jtBaseApp/node_modules/proj4/lib/projections/aeqd.js

import adjust_lon from '../common/adjust_lon';
import {HALF_PI, EPSLN} from '../constants/values';

import mlfn from '../common/mlfn';
import e0fn from '../common/e0fn';
import e1fn from '../common/e1fn';
import e2fn from '../common/e2fn';
import e3fn from '../common/e3fn';
import gN from '../common/gN';
import asinz from '../common/asinz';
import imlfn from '../common/imlfn';



export function init() {
  this.sin_p12 = Math.sin(this.lat0);
  this.cos_p12 = Math.cos(this.lat0);
}

export function forward(p) {
  var lon = p.x;
  var lat = p.y;
  var sinphi = Math.sin(p.y);
  var cosphi = Math.cos(p.y);
  var dlon = adjust_lon(lon - this.long0);
  var e0, e1, e2, e3, Mlp, Ml, tanphi, Nl1, Nl, psi, Az, G, H, GH, Hs, c, kp, cos_c, s, s2, s3, s4, s5;
  if (this.sphere) {
    if (Math.abs(this.sin_p12 - 1) <= EPSLN) {
      //North Pole case
      p.x = this.x0 + this.a * (HALF_PI - lat) * Math.sin(dlon);
      p.y = this.y0 - this.a * (HALF_PI - lat) * Math.cos(dlon);
      return p;
    }
    else if (Math.abs(this.sin_p12 + 1) <= EPSLN) {
      //South Pole case
      p.x = this.x0 + this.a * (HALF_PI + lat) * Math.sin(dlon);
      p.y = this.y0 + this.a * (HALF_PI + lat) * Math.cos(dlon);
      return p;
    }
    else {
      //default case
      cos_c = this.sin_p12 * sinphi + this.cos_p12 * cosphi * Math.cos(dlon);
      c = Math.acos(cos_c);
      kp = c ? c / Math.sin(c) : 1;
      p.x = this.x0 + this.a * kp * cosphi * Math.sin(dlon);
      p.y = this.y0 + this.a * kp * (this.cos_p12 * sinphi - this.sin_p12 * cosphi * Math.cos(dlon));
      return p;
    }
  }
  else {
    e0 = e0fn(this.es);
    e1 = e1fn(this.es);
    e2 = e2fn(this.es);
    e3 = e3fn(this.es);
    if (Math.abs(this.sin_p12 - 1) <= EPSLN) {
      //North Pole case
      Mlp = this.a * mlfn(e0, e1, e2, e3, HALF_PI);
      Ml = this.a * mlfn(e0, e1, e2, e3, lat);
      p.x = this.x0 + (Mlp - Ml) * Math.sin(dlon);
      p.y = this.y0 - (Mlp - Ml) * Math.cos(dlon);
      return p;
    }
    else if (Math.abs(this.sin_p12 + 1) <= EPSLN) {
      //South Pole case
      Mlp = this.a * mlfn(e0, e1, e2, e3, HALF_PI);
      Ml = this.a * mlfn(e0, e1, e2, e3, lat);
      p.x = this.x0 + (Mlp + Ml) * Math.sin(dlon);
      p.y = this.y0 + (Mlp + Ml) * Math.cos(dlon);
      return p;
    }
    else {
      //Default case
      tanphi = sinphi / cosphi;
      Nl1 = gN(this.a, this.e, this.sin_p12);
      Nl = gN(this.a, this.e, sinphi);
      psi = Math.atan((1 - this.es) * tanphi + this.es * Nl1 * this.sin_p12 / (Nl * cosphi));
      Az = Math.atan2(Math.sin(dlon), this.cos_p12 * Math.tan(psi) - this.sin_p12 * Math.cos(dlon));
      if (Az === 0) {
        s = Math.asin(this.cos_p12 * Math.sin(psi) - this.sin_p12 * Math.cos(psi));
      }
      else if (Math.abs(Math.abs(Az) - Math.PI) <= EPSLN) {
        s = -Math.asin(this.cos_p12 * Math.sin(psi) - this.sin_p12 * Math.cos(psi));
      }
      else {
        s = Math.asin(Math.sin(dlon) * Math.cos(psi) / Math.sin(Az));
      }
      G = this.e * this.sin_p12 / Math.sqrt(1 - this.es);
      H = this.e * this.cos_p12 * Math.cos(Az) / Math.sqrt(1 - this.es);
      GH = G * H;
      Hs = H * H;
      s2 = s * s;
      s3 = s2 * s;
      s4 = s3 * s;
      s5 = s4 * s;
      c = Nl1 * s * (1 - s2 * Hs * (1 - Hs) / 6 + s3 / 8 * GH * (1 - 2 * Hs) + s4 / 120 * (Hs * (4 - 7 * Hs) - 3 * G * G * (1 - 7 * Hs)) - s5 / 48 * GH);
      p.x = this.x0 + c * Math.sin(Az);
      p.y = this.y0 + c * Math.cos(Az);
      return p;
    }
  }


