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/**
******************************************************************************
*
* @file lks94projection.cpp
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
* @brief
* @see The GNU Public License (GPL) Version 3
* @defgroup OPMapWidget
* @{
*
*****************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#include "lks94projection.h"
#include <qmath.h>
// These pragmas are local modifications to this third party library to silence warnings
#ifdef Q_OS_LINUX
#pragma GCC diagnostic push
#pragma GCC diagnostic ignored "-Wunused-but-set-variable"
#endif
namespace projections {
LKS94Projection::LKS94Projection():MinLatitude (53.33 ), MaxLatitude (56.55 ), MinLongitude (20.22 ),
MaxLongitude (27.11 ), orignX (5122000 ), orignY (10000100 ),tileSize(256, 256)
{
}
Size LKS94Projection::TileSize() const
{
return tileSize;
}
double LKS94Projection::Axis() const
{
return 6378137;
}
double LKS94Projection::Flattening() const
{
return (1.0 / 298.257222101);
}
Point LKS94Projection::FromLatLngToPixel(double lat, double lng, int const& zoom)
{
Point ret;
lat = Clip(lat, MinLatitude, MaxLatitude);
lng = Clip(lng, MinLongitude, MaxLongitude);
QVector <double> lks(3);
lks[0]=lng;
lks[1]=lat;
lks = DTM10(lks);
lks = MTD10(lks);
lks = DTM00(lks);
double res = GetTileMatrixResolution(zoom);
ret.SetX((int) floor((lks[0] + orignX) / res));
ret.SetY((int) floor((orignY - lks[1]) / res));
return ret;
}
internals::PointLatLng LKS94Projection::FromPixelToLatLng(int const& x, int const& y, int const& zoom)
{
internals::PointLatLng ret;// = internals::PointLatLng::Empty;
double res = GetTileMatrixResolution(zoom);
QVector <double> lks(2);
lks[0]=(x * res) - orignX;
lks[1]=-(y * res) + orignY;
lks = MTD11(lks);
lks = DTM10(lks);
lks = MTD10(lks);
ret.SetLat(Clip(lks[1], MinLatitude, MaxLatitude));
ret.SetLng(Clip(lks[0], MinLongitude, MaxLongitude));
return ret;
}
QVector <double> LKS94Projection::DTM10(const QVector <double>& lonlat)
{
double es; // Eccentricity squared : (a^2 - b^2)/a^2
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3142451793; // minor axis
double ab; // Semi_major / semi_minor
double ba; // Semi_minor / semi_major
double ses; // Second eccentricity squared : (a^2 - b^2)/b^2
es = 1.0 - (semiMinor * semiMinor) / (semiMajor * semiMajor); //e^2
ses = (pow(semiMajor, 2) - pow(semiMinor, 2)) / pow(semiMinor, 2);
ba = semiMinor / semiMajor;
ab = semiMajor / semiMinor;
// ...
double lon = DegreesToRadians(lonlat[0]);
double lat = DegreesToRadians(lonlat[1]);
double h = lonlat.count() < 3 ? 0 : (lonlat[2] != lonlat[2]) ? 0 : lonlat[2];//TODO NAN
double v = semiMajor / sqrt(1 - es * pow(sin(lat), 2));
double x = (v + h) * cos(lat) * cos(lon);
double y = (v + h) * cos(lat) * sin(lon);
double z = ((1 - es) * v + h) * sin(lat);
QVector <double> ret(3);
ret[0]=x;
ret[1]=y;
ret[2]=z;
return ret;
}
QVector <double> LKS94Projection::MTD10(QVector <double>& pnt)
{
QVector <double> ret(3);
const double COS_67P5 = 0.38268343236508977; // cosine of 67.5 degrees
const double AD_C = 1.0026000; // Toms region 1 constant
double es; // Eccentricity squared : (a^2 - b^2)/a^2
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3141403561; // minor axis
double ab; // Semi_major / semi_minor
double ba; // Semi_minor / semi_major
double ses; // Second eccentricity squared : (a^2 - b^2)/b^2
es = 1.0 - (semiMinor * semiMinor) / (semiMajor * semiMajor); //e^2
ses = (pow(semiMajor, 2) - pow(semiMinor, 2)) / pow(semiMinor, 2);
ba = semiMinor / semiMajor;
ab = semiMajor / semiMinor;
// ...
