public Int32 swe_nod_aps(double tjd_et, Int32 ipl, Int32 iflag,
Int32 method,
double[] xnasc, double[] xndsc,
double[] xperi, double[] xaphe,
ref string serr)
{
int ij, i, j;
Int32 iplx;
Int32 ipli;
int istart, iend;
Int32 iflJ2000;
double plm;
double t = (tjd_et - Sweph.J2000) / 36525, dt;
double[] x = new double[6], xx = new double[24], xobs = new double[6], x2000 = new double[6];
double[][] xpos = CreateArray<double>(3, 6); double[] xnorm = new double[6];
double[] xposm = new double[6];
double[][] xn = CreateArray<double>(3, 6), xs = CreateArray<double>(3, 6);
double[][] xq = CreateArray<double>(3, 6), xa = CreateArray<double>(3, 6);
double[] xobs2 = new double[6], x2 = new double[6];
CPointer<double> xna, xnd, xpe, xap, xp;
double incl, sema, ecce, parg, ea, vincl, vsema, vecce, pargx, eax;
Sweph.plan_data pedp = SE.Sweph.swed.pldat[Sweph.SEI_EARTH];
Sweph.plan_data psbdp = SE.Sweph.swed.pldat[Sweph.SEI_SUNBARY];
Sweph.plan_data pldat = new Sweph.plan_data();
CPointer<double> xsun = psbdp.x;
CPointer<double> xear = pedp.x;
CPointer<double> ep;
double Gmsm, dzmin;
double rxy, rxyz, fac, sgn;
double sinnode, cosnode, sinincl, cosincl, sinu, cosu, sinE, cosE, cosE2;
double uu, ny, ny2, c2, v2, pp, ro, ro2, rn, rn2;
Sweph.epsilon oe;
bool is_true_nodaps = false;
bool do_aberr = 0 == (iflag & (SwissEph.SEFLG_TRUEPOS | SwissEph.SEFLG_NOABERR));
bool do_defl = 0 == (iflag & SwissEph.SEFLG_TRUEPOS) && 0 == (iflag & SwissEph.SEFLG_NOGDEFL);
bool do_focal_point = (method & SwissEph.SE_NODBIT_FOPOINT) != 0;
bool ellipse_is_bary = false;
Int32 iflg0;
iflag &= ~(SwissEph.SEFLG_JPLHOR | SwissEph.SEFLG_JPLHOR_APPROX);
/* function calls for Pluto with asteroid number 134340
* are treated as calls for Pluto as main body SE_PLUTO */
if (ipl == SwissEph.SE_AST_OFFSET + 134340)
ipl = SwissEph.SE_PLUTO;
xna = xx;
xnd = xx.GetPointer(6);
xpe = xx.GetPointer(12);
xap = xx.GetPointer(18);
xpos[0][0] = 0; /* to shut up mint */
/* to get control over the save area: */
SE.Sweph.swi_force_app_pos_etc();
method %= SwissEph.SE_NODBIT_FOPOINT;
ipli = ipl;
if (ipl == SwissEph.SE_SUN)
ipli = SwissEph.SE_EARTH;
if (ipl == SwissEph.SE_MOON) {
do_defl = false;
if (0 == (iflag & SwissEph.SEFLG_HELCTR))
do_aberr = false;
}
iflg0 = (iflag & (SEFLG_EPHMASK | SwissEph.SEFLG_NONUT)) | SwissEph.SEFLG_SPEED | SwissEph.SEFLG_TRUEPOS;
if (ipli != SwissEph.SE_MOON)
iflg0 |= SwissEph.SEFLG_HELCTR;
if (ipl == SwissEph.SE_MEAN_NODE || ipl == SwissEph.SE_TRUE_NODE ||
ipl == SwissEph.SE_MEAN_APOG || ipl == SwissEph.SE_OSCU_APOG ||
ipl < 0 ||
(ipl >= SwissEph.SE_NPLANETS && ipl <= SwissEph.SE_AST_OFFSET)) {
/*(ipl >= SE_FICT_OFFSET && ipl - SE_FICT_OFFSET < SE_NFICT_ELEM)) */
serr = C.sprintf("nodes/apsides for planet %5.0f are not implemented", (double)ipl);
if (xnasc != null)
