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/*
 * Copyright 1998-2009 University Corporation for Atmospheric Research/Unidata
 *
 * Portions of this software were developed by the Unidata Program at the
 * University Corporation for Atmospheric Research.
 *
 * Access and use of this software shall impose the following obligations
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 * any fee or cost, to use, copy, modify, alter, enhance and distribute
 * this software, and any derivative works thereof, and its supporting
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 * notice appears in all copies of the software, derivative works and
 * supporting documentation.  Further, UCAR requests that the user credit
 * UCAR/Unidata in any publications that result from the use of this
 * software or in any product that includes this software. The names UCAR
 * and/or Unidata, however, may not be used in any advertising or publicity
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 * understands that UCAR/Unidata is not obligated to provide the user with
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 * IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED
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 * DISCLAIMED. IN NO EVENT SHALL UCAR/UNIDATA BE LIABLE FOR ANY SPECIAL,
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//
// Filename: Utm_To_Gdc_Converter.java
//
// Author: Dan Toms, SRI International
//
// Package: GeoTransform http://www.ai.sri.com/geotransform/
//
// Acknowledgements:
// The algorithms used in the package were created by Ralph Toms and
// first appeared as part of the SEDRIS Coordinate Transformation API.
// These were subsequently modified for this package. This package is
// not part of the SEDRIS project, and the Java code written for this
// package has not been certified or tested for correctness by NIMA.
//
// License:
// The contents of this file are subject to GeoTransform License Agreement
// (the "License"); you may not use this file except in compliance with
// the License. You may obtain a copy of the License at
// http://www.ai.sri.com/geotransformtest/license.html
//
// Software distributed under the License is distributed on an "AS IS"
// basis, WITHOUT WARRANTY OF ANY KIND, either express or implied. See
// the License for the specific language governing rights and limitations
// under the License.
//
// Portions are Copyright (c) SRI International, 1998.
//

package ucar.unidata.geoloc.projection;


import ucar.unidata.geoloc.EarthEllipsoid;
import ucar.unidata.geoloc.LatLonPoint;

import ucar.unidata.geoloc.LatLonPointImpl;


import java.lang.*;


/**
 * Class: Utm_To_Gdc_Converter
 * 

* Converts UTM coordinate(s) to GDC. *

* This class provides the capability to convert from * Universal Transverse Mercator (UTM) coordinates to * geodetic (GDC), i.e. lat/long. * This is a direct conversion. * * @author Dan Toms, SRI International *

* modified JCaron 01/2005 *

    *
  1. turn static methods into object methods, to make thread-safe *
  2. rename methods to follow upper/lower case conventions *
  3. add convenience methods for ucar.unidata.geoloc.Projection *
  4. longitude must be in range +=180. *
*

* random testing shows: * avg error x= 0.4 y=0.06 meters * but sometimes x error can be as high as 15 meters * where err = abs(x - inverse(f(x))) *