bool AtPole = false; // is location in polar region
double Z = pnt.count() < 3 ? 0 : (pnt[2] != pnt[2]) ? 0 : pnt[2];//TODO NaN
double lon = 0;
double lat = 0;
double Height = 0;
if(pnt[0] != 0.0)
{
lon = atan2(pnt[1], pnt[0]);
}
else
{
if(pnt[1] > 0)
{
lon = M_PI / 2;
}
else
if(pnt[1] < 0)
{
lon = -M_PI * 0.5;
}
else
{
AtPole = true;
lon = 0.0;
if(Z > 0.0) // north pole
{
lat = M_PI * 0.5;
}
else
if(Z < 0.0) // south pole
{
lat = -M_PI * 0.5;
}
else // center of earth
{
ret[0]=RadiansToDegrees(lon);
ret[1]=RadiansToDegrees(M_PI * 0.5);
ret[2]=-semiMinor;
return ret;
}
}
}
double W2 = pnt[0] * pnt[0] + pnt[1] * pnt[1]; // Square of distance from Z axis
double W = sqrt(W2); // distance from Z axis
double T0 = Z * AD_C; // initial estimate of vertical component
double S0 = sqrt(T0 * T0 + W2); // initial estimate of horizontal component
double Sin_B0 = T0 / S0; // sin(B0), B0 is estimate of Bowring aux variable
double Cos_B0 = W / S0; // cos(B0)
double Sin3_B0 = pow(Sin_B0, 3);
double T1 = Z + semiMinor * ses * Sin3_B0; // corrected estimate of vertical component
double Sum = W - semiMajor * es * Cos_B0 * Cos_B0 * Cos_B0; // numerator of cos(phi1)
double S1 = sqrt(T1 * T1 + Sum * Sum); // corrected estimate of horizontal component
double Sin_p1 = T1 / S1; // sin(phi1), phi1 is estimated latitude
double Cos_p1 = Sum / S1; // cos(phi1)
double Rn = semiMajor / sqrt(1.0 - es * Sin_p1 * Sin_p1); // Earth radius at location
if(Cos_p1 >= COS_67P5)
{
Height = W / Cos_p1 - Rn;
}
else
if(Cos_p1 <= -COS_67P5)
{
Height = W / -Cos_p1 - Rn;
}
else
{
Height = Z / Sin_p1 + Rn * (es - 1.0);
}
if(!AtPole)
{
lat = atan(Sin_p1 / Cos_p1);
}
ret[0]=RadiansToDegrees(lon);
ret[1]=RadiansToDegrees(lat);
ret[2]=Height;
return ret;
}
QVector <double> LKS94Projection::DTM00(QVector <double>& lonlat)
{
double scaleFactor = 0.9998; // scale factor
double centralMeridian = 0.41887902047863912; // Center qlonglongitude (projection center) */
double latOrigin = 0.0; // center latitude
double falseNorthing = 0.0; // y offset in meters
double falseEasting = 500000.0; // x offset in meters
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3141403561; // minor axis
double metersPerUnit = 1.0;
double e0, e1, e2, e3; // eccentricity constants
double e, es, esp; // eccentricity constants
double ml0; // small value m
es = 1.0 - pow(semiMinor / semiMajor, 2);
e = sqrt(es);
e0 = e0fn(es);
e1 = e1fn(es);
e2 = e2fn(es);
e3 = e3fn(es);
ml0 = semiMajor * mlfn(e0, e1, e2, e3, latOrigin);
esp = es / (1.0 - es);
// ...