for (i = 0; i <= 5; i++)
xnasc[i] = 0;
if (xndsc != null)
for (i = 0; i <= 5; i++)
xndsc[i] = 0;
if (xaphe != null)
for (i = 0; i <= 5; i++)
xaphe[i] = 0;
if (xperi != null)
for (i = 0; i <= 5; i++)
xperi[i] = 0;
return SwissEph.ERR;
}
for (i = 0; i < 24; i++)
xx[i] = 0;
/***************************************
* mean nodes and apsides
***************************************/
/* mean points only for Sun - Neptune */
if ((method == 0 || (method & SwissEph.SE_NODBIT_MEAN) != 0) &&
((ipl >= SwissEph.SE_SUN && ipl <= SwissEph.SE_NEPTUNE) || ipl == SwissEph.SE_EARTH)) {
if (ipl == SwissEph.SE_MOON) {
double[] xdummy = new double[] { xna[0], xna[3], xpe[0], xpe[3] };
SE.SwemMoon.swi_mean_lunar_elements(tjd_et, ref xdummy[0], ref xdummy[1], ref xdummy[2], ref xdummy[3]);
xna[0] = xdummy[0]; xna[3] = xdummy[1]; xpe[0] = xdummy[2]; xpe[3] = xdummy[3];
incl = Sweph.MOON_MEAN_INCL;
vincl = 0;
ecce = Sweph.MOON_MEAN_ECC;
vecce = 0;
sema = Sweph.MOON_MEAN_DIST / Sweph.AUNIT;
vsema = 0;
} else {
iplx = ipl_to_elem[ipl];
ep = el_incl[iplx];
incl = ep[0] + ep[1] * t + ep[2] * t * t + ep[3] * t * t * t;
vincl = ep[1] / 36525;
ep = el_sema[iplx];
sema = ep[0] + ep[1] * t + ep[2] * t * t + ep[3] * t * t * t;
vsema = ep[1] / 36525;
ep = el_ecce[iplx];
ecce = ep[0] + ep[1] * t + ep[2] * t * t + ep[3] * t * t * t;
vecce = ep[1] / 36525;
ep = el_node[iplx];
/* ascending node */
xna[0] = ep[0] + ep[1] * t + ep[2] * t * t + ep[3] * t * t * t;
xna[3] = ep[1] / 36525;
/* perihelion */
ep = el_peri[iplx];
xpe[0] = ep[0] + ep[1] * t + ep[2] * t * t + ep[3] * t * t * t;
xpe[3] = ep[1] / 36525;
}
/* descending node */
xnd[0] = SE.swe_degnorm(xna[0] + 180);
xnd[3] = xna[3];
/* angular distance of perihelion from node */
parg = xpe[0] = SE.swe_degnorm(xpe[0] - xna[0]);
pargx = xpe[3] = SE.swe_degnorm(xpe[0] + xpe[3] - xna[3]);
/* transform from orbital plane to mean ecliptic of date */
SE.swe_cotrans(xpe, xpe, -incl);
/* xpe+3 is aux. position, not speed!!! */
SE.swe_cotrans(xpe + 3, xpe + 3, -incl - vincl);
/* add node again */
xpe[0] = SE.swe_degnorm(xpe[0] + xna[0]);
/* xpe+3 is aux. position, not speed!!! */
xpe[3] = SE.swe_degnorm(xpe[3] + xna[0] + xna[3]);
/* speed */
xpe[3] = SE.swe_degnorm(xpe[3] - xpe[0]);
/* heliocentric distance of perihelion and aphelion */
xpe[2] = sema * (1 - ecce);
xpe[5] = (sema + vsema) * (1 - ecce - vecce) - xpe[2];
/* aphelion */
xap[0] = SE.swe_degnorm(xpe[0] + 180);
xap[1] = -xpe[1];
xap[3] = xpe[3];
xap[4] = -xpe[4];
if (do_focal_point) {
xap[2] = sema * ecce * 2;
xap[5] = (sema + vsema) * (ecce + vecce) * 2 - xap[2];
} else {
xap[2] = sema * (1 + ecce);
xap[5] = (sema + vsema) * (1 + ecce + vecce) - xap[2];
}
/* heliocentric distance of nodes */
ea = Math.Atan(Math.Tan(-parg * SwissEph.DEGTORAD / 2) * Math.Sqrt((1 - ecce) / (1 + ecce))) * 2;