* timing: inverse(f(x)) takes 2 - 3 microseconds. */ class Utm_To_Gdc_Converter { static final double DEGREES_PER_RADIAN = 57.2957795130823208768; private double A; // major axis private double F; // flattening private double Eps2, Eps25, Con2, EF, Epsp2, Con6, Con24, Con120, Con720, polx2b, polx3b, polx4b, polx5b, conap; private int zone; private boolean hemisphere_north; /** * Constructor using a, f. * * @param a the semi-major axis (meters) for the ellipsoid * @param f the inverse flattening for the ellipsoid * @param zone the UTM zone number (1..60) * @param hemisphere_north true if the UTM coordinate is in the northern hemisphere */ public Utm_To_Gdc_Converter(double a, double f, int zone, boolean hemisphere_north) { init(a, f, zone, hemisphere_north); } /** * Default contructor uses WGS 84 ellipsoid * * @param zone the UTM zone number (1..60) * @param hemisphere_north true if the UTM coordinate is in the northern hemisphere */ public Utm_To_Gdc_Converter(int zone, boolean hemisphere_north) { this(EarthEllipsoid.WGS84, zone, hemisphere_north); // default to wgs 84 } /* * Constructor with ellipsoid. * @param E an Ellipsoid instance for the ellipsoid, e.g. WE_Ellipsoid * @param zone the UTM zone number (1..60) * @param hemisphere_north true if the UTM coordinate is in the northern hemisphere */ /** * Constructor using given ellipse * * @param ellipse use this ellipse. * @param zone the UTM zone number (1..60) * @param hemisphere_north true if the UTM coordinate is in the northern hemisphere */ public Utm_To_Gdc_Converter(EarthEllipsoid ellipse, int zone, boolean hemisphere_north) { init(ellipse.getMajor(), 1.0 / ellipse.getFlattening(), zone, hemisphere_north); } /** * initialize * * @param a major axis * @param f inverse flattening * @param zone UTM zone * @param hemisphere_north is in northern hemisphere */ private void init(double a, double f, int zone, boolean hemisphere_north) { A = a; F = 1.0 / f; // F is flattening this.zone = zone; this.hemisphere_north = hemisphere_north; // Create the ERM constants. Eps2 = (F) * (2.0 - F); Eps25 = .25 * (Eps2); EF = F / (2.0 - F); Con2 = 2 / (1.0 - Eps2); Con6 = .166666666666667; Con24 = 4 * .0416666666666667 / (1 - Eps2); Con120 = .00833333333333333; Con720 = 4 * .00138888888888888 / (1 - Eps2); double polx1a = 1.0 - Eps2 / 4.0 - 3.0 / 64.0 * Math.pow(Eps2, 2) - 5.0 / 256.0 * Math.pow(Eps2, 3) - 175.0 / 16384.0 * Math.pow(Eps2, 4); conap = A * polx1a; double polx2a = 3.0 / 2.0 * EF - 27.0 / 32.0 * Math.pow(EF, 3); double polx4a = 21.0 / 16.0 * Math.pow(EF, 2) - 55.0 / 32.0 * Math.pow(EF, 4); double polx6a = 151.0 / 96.0 * Math.pow(EF, 3); double polx8a = 1097.0 / 512.0 * Math.pow(EF, 4); polx2b = polx2a * 2.0 + polx4a * 4.0 + polx6a * 6.0 + polx8a * 8.0; polx3b = polx4a * -8.0 - polx6a * 32.0 - 80.0 * polx8a; polx4b = polx6a * 32.0 + 192.0 * polx8a; polx5b = -128.0 * polx8a; } public double getA() { return A; } public double getF() { return F; } public int getZone() { return zone; } public boolean isNorth() { return hemisphere_north; } /** * @param x the UTM easting coordinate (meters) * @param y the UTM northing coordinate (meters) * @param latlon put result here * @return LatLonPoint */ public LatLonPoint projToLatLon(double x, double y, LatLonPointImpl latlon) { double source_x, source_y, u, su, cu, su2, xlon0, temp, phi1; double sp, sp2, cp, cp2, tp, tp2, eta2, top, rn, b3, b4, b5, b6, d1, d2; source_x = x * 1000.0; // wants meters source_x = (source_x - 500000.0) / .9996; if (hemisphere_north) { source_y = y * 1000.0 / .9996; } else { source_y = (y * 1000.0 - 1.0E7) / .9996; } u = source_y / conap; /* TEST U TO SEE IF AT POLES */ su = Math.sin(u); cu = Math.cos(u); su2 = su * su; xlon0 = (6.0 * ((double) zone) - 183.0) / DEGREES_PER_RADIAN; temp = polx2b + su2 * (polx3b + su2 * (polx4b + su2 * polx5b)); phi1 = u + su * cu * temp; sp = Math.sin(phi1); cp = Math.cos(phi1); tp = sp / cp; tp2 = tp * tp; sp2 = sp * sp; cp2 = cp * cp; eta2 = Epsp2 * cp2; top = .25 - (sp2 * (Eps2 / 4)); /* inline sq root*/ rn = A / ((.25 - Eps25 * sp2 + .9999944354799 / 4) + (.25 - Eps25 * sp2) / (.25 - Eps25 * sp2 + .9999944354799 / 4)); b3 = 1.0 + tp2 + tp2 + eta2; b4 = 5 + tp2 * (3 - 9 * eta2) + eta2 * (1 - 4 * eta2); b5 = 5 + tp2 * (tp2 * 24.0 + 28.0); b5 += eta2 * (tp2 * 8.0 + 6.0); b6 = 46.0 - 3.0 * eta2 + tp2 * (-252.0 - tp2 * 90.0); b6 = eta2 * (b6 + eta2 * tp2 * (tp2 * 225.0 - 66.0)); b6 += 61.0 + tp2 * (tp2 * 45.0 + 90.0); d1 = source_x / rn; d2 = d1 * d1; double latitude = phi1 - tp * top * (d2 * (Con2 + d2 * ((-Con24) * b4 + d2 * Con720 * b6))); double longitude = xlon0 + d1 * (1.0 + d2 * (-Con6 * b3 + d2 * Con120 * b5)) / cp; latlon.setLatitude(latitude * DEGREES_PER_RADIAN); latlon.setLongitude(longitude * DEGREES_PER_RADIAN); return latlon; } /** * _more_ * * @param from _more_ * @param to _more_ * @return _more_ */ public float[][] projToLatLon(float[][] from, float[][] to) { double source_x, source_y, u, su, cu, su2, temp, phi1; double sp, sp2, cp, cp2, tp, tp2, eta2, top, rn, b3, b4, b5, b6, d1, d2; double xlon0 = (6.0 * ((double) zone) - 183.0) / DEGREES_PER_RADIAN; for (int i = 0; i < from[0].length; i++) { source_x = from[0][i] * 1000.0; // wants meters source_x = (source_x - 500000.0) / .9996; if (hemisphere_north) { source_y = from[1][i] * 1000.0 / .9996; } else { source_y = (from[1][i] * 1000.0 - 1.0E7) / .9996; } u = source_y / conap; su = Math.sin(u); cu = Math.cos(u); su2 = su * su; temp = polx2b + su2 * (polx3b + su2 * (polx4b + su2 * polx5b)); phi1 = u + su * cu * temp; sp = Math.sin(phi1); cp = Math.cos(phi1); tp = sp / cp; tp2 = tp * tp; sp2 = sp * sp; cp2 = cp * cp; eta2 = Epsp2 * cp2; top = .25 - (sp2 * (Eps2 / 4)); /* inline sq root*/ rn = A / ((.25 - Eps25 * sp2 + .9999944354799 / 4) + (.25 - Eps25 * sp2) / (.25 - Eps25 * sp2 + .9999944354799 / 4)); b3 = 1.0 + tp2 + tp2 + eta2; b4 = 5 + tp2 * (3 - 9 * eta2) + eta2 * (1 - 4 * eta2); b5 = 5 + tp2 * (tp2 * 24.0 + 28.0); b5 += eta2 * (tp2 * 8.0 + 6.0); b6 = 46.0 - 3.0 * eta2 + tp2 * (-252.0 - tp2 * 90.0); b6 = eta2 * (b6 + eta2 * tp2 * (tp2 * 225.0 - 66.0)); b6 += 61.0 + tp2 * (tp2 * 45.0 + 90.0); d1 = source_x / rn; d2 = d1 * d1; double latitude = phi1 - tp * top * (d2 * (Con2 + d2 * ((-Con24) * b4 + d2 * Con720 * b6))); double longitude = xlon0 + d1 * (1.0 + d2 * (-Con6 * b3 + d2 * Con120 * b5)) / cp; to[0][i] = (float) (latitude * DEGREES_PER_RADIAN); to[1][i] = (float) (longitude * DEGREES_PER_RADIAN); } return to; } /** * _more_ * * @param from _more_ * @param to _more_ * @return _more_ */ public double[][] projToLatLon(double[][] from, double[][] to) { double source_x, source_y, u, su, cu, su2, temp, phi1; double sp, sp2, cp, cp2, tp, tp2, eta2, top, rn, b3, b4, b5, b6, d1, d2; double xlon0 = (6.0 * ((double) zone) - 183.0) / DEGREES_PER_RADIAN; for (int i = 0; i < from[0].length; i++) { source_x = from[0][i] * 1000.0; // wants meters source_x = (source_x - 500000.0) / .9996; if (hemisphere_north) { source_y = from[1][i] * 1000.0 / .9996; } else { source_y = (from[1][i] * 1000.0 - 1.0E7) / .9996; } u = source_y / conap; su = Math.sin(u); cu = Math.cos(u); su2 = su * su; temp = polx2b + su2 * (polx3b + su2 * (polx4b + su2 * polx5b)); phi1 = u + su * cu * temp; sp = Math.sin(phi1); cp = Math.cos(phi1); tp = sp / cp; tp2 = tp * tp; sp2 = sp * sp; cp2 = cp * cp; eta2 = Epsp2 * cp2; top = .25 - (sp2 * (Eps2 / 4)); /* inline sq root*/ rn = A / ((.25 - Eps25 * sp2 + .9999944354799 / 4) + (.25 - Eps25 * sp2) / (.25 - Eps25 * sp2 + .9999944354799 / 4)); b3 = 1.0 + tp2 + tp2 + eta2; b4 = 5 + tp2 * (3 - 9 * eta2) + eta2 * (1 - 4 * eta2); b5 = 5 + tp2 * (tp2 * 24.0 + 28.0); b5 += eta2 * (tp2 * 8.0 + 6.0); b6 = 46.0 - 3.0 * eta2 + tp2 * (-252.0 - tp2 * 90.0); b6 = eta2 * (b6 + eta2 * tp2 * (tp2 * 225.0 - 66.0)); b6 += 61.0 + tp2 * (tp2 * 45.0 + 90.0); d1 = source_x / rn; d2 = d1 * d1; double latitude = phi1 - tp * top * (d2 * (Con2 + d2 * ((-Con24) * b4 + d2 * Con720 * b6))); double longitude = xlon0 + d1 * (1.0 + d2 * (-Con6 * b3 + d2 * Con120 * b5)) / cp; to[0][i] = (latitude * DEGREES_PER_RADIAN); to[1][i] = (longitude * DEGREES_PER_RADIAN); } return to; } }





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