double lon = DegreesToRadians(lonlat[0]);
double lat = DegreesToRadians(lonlat[1]);
double delta_lon = 0.0; // Delta qlonglongitude (Given qlonglongitude - center)
double sin_phi, cos_phi; // sin and cos value
double al, als; // temporary values
double c, t, tq; // temporary values
double con, n, ml; // cone constant, small m
delta_lon = LKS94Projection::AdjustLongitude(lon - centralMeridian);
LKS94Projection::SinCos(lat, sin_phi, cos_phi);
al = cos_phi * delta_lon;
als = pow(al, 2);
c = pow(cos_phi, 2);
tq = tan(lat);
t = pow(tq, 2);
con = 1.0 - es * pow(sin_phi, 2);
n = semiMajor / sqrt(con);
ml = semiMajor * mlfn(e0, e1, e2, e3, lat);
double x = scaleFactor * n * al * (1.0 + als / 6.0 * (1.0 - t + c + als / 20.0 *
(5.0 - 18.0 * t + pow(t, 2) + 72.0 * c - 58.0 * esp))) + falseEasting;
double y = scaleFactor * (ml - ml0 + n * tq * (als * (0.5 + als / 24.0 *
(5.0 - t + 9.0 * c + 4.0 * pow(c, 2) + als / 30.0 * (61.0 - 58.0 * t
+ pow(t, 2) + 600.0 * c - 330.0 * esp))))) + falseNorthing;
if(lonlat.count() < 3)
{
QVector <double> ret(2);
ret[0]= x / metersPerUnit;
ret[1]= y / metersPerUnit;
return ret;
}
else
{
QVector <double> ret(3);
ret[0]= x / metersPerUnit;
ret[1]= y / metersPerUnit;
ret[2]=lonlat[2];
return ret;
}
}
QVector <double> LKS94Projection::DTM01(QVector <double>& lonlat)
{
double es; // Eccentricity squared : (a^2 - b^2)/a^2
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3141403561; // minor axis
double ab; // Semi_major / semi_minor
double ba; // Semi_minor / semi_major
double ses; // Second eccentricity squared : (a^2 - b^2)/b^2
es = 1.0 - (semiMinor * semiMinor) / (semiMajor * semiMajor);
ses = (pow(semiMajor, 2) -pow(semiMinor, 2)) / pow(semiMinor, 2);
ba = semiMinor / semiMajor;
ab = semiMajor / semiMinor;
// ...
double lon = DegreesToRadians(lonlat[0]);
double lat = DegreesToRadians(lonlat[1]);
double h = lonlat.count() < 3 ? 0 : (lonlat[2] != lonlat[2]) ? 0 : lonlat[2];//TODO NaN
double v = semiMajor / sqrt(1 - es * pow(sin(lat), 2.0));
double x = (v + h) * cos(lat) * cos(lon);
double y = (v + h) * cos(lat) * sin(lon);
double z = ((1 - es) * v + h) * sin(lat);
QVector <double> ret(3);
ret[0]=x;
ret[1]=y;
ret[2]=z;
return ret;
}
QVector <double> LKS94Projection::MTD01(QVector <double>& pnt)
{
const double COS_67P5 = 0.38268343236508977; // cosine of 67.5 degrees
const double AD_C = 1.0026000; // Toms region 1 constant
double es; // Eccentricity squared : (a^2 - b^2)/a^2
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3142451793; // minor axis
double ab; // Semi_major / semi_minor
double ba; // Semi_minor / semi_major
double ses; // Second eccentricity squared : (a^2 - b^2)/b^2
es = 1.0 - (semiMinor * semiMinor) / (semiMajor * semiMajor);
ses = (pow(semiMajor, 2) - pow(semiMinor, 2)) / pow(semiMinor, 2);
ba = semiMinor / semiMajor;
ab = semiMajor / semiMinor;
// ...