eax = Math.Atan(Math.Tan(-pargx * SwissEph.DEGTORAD / 2) * Math.Sqrt((1 - ecce - vecce) / (1 + ecce + vecce))) * 2;
xna[2] = sema * (Math.Cos(ea) - ecce) / Math.Cos(parg * SwissEph.DEGTORAD);
xna[5] = (sema + vsema) * (Math.Cos(eax) - ecce - vecce) / Math.Cos(pargx * SwissEph.DEGTORAD);
xna[5] -= xna[2];
ea = Math.Atan(Math.Tan((180 - parg) * SwissEph.DEGTORAD / 2) * Math.Sqrt((1 - ecce) / (1 + ecce))) * 2;
eax = Math.Atan(Math.Tan((180 - pargx) * SwissEph.DEGTORAD / 2) * Math.Sqrt((1 - ecce - vecce) / (1 + ecce + vecce))) * 2;
xnd[2] = sema * (Math.Cos(ea) - ecce) / Math.Cos((180 - parg) * SwissEph.DEGTORAD);
xnd[5] = (sema + vsema) * (Math.Cos(eax) - ecce - vecce) / Math.Cos((180 - pargx) * SwissEph.DEGTORAD);
xnd[5] -= xnd[2];
/* no light-time correction because speed is extremely small */
for (i = 0, xp = xx; i < 4; i++, xp += 6) {
/* to cartesian coordinates */
xp[0] *= SwissEph.DEGTORAD;
xp[1] *= SwissEph.DEGTORAD;
xp[3] *= SwissEph.DEGTORAD;
xp[4] *= SwissEph.DEGTORAD;
SE.SwephLib.swi_polcart_sp(xp, xp);
}
/***************************************
* "true" or osculating nodes and apsides
***************************************/
} else {
/* first, we need a heliocentric distance of the planet */
if (SE.swe_calc(tjd_et, ipli, iflg0, x, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
iflJ2000 = (iflag & SEFLG_EPHMASK) | SwissEph.SEFLG_J2000 | SwissEph.SEFLG_EQUATORIAL | SwissEph.SEFLG_XYZ | SwissEph.SEFLG_TRUEPOS | SwissEph.SEFLG_NONUT | SwissEph.SEFLG_SPEED;
ellipse_is_bary = false;
if (ipli != SwissEph.SE_MOON) {
if ((method & SwissEph.SE_NODBIT_OSCU_BAR) != 0 && x[2] > 6) {
iflJ2000 |= SwissEph.SEFLG_BARYCTR; /* only planets beyond Jupiter */
ellipse_is_bary = true;
} else {
iflJ2000 |= SwissEph.SEFLG_HELCTR;
}
}
/* we need three positions and three speeds
* for three nodes/apsides. from the three node positions,
* the speed of the node will be computed. */
if (ipli == SwissEph.SE_MOON) {
dt = Sweph.NODE_CALC_INTV;
dzmin = 1e-15;
Gmsm = Sweph.GEOGCONST * (1 + 1 / Sweph.EARTH_MOON_MRAT) / Sweph.AUNIT / Sweph.AUNIT / Sweph.AUNIT * 86400.0 * 86400.0;
} else {
if ((ipli >= SwissEph.SE_MERCURY && ipli <= SwissEph.SE_PLUTO) || ipli == SwissEph.SE_EARTH)
plm = 1 / plmass[ipl_to_elem[ipl]];
else
plm = 0;
dt = Sweph.NODE_CALC_INTV * 10 * x[2];
dzmin = 1e-15 * dt / Sweph.NODE_CALC_INTV;
Gmsm = Sweph.HELGRAVCONST * (1 + plm) / Sweph.AUNIT / Sweph.AUNIT / Sweph.AUNIT * 86400.0 * 86400.0;
}
if ((iflag & SwissEph.SEFLG_SPEED) != 0) {
istart = 0;
iend = 2;
} else {
istart = iend = 0;
dt = 0;
}
for (i = istart, t = tjd_et - dt; i <= iend; i++, t += dt) {
if (istart == iend)
t = tjd_et;
if (SE.swe_calc(t, ipli, iflJ2000, xpos[i], ref serr) == SwissEph.ERR)
return SwissEph.ERR;
/* the EMB is used instead of the earth */
if (ipli == SwissEph.SE_EARTH) {
