest.java
@@ -51,7 +51,7 @@ public class CylindricalSatelliteTrackingTest extends 
ConicSatelliteTrackingTest
      * @param λ0 : central meridian.
      * @param φ1 : first parallel of conformality, with true scale.
      * @param φ2 : second parallel of conformality, without true scale.
-     * @param φ0 : lattitude_of_origin : latitude Crossing the central meridian
+     * @param φ0 : latitude_of_origin : latitude Crossing the central meridian
      * at the desired origin of rectangular coordinates (null or NaN for
      * cylindrical satellite tracking projection.)
      * @return
@@ -66,6 +66,9 @@ public class CylindricalSatelliteTrackingTest extends 
ConicSatelliteTrackingTest
     /**
      * Tests the projection of a few points on a sphere.
      *
+     * Test based on the numerical example given by Snyder p. 360 to 363 of 
+     * <cite> Map Projections - A working Manual</cite>
+     * 
      * @throws FactoryException if an error occurred while creating the map
      * projection.
      * @throws TransformException if an error occurred while projecting a 
point.
@@ -89,7 +92,28 @@ public class CylindricalSatelliteTrackingTest extends 
ConicSatelliteTrackingTest
                 new double[]{ // Expected (x,y) results in metres.
                     0.2267249, 0.6459071
                 });
+    }
+    
+    /**
+     * Tests the projection of a few points on a sphere.
+     *
+     * Test based on the sample coordinates for several of the
+     * Satellite-Tracking Projections shown in table 38 from
+     * <cite> Map Projections - A working Manual</cite>
+     *
+     * @throws FactoryException if an error occurred while creating the map
+     * projection.
+     * @throws TransformException if an error occurred while projecting a 
point.
+     */
+    @Test
+    public void testSampleCoordinates() throws FactoryException, 
TransformException {
         
+        //Following tests don't pass with the former tolerance.
+        tolerance = Formulas.LINEAR_TOLERANCE; 
+        
+        
//----------------------------------------------------------------------
+        // φ1 = 0°
+        //---------
         createProjection(
                 99.092,  //satellite_orbit_inclination
                 103.267, //satellite_orbital_period
@@ -97,21 +121,88 @@ public class CylindricalSatelliteTrackingTest extends 
ConicSatelliteTrackingTest
                 0,       //central_meridian
                 0        //standard_parallel_1
         );
+       
+        double xConverterFactor=0.017453;
+        verifyTransform(
+                new double[]{ // (λ,φ) coordinates in degrees to project.
+                      0,  0,
+                     10,  0, 
+                    -10, 10,
+                     60, 40,
+                     80, 70,
+                    -120, 80.908  //Tracking limit
+                },
+                new double[]{ // Expected (x,y) results in metres.
+                    0, 0,
+                    xConverterFactor *   10,  0,
+                    xConverterFactor *  -10,  0.17579,
+                    xConverterFactor *   60,  0.79741,
+                    xConverterFactor *   80,  2.34465,
+                    xConverterFactor * -120,  7.23571 //Tracking limit
+                });
         
-        tolerance = Formulas.LINEAR_TOLERANCE; //Don't pass with the former 
tolerance.
         
-        final double xConverterFactor=0.017453;
+        
//----------------------------------------------------------------------
+        // φ1 = +- 30°
+        //------------
+        createProjection(
+                99.092,  //satellite_orbit_inclination
+                103.267, //satellite_orbital_period
+                1440.0,  //ascending_node_period
+                0,       //central_meridian
+                -30        //standard_parallel_1
+        );
+       
+        xConverterFactor=0.015115;
         verifyTransform(
                 new double[]{ // (λ,φ) coordinates in degrees to project.
                       0,  0,
                      10,  0, 
-                    -10, 10
+                    -10, 10,
+                     60, 40,
+                     80, 70,
+                    -120, 80.908  //Tracking limit
                 },
                 new double[]{ // Expected (x,y) results in metres.
                     0, 0,
-                    xConverterFactor *  10,  0,
-                    xConverterFactor * -10,  0.17579,
+                    xConverterFactor *   10,  0,
+                    xConverterFactor *  -10,  0.14239,
+                    xConverterFactor *   60,  0.64591,
+                    xConverterFactor *   80,  1.89918,
+                    xConverterFactor * -120,  5.86095 //Tracking limit
                 });
+        
+        
//----------------------------------------------------------------------
+        // φ1 = +- 45°
+        //------------
+        createProjection(
+                99.092,  //satellite_orbit_inclination
+                103.267, //satellite_orbital_period
+                1440.0,  //ascending_node_period
+                0,       //central_meridian
+                45        //standard_parallel_1
+        );
+       
+        xConverterFactor=0.012341;
+        verifyTransform(
+                new double[]{ // (λ,φ) coordinates in degrees to project.
+                      0,  0,
+                     10,  0, 
+                    -10, 10,
+                     60, 40,
+                     80, 70,
+                    -120, 80.908  //Tracking limit
+                },
+                new double[]{ // Expected (x,y) results in metres.
+                    0, 0,
+                    xConverterFactor *   10,  0,
+                    xConverterFactor *  -10,  0.10281,
+                    xConverterFactor *   60,  0.46636,
+                    xConverterFactor *   80,  1.37124,
+                    xConverterFactor * -120,  4.23171 //Tracking limit
+                });
+        
+        
     }
     
 }

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