}

export function inverse(p) {
  p.x -= this.x0;
  p.y -= this.y0;
  var rh, z, sinz, cosz, lon, lat, con, e0, e1, e2, e3, Mlp, M, N1, psi, Az, cosAz, tmp, A, B, D, Ee, F, sinpsi;
  if (this.sphere) {
    rh = Math.sqrt(p.x * p.x + p.y * p.y);
    if (rh > (2 * HALF_PI * this.a)) {
      return;
    }
    z = rh / this.a;

    sinz = Math.sin(z);
    cosz = Math.cos(z);

    lon = this.long0;
    if (Math.abs(rh) <= EPSLN) {
      lat = this.lat0;
    }
    else {
      lat = asinz(cosz * this.sin_p12 + (p.y * sinz * this.cos_p12) / rh);
      con = Math.abs(this.lat0) - HALF_PI;
      if (Math.abs(con) <= EPSLN) {
        if (this.lat0 >= 0) {
          lon = adjust_lon(this.long0 + Math.atan2(p.x, - p.y));
        }
        else {
          lon = adjust_lon(this.long0 - Math.atan2(-p.x, p.y));
        }
      }
      else {
        /*con = cosz - this.sin_p12 * Math.sin(lat);
        if ((Math.abs(con) < EPSLN) && (Math.abs(p.x) < EPSLN)) {
          //no-op, just keep the lon value as is
        } else {
          var temp = Math.atan2((p.x * sinz * this.cos_p12), (con * rh));
          lon = adjust_lon(this.long0 + Math.atan2((p.x * sinz * this.cos_p12), (con * rh)));
        }*/
        lon = adjust_lon(this.long0 + Math.atan2(p.x * sinz, rh * this.cos_p12 * cosz - p.y * this.sin_p12 * sinz));
      }
    }

    p.x = lon;
    p.y = lat;
    return p;
  }
  else {
    e0 = e0fn(this.es);
    e1 = e1fn(this.es);
    e2 = e2fn(this.es);
    e3 = e3fn(this.es);
    if (Math.abs(this.sin_p12 - 1) <= EPSLN) {
      //North pole case
      Mlp = this.a * mlfn(e0, e1, e2, e3, HALF_PI);
      rh = Math.sqrt(p.x * p.x + p.y * p.y);
      M = Mlp - rh;
      lat = imlfn(M / this.a, e0, e1, e2, e3);
      lon = adjust_lon(this.long0 + Math.atan2(p.x, - 1 * p.y));
      p.x = lon;
      p.y = lat;
      return p;
    }
    else if (Math.abs(this.sin_p12 + 1) <= EPSLN) {
      //South pole case
      Mlp = this.a * mlfn(e0, e1, e2, e3, HALF_PI);
      rh = Math.sqrt(p.x * p.x + p.y * p.y);
      M = rh - Mlp;

      lat = imlfn(M / this.a, e0, e1, e2, e3);
      lon = adjust_lon(this.long0 + Math.atan2(p.x, p.y));
      p.x = lon;
      p.y = lat;
      return p;
    }
    else {
      //default case
      rh = Math.sqrt(p.x * p.x + p.y * p.y);
      Az = Math.atan2(p.x, p.y);
      N1 = gN(this.a, this.e, this.sin_p12);
      cosAz = Math.cos(Az);
      tmp = this.e * this.cos_p12 * cosAz;
      A = -tmp * tmp / (1 - this.es);
      B = 3 * this.es * (1 - A) * this.sin_p12 * this.cos_p12 * cosAz / (1 - this.es);
      D = rh / N1;
      Ee = D - A * (1 + A) * Math.pow(D, 3) / 6 - B * (1 + 3 * A) * Math.pow(D, 4) / 24;
      F = 1 - A * Ee * Ee / 2 - D * Ee * Ee * Ee / 6;
      psi = Math.asin(this.sin_p12 * Math.cos(Ee) + this.cos_p12 * Math.sin(Ee) * cosAz);
      lon = adjust_lon(this.long0 + Math.asin(Math.sin(Az) * Math.sin(Ee) / Math.cos(psi)));
      sinpsi = Math.sin(psi);
      lat = Math.atan2((sinpsi - this.es * F * this.sin_p12) * Math.tan(psi), sinpsi * (1 - this.es));
      p.x = lon;
      p.y = lat;
      return p;
    }
  }

}

export var names = ["Azimuthal_Equidistant", "aeqd"];
export default {
  init: init,
  forward: forward,
  inverse: inverse,
  names: names
};