if (SE.swe_calc(t, SwissEph.SE_MOON, iflJ2000 & ~(SwissEph.SEFLG_BARYCTR | SwissEph.SEFLG_HELCTR), xposm, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
for (j = 0; j <= 2; j++)
xpos[i][j] += xposm[j] / (Sweph.EARTH_MOON_MRAT + 1.0);
}
SE.Sweph.swi_plan_for_osc_elem(iflg0, t, xpos[i]);
}
for (i = istart; i <= iend; i++) {
if (Math.Abs(xpos[i][5]) < dzmin)
xpos[i][5] = dzmin;
fac = xpos[i][2] / xpos[i][5];
sgn = xpos[i][5] / Math.Abs(xpos[i][5]);
for (j = 0; j <= 2; j++) {
xn[i][j] = (xpos[i][j] - fac * xpos[i][j + 3]) * sgn;
xs[i][j] = -xn[i][j];
}
}
for (i = istart; i <= iend; i++) {
/* node */
rxy = Math.Sqrt(xn[i][0] * xn[i][0] + xn[i][1] * xn[i][1]);
cosnode = xn[i][0] / rxy;
sinnode = xn[i][1] / rxy;
/* inclination */
SE.SwephLib.swi_cross_prod(xpos[i], xpos[i].GetPointer(3), xnorm);
rxy = xnorm[0] * xnorm[0] + xnorm[1] * xnorm[1];
c2 = (rxy + xnorm[2] * xnorm[2]);
rxyz = Math.Sqrt(c2);
rxy = Math.Sqrt(rxy);
sinincl = rxy / rxyz;
cosincl = Math.Sqrt(1 - sinincl * sinincl);
if (xnorm[2] < 0) cosincl = -cosincl; /* retrograde asteroid, e.g. 20461 Dioretsa */
/* argument of latitude */
cosu = xpos[i][0] * cosnode + xpos[i][1] * sinnode;
sinu = xpos[i][2] / sinincl;
uu = Math.Atan2(sinu, cosu);
/* semi-axis */
rxyz = Math.Sqrt(SE.Sweph.square_sum(xpos[i]));
v2 = SE.Sweph.square_sum((xpos[i].GetPointer(3)));
sema = 1 / (2 / rxyz - v2 / Gmsm);
/* eccentricity */
pp = c2 / Gmsm;
ecce = Math.Sqrt(1 - pp / sema);
/* eccentric anomaly */
cosE = 1 / ecce * (1 - rxyz / sema);
sinE = 1 / ecce / Math.Sqrt(sema * Gmsm) * SE.Sweph.dot_prod(xpos[i], (xpos[i].GetPointer(3)));
/* true anomaly */
ny = 2 * Math.Atan(Math.Sqrt((1 + ecce) / (1 - ecce)) * sinE / (1 + cosE));
/* distance of perihelion from ascending node */
xq[i][0] = SE.SwephLib.swi_mod2PI(uu - ny);
xq[i][1] = 0; /* latitude */
xq[i][2] = sema * (1 - ecce); /* distance of perihelion */
/* transformation to ecliptic coordinates */
SE.SwephLib.swi_polcart(xq[i], xq[i]);
SE.SwephLib.swi_coortrf2(xq[i], xq[i], -sinincl, cosincl);
SE.SwephLib.swi_cartpol(xq[i], xq[i]);
/* adding node, we get perihelion in ecl. coord. */
xq[i][0] += Math.Atan2(sinnode, cosnode);
xa[i][0] = SE.SwephLib.swi_mod2PI(xq[i][0] + Math.PI);
xa[i][1] = -xq[i][1];
if (do_focal_point) {
xa[i][2] = sema * ecce * 2; /* distance of aphelion */
} else {
xa[i][2] = sema * (1 + ecce); /* distance of aphelion */
}
SE.SwephLib.swi_polcart(xq[i], xq[i]);
SE.SwephLib.swi_polcart(xa[i], xa[i]);
/* new distance of node from orbital ellipse:
* true anomaly of node: */
ny = SE.SwephLib.swi_mod2PI(ny - uu);
ny2 = SE.SwephLib.swi_mod2PI(ny + Math.PI);
/* eccentric anomaly */
cosE = Math.Cos(2 * Math.Atan(Math.Tan(ny / 2) / Math.Sqrt((1 + ecce) / (1 - ecce))));
cosE2 = Math.Cos(2 * Math.Atan(Math.Tan(ny2 / 2) / Math.Sqrt((1 + ecce) / (1 - ecce))));