bool At_Pole = false; // is location in polar region
double Z = pnt.count() < 3 ? 0 : (pnt[2] != pnt[2]) ? 0 : pnt[2];//TODO NaN
double lon = 0;
double lat = 0;
double Height = 0;
if(pnt[0] != 0.0)
{
lon = atan2(pnt[1], pnt[0]);
}
else
{
if(pnt[1] > 0)
{
lon = M_PI / 2;
}
else
if(pnt[1] < 0)
{
lon = -M_PI * 0.5;
}
else
{
At_Pole = true;
lon = 0.0;
if(Z > 0.0) // north pole
{
lat = M_PI * 0.5;
}
else
if(Z < 0.0) // south pole
{
lat = -M_PI * 0.5;
}
else // center of earth
{
QVector<double> ret(3);
ret[0]=RadiansToDegrees(lon);
ret[1]=RadiansToDegrees(M_PI * 0.5);
ret[2]=-semiMinor;
return ret;
}
}
}
double W2 = pnt[0] * pnt[0] + pnt[1] * pnt[1]; // Square of distance from Z axis
double W = sqrt(W2); // distance from Z axis
double T0 = Z * AD_C; // initial estimate of vertical component
double S0 = sqrt(T0 * T0 + W2); //initial estimate of horizontal component
double Sin_B0 = T0 / S0; // sin(B0), B0 is estimate of Bowring aux variable
double Cos_B0 = W / S0; // cos(B0)
double Sin3_B0 = pow(Sin_B0, 3);
double T1 = Z + semiMinor * ses * Sin3_B0; //corrected estimate of vertical component
double Sum = W - semiMajor * es * Cos_B0 * Cos_B0 * Cos_B0; // numerator of cos(phi1)
double S1 = sqrt(T1 * T1 + Sum * Sum); // corrected estimate of horizontal component
double Sin_p1 = T1 / S1; // sin(phi1), phi1 is estimated latitude
double Cos_p1 = Sum / S1; // cos(phi1)
double Rn = semiMajor / sqrt(1.0 - es * Sin_p1 * Sin_p1); // Earth radius at location
if(Cos_p1 >= COS_67P5)
{
Height = W / Cos_p1 - Rn;
}
else
if(Cos_p1 <= -COS_67P5)
{
Height = W / -Cos_p1 - Rn;
}
else
{
Height = Z / Sin_p1 + Rn * (es - 1.0);
}
if(!At_Pole)
{
lat = atan(Sin_p1 / Cos_p1);
}
QVector<double> ret(3);
ret[0]=RadiansToDegrees(lon);
ret[1]=RadiansToDegrees(lat);
ret[2]=Height;
return ret;
}
QVector <double> LKS94Projection::MTD11(QVector <double>& p)
{
double scaleFactor = 0.9998; // scale factor
double centralMeridian = 0.41887902047863912; // Center qlonglongitude (projection center)
double latOrigin = 0.0; // center latitude
double falseNorthing = 0.0; // y offset in meters
double falseEasting = 500000.0; // x offset in meters
double semiMajor = 6378137.0; // major axis
double semiMinor = 6356752.3141403561; // minor axis
double metersPerUnit = 1.0;
double e0, e1, e2, e3; // eccentricity constants
double e, es, esp; // eccentricity constants
double ml0; // small value m
es =(semiMinor * semiMinor) / (semiMajor * semiMajor);
es=1.0-es;
e = sqrt(es);
e0 = e0fn(es);
e1 = e1fn(es);
e2 = e2fn(es);
e3 = e3fn(es);
ml0 = semiMajor * mlfn(e0, e1, e2, e3, latOrigin);
esp = es / (1.0 - es);
// ...
double con, phi;
double delta_phi;
qlonglong i;
double sin_phi, cos_phi, tan_phi;
double c, cs, t, ts, n, r, d, ds;
qlonglong max_iter = 6;
double x = p[0] * metersPerUnit - falseEasting;
double y = p[1] * metersPerUnit - falseNorthing;
con = (ml0 + y / scaleFactor) / semiMajor;
phi = con;
for(i = 0; ; i++)
{
delta_phi = ((con + e1 * sin(2.0 * phi) - e2 * sin(4.0 * phi) + e3 * sin(6.0 * phi)) / e0) - phi;
phi += delta_phi;
if(fabs(delta_phi) <= EPSLoN)
break;
if(i >= max_iter)
throw "Latitude failed to converge";
}
if(fabs(phi) < HALF_PI)
{
SinCos(phi, sin_phi, cos_phi);
tan_phi = tan(phi);
c = esp * pow(cos_phi, 2);
cs = pow(c, 2);
t = pow(tan_phi, 2);
ts = pow(t, 2);
con = 1.0 - es * pow(sin_phi, 2);
