/*!
 * satellite-js v5.0.0
 * (c) 2013 Shashwat Kandadai and UCSC
 * https://github.com/shashwatak/satellite-js
 * License: MIT
 */

"use strict";

Object.defineProperty(exports, "__esModule", {
  value: true
});
exports["default"] = dpper;
var _constants = require("../constants");
/* -----------------------------------------------------------------------------
 *
 *                           procedure dpper
 *
 *  this procedure provides deep space long period periodic contributions
 *    to the mean elements.  by design, these periodics are zero at epoch.
 *    this used to be dscom which included initialization, but it's really a
 *    recurring function.
 *
 *  author        : david vallado                  719-573-2600   28 jun 2005
 *
 *  inputs        :
 *    e3          -
 *    ee2         -
 *    peo         -
 *    pgho        -
 *    pho         -
 *    pinco       -
 *    plo         -
 *    se2 , se3 , sgh2, sgh3, sgh4, sh2, sh3, si2, si3, sl2, sl3, sl4 -
 *    t           -
 *    xh2, xh3, xi2, xi3, xl2, xl3, xl4 -
 *    zmol        -
 *    zmos        -
 *    ep          - eccentricity                           0.0 - 1.0
 *    inclo       - inclination - needed for lyddane modification
 *    nodep       - right ascension of ascending node
 *    argpp       - argument of perigee
 *    mp          - mean anomaly
 *
 *  outputs       :
 *    ep          - eccentricity                           0.0 - 1.0
 *    inclp       - inclination
 *    nodep        - right ascension of ascending node
 *    argpp       - argument of perigee
 *    mp          - mean anomaly
 *
 *  locals        :
 *    alfdp       -
 *    betdp       -
 *    cosip  , sinip  , cosop  , sinop  ,
 *    dalf        -
 *    dbet        -
 *    dls         -
 *    f2, f3      -
 *    pe          -
 *    pgh         -
 *    ph          -
 *    pinc        -
 *    pl          -
 *    sel   , ses   , sghl  , sghs  , shl   , shs   , sil   , sinzf , sis   ,
 *    sll   , sls
 *    xls         -
 *    xnoh        -
 *    zf          -
 *    zm          -
 *
 *  coupling      :
 *    none.
 *
 *  references    :
 *    hoots, roehrich, norad spacetrack report #3 1980
 *    hoots, norad spacetrack report #6 1986
 *    hoots, schumacher and glover 2004
 *    vallado, crawford, hujsak, kelso  2006
 ----------------------------------------------------------------------------*/
function dpper(satrec, options) {
  var e3 = satrec.e3,
    ee2 = satrec.ee2,
    peo = satrec.peo,
    pgho = satrec.pgho,
    pho = satrec.pho,
    pinco = satrec.pinco,
    plo = satrec.plo,
    se2 = satrec.se2,
    se3 = satrec.se3,
    sgh2 = satrec.sgh2,
    sgh3 = satrec.sgh3,
    sgh4 = satrec.sgh4,
    sh2 = satrec.sh2,
    sh3 = satrec.sh3,
    si2 = satrec.si2,
    si3 = satrec.si3,
    sl2 = satrec.sl2,
    sl3 = satrec.sl3,
    sl4 = satrec.sl4,
    t = satrec.t,
    xgh2 = satrec.xgh2,
    xgh3 = satrec.xgh3,
    xgh4 = satrec.xgh4,
    xh2 = satrec.xh2,
    xh3 = satrec.xh3,
    xi2 = satrec.xi2,
    xi3 = satrec.xi3,
    xl2 = satrec.xl2,
    xl3 = satrec.xl3,
    xl4 = satrec.xl4,
    zmol = satrec.zmol,
    zmos = satrec.zmos;
  var init = options.init,
    opsmode = options.opsmode;
  var ep = options.ep,
    inclp = options.inclp,
    nodep = options.nodep,
    argpp = options.argpp,
    mp = options.mp;

  // Copy satellite attributes into local variables for convenience
  // and symmetry in writing formulae.

  var alfdp;
  var betdp;
  var cosip;
  var sinip;
  var cosop;
  var sinop;
  var dalf;
  var dbet;
  var dls;
  var f2;
  var f3;
  var pe;
  var pgh;
  var ph;
  var pinc;
  var pl;
  var sinzf;
  var xls;
  var xnoh;
  var zf;
  var zm;