/* new distance */
rn = sema * (1 - ecce * cosE);
rn2 = sema * (1 - ecce * cosE2);
/* old node distance */
ro = Math.Sqrt(SE.Sweph.square_sum(xn[i]));
ro2 = Math.Sqrt(SE.Sweph.square_sum(xs[i]));
/* correct length of position vector */
for (j = 0; j <= 2; j++) {
xn[i][j] *= rn / ro;
xs[i][j] *= rn2 / ro2;
}
}
for (i = 0; i <= 2; i++) {
if ((iflag & SwissEph.SEFLG_SPEED) != 0) {
xpe[i] = xq[1][i];
xpe[i + 3] = (xq[2][i] - xq[0][i]) / dt / 2;
xap[i] = xa[1][i];
xap[i + 3] = (xa[2][i] - xa[0][i]) / dt / 2;
xna[i] = xn[1][i];
xna[i + 3] = (xn[2][i] - xn[0][i]) / dt / 2;
xnd[i] = xs[1][i];
xnd[i + 3] = (xs[2][i] - xs[0][i]) / dt / 2;
} else {
xpe[i] = xq[0][i];
xpe[i + 3] = 0;
xap[i] = xa[0][i];
xap[i + 3] = 0;
xna[i] = xn[0][i];
xna[i + 3] = 0;
xnd[i] = xs[0][i];
xnd[i + 3] = 0;
}
}
is_true_nodaps = true;
}
/* to set the variables required in the save area,
* i.e. ecliptic, nutation, barycentric sun, earth
* we compute the planet */
if (ipli == SwissEph.SE_MOON && (iflag & (SwissEph.SEFLG_HELCTR | SwissEph.SEFLG_BARYCTR)) != 0) {
SE.Sweph.swi_force_app_pos_etc();
if (SE.swe_calc(tjd_et, SwissEph.SE_SUN, iflg0, x, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
} else {
if (SE.swe_calc(tjd_et, ipli, iflg0 | (iflag & SwissEph.SEFLG_TOPOCTR), x, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
}
/***********************
* position of observer
***********************/
if ((iflag & SwissEph.SEFLG_TOPOCTR) != 0) {
/* geocentric position of observer */
if (SE.Sweph.swi_get_observer(tjd_et, iflag, false, xobs, ref serr) != SwissEph.OK)
return SwissEph.ERR;
/*for (i = 0; i <= 5; i++)
xobs[i] = swed.topd.xobs[i];*/
} else {
for (i = 0; i <= 5; i++)
xobs[i] = 0;
}
if ((iflag & (SwissEph.SEFLG_HELCTR | SwissEph.SEFLG_BARYCTR)) != Sweph.B1950) {
if ((iflag & SwissEph.SEFLG_HELCTR) != 0 && 0 == (iflag & SwissEph.SEFLG_MOSEPH))
for (i = 0; i <= 5; i++)
xobs[i] = xsun[i];
} else if (ipl == SwissEph.SE_SUN && 0 == (iflag & SwissEph.SEFLG_MOSEPH)) {
for (i = 0; i <= 5; i++)
xobs[i] = xsun[i];
} else {
/* barycentric position of observer */
for (i = 0; i <= 5; i++)
xobs[i] += xear[i];
}
/* ecliptic obliqity */
if ((iflag & SwissEph.SEFLG_J2000) != 0)
oe = SE.Sweph.swed.oec2000;
else
oe = SE.Sweph.swed.oec;
/*************************************************
* conversions shared by mean and osculating points
*************************************************/
for (ij = 0, xp = xx; ij < 4; ij++, xp += 6) {
/* no nodes for earth */
if (ipli == SwissEph.SE_EARTH && ij <= 1) {
for (i = 0; i <= 5; i++)
xp[i] = 0;
continue;
}
/*********************
* to equator
*********************/
if (is_true_nodaps && 0 == (iflag & SwissEph.SEFLG_NONUT)) {
SE.SwephLib.swi_coortrf2(xp, xp, -SE.Sweph.swed.nut.snut, SE.Sweph.swed.nut.cnut);