n = semiMajor / sqrt(con);
r = n * (1.0 - es) / con;
d = x / (n * scaleFactor);
ds = pow(d, 2);
double lat = phi - (n * tan_phi * ds / r) * (0.5 - ds / 24.0 * (5.0 + 3.0 * t +
10.0 * c - 4.0 * cs - 9.0 * esp - ds / 30.0 * (61.0 + 90.0 * t +
298.0 * c + 45.0 * ts - 252.0 * esp - 3.0 * cs)));
double lon = AdjustLongitude(centralMeridian + (d * (1.0 - ds / 6.0 * (1.0 + 2.0 * t +
c - ds / 20.0 * (5.0 - 2.0 * c + 28.0 * t - 3.0 * cs + 8.0 * esp +
24.0 * ts))) / cos_phi));
if(p.count() < 3)
{
QVector<double> ret(2);
ret[0]= RadiansToDegrees(lon);
ret[1]= RadiansToDegrees(lat);
return ret;
}
else
{
QVector<double> ret(3);
ret[0]= RadiansToDegrees(lon);
ret[1]= RadiansToDegrees(lat);
ret[2]=p[2];
return ret;
//return new double[] { RadiansToDegrees(lon), RadiansToDegrees(lat), p[2] };
}
}
else
{
if(p.count() < 3)
{
QVector<double> ret(2);
ret[0]= RadiansToDegrees(HALF_PI * Sign(y));
ret[1]= RadiansToDegrees(centralMeridian);
return ret;
}
else
{
QVector<double> ret(3);
ret[0]= RadiansToDegrees(HALF_PI * Sign(y));
ret[1]= RadiansToDegrees(centralMeridian);
ret[2]=p[2];
return ret;
}
}
}
double LKS94Projection::Clip(double const& n, double const& minValue, double const& maxValue)
{
return qMin(qMax(n, minValue), maxValue);
}
double LKS94Projection::GetTileMatrixResolution(int const& zoom)
{
double ret = 0;
switch(zoom)
{
case 0:
{
ret = 1587.50317500635;
}
break;
case 1:
{
ret = 793.751587503175;
}
break;
case 2:
{
ret = 529.167725002117;
}
break;
case 3:
{
ret = 264.583862501058;
}
break;
case 4:
{
ret = 132.291931250529;
}
break;
case 5:
{
ret = 52.9167725002117;
}
break;
case 6:
{
ret = 26.4583862501058;
}
break;
case 7:
{
ret = 13.2291931250529;
}
break;
case 8:
{
ret = 6.61459656252646;
}
break;
case 9:
{
ret = 2.64583862501058;
}
break;
case 10:
{
ret = 1.32291931250529;
}
break;
case 11:
{
ret = 0.529167725002117;
}
break;
}
return ret;
}
double LKS94Projection::GetGroundResolution(int const& zoom, double const& latitude)
{
Q_UNUSED(zoom);
Q_UNUSED(latitude);
return GetTileMatrixResolution(zoom);
}
Size LKS94Projection::GetTileMatrixMinXY(int const& zoom)
{
Size ret;
switch(zoom)
{
case 0:
{
ret = Size(12, 8);
}
break;
case 1:
{
ret = Size(24, 17);
}
break;
case 2:
{
ret = Size(37, 25);
}
break;
case 3:
{
ret = Size(74, 51);
}
break;
case 4:
{
ret = Size(149, 103);
}
break;
case 5:
{
ret = Size(374, 259);
}
break;
case 6:
{
ret = Size(749, 519);
}
break;
case 7:
{
ret = Size(1594, 1100);
}
break;
case 8:
{
ret = Size(3188, 2201);
}
break;
case 9:
{
ret = Size(7971, 5502);
}
break;
case 10:
{
ret = Size(15943, 11005);
}
break;
case 11:
{
ret = Size(39858, 27514);
}
break;
}
return ret;
}
Size LKS94Projection::GetTileMatrixMaxXY(int const& zoom)
{
Size ret;
switch(zoom)
{
case 0:
{
ret = Size(14, 10);
}
break;
case 1:
{
ret = Size(30, 20);
}
break;
case 2:
{
ret = Size(45, 31);
}
break;
case 3:
{
ret = Size(90, 62);
}
break;
case 4:
{
ret = Size(181, 125);
}
break;
case 5:
{
ret = Size(454, 311);
}
break;
case 6:
{
ret = Size(903, 623);
}
break;
case 7:
{
ret = Size(1718, 1193);
}
break;
case 8:
{
ret = Size(3437, 2386);
}
break;
case 9:
{
ret = Size(8594, 5966);
}
break;
case 10:
{
ret = Size(17189, 11932);
}
break;
case 11:
{
ret = Size(42972, 29831);
}
break;
}
return ret;
}
}
#ifdef Q_OS_LINUX
#pragma GCC diagnostic pop
#endif