svn-gvsig-desktop / tags / v2_0_Build_1217 / libraries / libjni-proj4 / src / PJ_geos.c @ 44178
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/*
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** libproj -- library of cartographic projections
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**
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** Copyright (c) 2004 Gerald I. Evenden
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*/
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static const char |
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LIBPROJ_ID[] = "$Id: PJ_geos.c,v 1.1 2004/10/20 17:04:00 fwarmerdam Exp $";
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/*
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** Permission is hereby granted, free of charge, to any person obtaining
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** a copy of this software and associated documentation files (the
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** "Software"), to deal in the Software without restriction, including
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** without limitation the rights to use, copy, modify, merge, publish,
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** distribute, sublicense, and/or sell copies of the Software, and to
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** permit persons to whom the Software is furnished to do so, subject to
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** the following conditions:
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**
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** The above copyright notice and this permission notice shall be
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** included in all copies or substantial portions of the Software.
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**
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** THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND,
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** EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF
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** MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT.
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** IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY
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** CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT,
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** TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE
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** SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE.
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*/
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#define PROJ_PARMS__ \
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double h; \
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double radius_p; \
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double radius_p2; \
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double radius_p_inv2; \
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double radius_g; \
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double radius_g_1; \
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double C;
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#define PJ_LIB__
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#include <projects.h> |
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PROJ_HEAD(geos, "Geostationary Satellite View") "\n\tAzi, Sph&Ell\n\th="; |
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FORWARD(s_forward); /* spheroid */
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double Vx, Vy, Vz, tmp;
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/* Calculation of the three components of the vector from satellite to
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** position on earth surface (lon,lat).*/
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tmp = cos(lp.phi); |
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Vx = cos (lp.lam) * tmp; |
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Vy = sin (lp.lam) * tmp; |
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Vz = sin (lp.phi); |
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/* Check visibility.*/
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if (((P->radius_g - Vx) * Vx - Vy * Vy - Vz * Vz) < 0.) F_ERROR; |
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/* Calculation based on view angles from satellite.*/
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tmp = P->radius_g - Vx; |
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xy.x = P->radius_g_1 * atan(Vy / tmp); |
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xy.y = P->radius_g_1 * atan(Vz / hypot(Vy, tmp)); |
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return (xy);
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} |
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FORWARD(e_forward); /* ellipsoid */
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double r, Vx, Vy, Vz, tmp;
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/* Calculation of geocentric latitude. */
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lp.phi = atan (P->radius_p2 * tan (lp.phi)); |
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/* Calculation of the three components of the vector from satellite to
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** position on earth surface (lon,lat).*/
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r = (P->radius_p) / hypot(P->radius_p * cos (lp.phi), sin (lp.phi)); |
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Vx = r * cos (lp.lam) * cos (lp.phi); |
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Vy = r * sin (lp.lam) * cos (lp.phi); |
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Vz = r * sin (lp.phi); |
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/* Check visibility. */
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if (((P->radius_g - Vx) * Vx - Vy * Vy - Vz * Vz * P->radius_p_inv2) < 0.) |
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F_ERROR; |
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/* Calculation based on view angles from satellite. */
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tmp = P->radius_g - Vx; |
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xy.x = P->radius_g_1 * atan (Vy / tmp); |
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xy.y = P->radius_g_1 * atan (Vz / hypot (Vy, tmp)); |
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return (xy);
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} |
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INVERSE(s_inverse); /* spheroid */
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double Vx, Vy, Vz, a, b, c, det, k;
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/* Setting three components of vector from satellite to position.*/
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Vx = -1.0; |
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Vy = tan (xy.x / (P->radius_g - 1.0)); |
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Vz = tan (xy.y / (P->radius_g - 1.0)) * sqrt (1.0 + Vy * Vy); |
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/* Calculation of terms in cubic equation and determinant.*/
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a = Vy * Vy + Vz * Vz + Vx * Vx; |
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b = 2 * P->radius_g * Vx;
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if ((det = (b * b) - 4 * a * P->C) < 0.) I_ERROR; |
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/* Calculation of three components of vector from satellite to position.*/
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k = (-b - sqrt(det)) / (2 * a);
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Vx = P->radius_g + k * Vx; |
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Vy *= k; |
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Vz *= k; |
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/* Calculation of longitude and latitude.*/
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lp.lam = atan2 (Vy, Vx); |
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lp.phi = atan (Vz * cos (lp.lam) / Vx); |
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return (lp);
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} |
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INVERSE(e_inverse); /* ellipsoid */
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double Vx, Vy, Vz, a, b, c, det, k;
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/* Setting three components of vector from satellite to position.*/
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Vx = -1.0; |
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Vy = tan (xy.x / P->radius_g_1); |
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Vz = tan (xy.y / P->radius_g_1) * hypot(1.0, Vy); |
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/* Calculation of terms in cubic equation and determinant.*/
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a = Vz / P->radius_p; |
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a = Vy * Vy + a * a + Vx * Vx; |
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b = 2 * P->radius_g * Vx;
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if ((det = (b * b) - 4 * a * P->C) < 0.) I_ERROR; |
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/* Calculation of three components of vector from satellite to position.*/
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k = (-b - sqrt(det)) / (2. * a);
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Vx = P->radius_g + k * Vx; |
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Vy *= k; |
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Vz *= k; |
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/* Calculation of longitude and latitude.*/
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lp.lam = atan2 (Vy, Vx); |
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lp.phi = atan (Vz * cos (lp.lam) / Vx); |
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lp.phi = atan (P->radius_p_inv2 * tan (lp.phi)); |
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return (lp);
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} |
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FREEUP; if (P) free(P); }
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ENTRY0(geos) |
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if ((P->h = pj_param(P->params, "dh").f) <= 0.) E_ERROR(-30); |
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if (P->phi0) E_ERROR(-46); |
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P->radius_g = 1. + (P->radius_g_1 = P->h / P->a);
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P->C = P->radius_g * P->radius_g - 1.0; |
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if (P->es) {
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P->radius_p = sqrt (P->one_es); |
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P->radius_p2 = P->one_es; |
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P->radius_p_inv2 = P->rone_es; |
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P->inv = e_inverse; |
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P->fwd = e_forward; |
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} else {
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P->radius_p = P->radius_p2 = P->radius_p_inv2 = 1.0; |
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P->inv = s_inverse; |
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P->fwd = s_forward; |
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} |
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ENDENTRY(P) |
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/*
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** $Log: PJ_geos.c,v $
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** Revision 1.1 2004/10/20 17:04:00 fwarmerdam
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** New
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**
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** Revision 1.2 2004/07/14 18:08:57 gie
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** corrected P->phi_0 to P->phi0
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**
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** Revision 1.1 2004/07/12 17:58:25 gie
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** Initial revision
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**
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*/
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