if ((iflag & SwissEph.SEFLG_SPEED) != 0)
SE.SwephLib.swi_coortrf2(xp + 3, xp + 3, -SE.Sweph.swed.nut.snut, SE.Sweph.swed.nut.cnut);
}
SE.SwephLib.swi_coortrf2(xp, xp, -oe.seps, oe.ceps);
SE.SwephLib.swi_coortrf2(xp + 3, xp + 3, -oe.seps, oe.ceps);
if (is_true_nodaps) {
/****************************
* to mean ecliptic of date
****************************/
if (0 == (iflag & SwissEph.SEFLG_NONUT))
SE.Sweph.swi_nutate(xp, iflag, true);
}
/*********************
* to J2000
*********************/
SE.SwephLib.swi_precess(xp, tjd_et, iflag, Sweph.J_TO_J2000);
if ((iflag & SwissEph.SEFLG_SPEED) != 0)
SE.Sweph.swi_precess_speed(xp, tjd_et, iflag, Sweph.J_TO_J2000);
/*********************
* to barycenter
*********************/
if (ipli == SwissEph.SE_MOON) {
for (i = 0; i <= 5; i++)
xp[i] += xear[i];
} else {
if (0 == (iflag & SwissEph.SEFLG_MOSEPH) && !ellipse_is_bary)
for (j = 0; j <= 5; j++)
xp[j] += xsun[j];
}
/*********************
* to correct center
*********************/
for (j = 0; j <= 5; j++)
xp[j] -= xobs[j];
/* geocentric perigee/apogee of sun */
if (ipl == SwissEph.SE_SUN && 0 == (iflag & (SwissEph.SEFLG_HELCTR | SwissEph.SEFLG_BARYCTR)))
for (j = 0; j <= 5; j++)
xp[j] = -xp[j];
/*********************
* light deflection
*********************/
dt = Math.Sqrt(SE.Sweph.square_sum(xp)) * Sweph.AUNIT / Sweph.CLIGHT / 86400.0;
if (do_defl)
SE.Sweph.swi_deflect_light(xp, dt, iflag);
/*********************
* aberration
*********************/
if (do_aberr) {
SE.Sweph.swi_aberr_light(xp, xobs, iflag);
/*
* Apparent speed is also influenced by
* the difference of speed of the earth between t and t-dt.
* Neglecting this would result in an error of several 0.1"
*/
if ((iflag & SwissEph.SEFLG_SPEED) != 0) {
/* get barycentric sun and earth for t-dt into save area */
if (SE.swe_calc(tjd_et - dt, ipli, iflg0 | (iflag & SwissEph.SEFLG_TOPOCTR), x2, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
if ((iflag & SwissEph.SEFLG_TOPOCTR) != 0) {
/* geocentric position of observer */
/* if (swi_get_observer(tjd_et - dt, iflag, FALSE, xobs, serr) != OK)
return ERR;*/
for (i = 0; i <= 5; i++)
xobs2[i] = SE.Sweph.swed.topd.xobs[i];
} else {
for (i = 0; i <= 5; i++)
xobs2[i] = 0;
}
if ((iflag & (SwissEph.SEFLG_HELCTR | SwissEph.SEFLG_BARYCTR)) != 0) {
if ((iflag & SwissEph.SEFLG_HELCTR) != 0 && 0 == (iflag & SwissEph.SEFLG_MOSEPH))
for (i = 0; i <= 5; i++)
xobs2[i] = xsun[i];
} else if (ipl == SwissEph.SE_SUN && 0 == (iflag & SwissEph.SEFLG_MOSEPH)) {
for (i = 0; i <= 5; i++)
xobs2[i] = xsun[i];
} else {
/* barycentric position of observer */
for (i = 0; i <= 5; i++)
xobs2[i] += xear[i];
}
for (i = 3; i <= 5; i++)
xp[i] += xobs[i] - xobs2[i];
/* The above call of swe_calc() has destroyed the
* parts of the save area
* (i.e. bary sun, earth nutation matrix!).