  //  ---------------------- constants -----------------------------
  var zns = 1.19459e-5;
  var zes = 0.01675;
  var znl = 1.5835218e-4;
  var zel = 0.05490;

  //  --------------- calculate time varying periodics -----------
  zm = zmos + zns * t;

  // be sure that the initial call has time set to zero
  if (init === 'y') {
    zm = zmos;
  }
  zf = zm + 2.0 * zes * Math.sin(zm);
  sinzf = Math.sin(zf);
  f2 = 0.5 * sinzf * sinzf - 0.25;
  f3 = -0.5 * sinzf * Math.cos(zf);
  var ses = se2 * f2 + se3 * f3;
  var sis = si2 * f2 + si3 * f3;
  var sls = sl2 * f2 + sl3 * f3 + sl4 * sinzf;
  var sghs = sgh2 * f2 + sgh3 * f3 + sgh4 * sinzf;
  var shs = sh2 * f2 + sh3 * f3;
  zm = zmol + znl * t;
  if (init === 'y') {
    zm = zmol;
  }
  zf = zm + 2.0 * zel * Math.sin(zm);
  sinzf = Math.sin(zf);
  f2 = 0.5 * sinzf * sinzf - 0.25;
  f3 = -0.5 * sinzf * Math.cos(zf);
  var sel = ee2 * f2 + e3 * f3;
  var sil = xi2 * f2 + xi3 * f3;
  var sll = xl2 * f2 + xl3 * f3 + xl4 * sinzf;
  var sghl = xgh2 * f2 + xgh3 * f3 + xgh4 * sinzf;
  var shll = xh2 * f2 + xh3 * f3;
  pe = ses + sel;
  pinc = sis + sil;
  pl = sls + sll;
  pgh = sghs + sghl;
  ph = shs + shll;
  if (init === 'n') {
    pe -= peo;
    pinc -= pinco;
    pl -= plo;
    pgh -= pgho;
    ph -= pho;
    inclp += pinc;
    ep += pe;
    sinip = Math.sin(inclp);
    cosip = Math.cos(inclp);

    /* ----------------- apply periodics directly ------------ */
    // sgp4fix for lyddane choice
    // strn3 used original inclination - this is technically feasible
    // gsfc used perturbed inclination - also technically feasible
    // probably best to readjust the 0.2 limit value and limit discontinuity
    // 0.2 rad = 11.45916 deg
    // use next line for original strn3 approach and original inclination
    // if (inclo >= 0.2)
    // use next line for gsfc version and perturbed inclination
    if (inclp >= 0.2) {
      ph /= sinip;
      pgh -= cosip * ph;
      argpp += pgh;
      nodep += ph;
      mp += pl;
    } else {
      //  ---- apply periodics with lyddane modification ----
      sinop = Math.sin(nodep);
      cosop = Math.cos(nodep);
      alfdp = sinip * sinop;
      betdp = sinip * cosop;
      dalf = ph * cosop + pinc * cosip * sinop;
      dbet = -ph * sinop + pinc * cosip * cosop;
      alfdp += dalf;
      betdp += dbet;
      nodep %= _constants.twoPi;

      //  sgp4fix for afspc written intrinsic functions
      //  nodep used without a trigonometric function ahead
      if (nodep < 0.0 && opsmode === 'a') {
        nodep += _constants.twoPi;
      }
      xls = mp + argpp + cosip * nodep;
      dls = pl + pgh - pinc * nodep * sinip;
      xls += dls;
      xnoh = nodep;
      nodep = Math.atan2(alfdp, betdp);

      //  sgp4fix for afspc written intrinsic functions
      //  nodep used without a trigonometric function ahead
      if (nodep < 0.0 && opsmode === 'a') {
        nodep += _constants.twoPi;
      }
      if (Math.abs(xnoh - nodep) > _constants.pi) {
        if (nodep < xnoh) {
          nodep += _constants.twoPi;
        } else {
          nodep -= _constants.twoPi;
        }
      }
      mp += pl;
      argpp = xls - mp - cosip * nodep;
    }
  }
  return {
    ep: ep,
    inclp: inclp,
    nodep: nodep,
    argpp: argpp,
    mp: mp
  };
}