* to restore it:
*/
if (SE.swe_calc(tjd_et, SwissEph.SE_SUN, iflg0 | (iflag & SwissEph.SEFLG_TOPOCTR), x2, ref serr) == SwissEph.ERR)
return SwissEph.ERR;
}
}
/*********************
* precession
*********************/
/* save J2000 coordinates; required for sidereal positions */
for (j = 0; j <= 5; j++)
x2000[j] = xp[j];
if (0 == (iflag & SwissEph.SEFLG_J2000)) {
SE.SwephLib.swi_precess(xp, tjd_et, iflag, Sweph.J2000_TO_J);
if ((iflag & SwissEph.SEFLG_SPEED) != 0)
SE.Sweph.swi_precess_speed(xp, tjd_et, iflag, Sweph.J2000_TO_J);
}
/*********************
* nutation
*********************/
if (0 == (iflag & SwissEph.SEFLG_NONUT))
SE.Sweph.swi_nutate(xp, iflag, false);
/* now we have equatorial cartesian coordinates; keep them */
for (j = 0; j <= 5; j++)
pldat.xreturn[18 + j] = xp[j];
/************************************************
* transformation to ecliptic. *
* with sidereal calc. this will be overwritten *
* afterwards. *
************************************************/
SE.SwephLib.swi_coortrf2(xp, xp, oe.seps, oe.ceps);
if ((iflag & SwissEph.SEFLG_SPEED) != 0)
SE.SwephLib.swi_coortrf2(xp + 3, xp + 3, oe.seps, oe.ceps);
if (0 == (iflag & SwissEph.SEFLG_NONUT)) {
SE.SwephLib.swi_coortrf2(xp, xp, SE.Sweph.swed.nut.snut, SE.Sweph.swed.nut.cnut);
if ((iflag & SwissEph.SEFLG_SPEED) != 0)
SE.SwephLib.swi_coortrf2(xp + 3, xp + 3, SE.Sweph.swed.nut.snut, SE.Sweph.swed.nut.cnut);
}
/* now we have ecliptic cartesian coordinates */
for (j = 0; j <= 5; j++)
pldat.xreturn[6 + j] = xp[j];
/************************************
* sidereal positions *
************************************/
if ((iflag & SwissEph.SEFLG_SIDEREAL) != 0) {
/* project onto ecliptic t0 */
if ((SE.Sweph.swed.sidd.sid_mode & SwissEph.SE_SIDBIT_ECL_T0) != 0) {
if (SE.Sweph.swi_trop_ra2sid_lon(x2000, pldat.xreturn.GetPointer(6), pldat.xreturn.GetPointer(18), iflag, ref serr) != SwissEph.OK)
return SwissEph.ERR;
/* project onto solar system equator */
} else if ((SE.Sweph.swed.sidd.sid_mode & SwissEph.SE_SIDBIT_SSY_PLANE) != 0) {
if (SE.Sweph.swi_trop_ra2sid_lon_sosy(x2000, pldat.xreturn.GetPointer(6), pldat.xreturn.GetPointer(18), iflag, ref serr) != SwissEph.OK)
return SwissEph.ERR;
} else {
/* traditional algorithm */
SE.SwephLib.swi_cartpol_sp(pldat.xreturn.GetPointer(6), pldat.xreturn);
pldat.xreturn[0] -= SE.swe_get_ayanamsa(tjd_et) * SwissEph.DEGTORAD;
SE.SwephLib.swi_polcart_sp(pldat.xreturn, pldat.xreturn.GetPointer(6));
}
}
if ((iflag & SwissEph.SEFLG_XYZ) != 0 && (iflag & SwissEph.SEFLG_EQUATORIAL) != 0) {
for (j = 0; j <= 5; j++)
xp[j] = pldat.xreturn[18 + j];
continue;
}
if ((iflag & SwissEph.SEFLG_XYZ) != 0) {
for (j = 0; j <= 5; j++)
xp[j] = pldat.xreturn[6 + j];
continue;
}
/************************************************
* transformation to polar coordinates *
************************************************/
SE.SwephLib.swi_cartpol_sp(pldat.xreturn.GetPointer(18), pldat.xreturn.GetPointer(12));
SE.SwephLib.swi_cartpol_sp(pldat.xreturn.GetPointer(6), pldat.xreturn);
/**********************
* radians to degrees *
**********************/
if ((iflag & SwissEph.SEFLG_RADIANS) == 0)
{
for (j = 0; j < 2; j++)
{
pldat.xreturn[j] *= SwissEph.RADTODEG; /* ecliptic */
pldat.xreturn[j + 3] *= SwissEph.RADTODEG;
pldat.xreturn[j + 12] *= SwissEph.RADTODEG; /* equator */
pldat.xreturn[j + 15] *= SwissEph.RADTODEG;
}
}
if ((iflag & SwissEph.SEFLG_EQUATORIAL) != 0) {
for (j = 0; j <= 5; j++)
xp[j] = pldat.xreturn[12 + j];
continue;
} else {
for (j = 0; j <= 5; j++)
xp[j] = pldat.xreturn[j];
continue;
}
}
for (i = 0; i <= 5; i++) {
if (i > 2 && 0 == (iflag & SwissEph.SEFLG_SPEED))
xna[i] = xnd[i] = xpe[i] = xap[i] = 0;
if (xnasc != null)
xnasc[i] = xna[i];
if (xndsc != null)
xndsc[i] = xnd[i];
if (xperi != null)
xperi[i] = xpe[i];
if (xaphe != null)
xaphe[i] = xap[i];
}
return SwissEph.OK;
}
/* Moshier ephemeris.
* computes heliocentric cartesian equatorial coordinates of
* equinox 2000
* for earth and a planet
* tjd julian day
* ipli internal SWEPH planet number
* xp array of 6 doubles for planet's position and speed
* xe earth's
* serr error string
*/
public int swi_moshplan(double tjd, int ipli, bool do_save, CPointer <double> xpret, CPointer <double> xeret, ref string serr)
{
int i;
bool do_earth = false;
double[] dx = new double[3], x2 = new double[3], xxe = new double[6], xxp = new double[6];
double[] xp, xe;
double dt;
string s = String.Empty;
int iplm = pnoint2msh[ipli];
Sweph.plan_data pdp = SE.Sweph.swed.pldat[ipli];
Sweph.plan_data pedp = SE.Sweph.swed.pldat[Sweph.SEI_EARTH];
double seps2000 = SE.Sweph.swed.oec2000.seps;
double ceps2000 = SE.Sweph.swed.oec2000.ceps;
if (do_save)
{
xp = pdp.x;
xe = pedp.x;
}
else
{
xp = xxp;
xe = xxe;
}
if (do_save || ipli == Sweph.SEI_EARTH || xeret != null)
{
do_earth = true;
}
/* tjd beyond ephemeris limits, give some margin for spped at edge */
if (tjd < Sweph.MOSHPLEPH_START - 0.3 || tjd > Sweph.MOSHPLEPH_END + 0.3)
{
s = C.sprintf("jd %f outside Moshier planet range %.2f .. %.2f ",
tjd, Sweph.MOSHPLEPH_START, Sweph.MOSHPLEPH_END);
serr = (serr ?? String.Empty) + s;
return(SwissEph.ERR);
}
/* earth, for geocentric position */
if (do_earth)
{
if (tjd == pedp.teval &&
pedp.iephe == SwissEph.SEFLG_MOSEPH)
{
xe = pedp.x;
}
else
{
/* emb */
swi_moshplan2(tjd, pnoint2msh[Sweph.SEI_EMB], xe); /* emb hel. ecl. 2000 polar */
SE.SwephLib.swi_polcart(xe, xe); /* to cartesian */
SE.SwephLib.swi_coortrf2(xe, xe, -seps2000, ceps2000); /* and equator 2000 */
embofs_mosh(tjd, xe); /* emb -> earth */
if (do_save)
{
pedp.teval = tjd;
pedp.xflgs = -1;
pedp.iephe = SwissEph.SEFLG_MOSEPH;
}
/* one more position for speed. */
swi_moshplan2(tjd - Sweph.PLAN_SPEED_INTV, pnoint2msh[Sweph.SEI_EMB], x2);
SE.SwephLib.swi_polcart(x2, x2);
SE.SwephLib.swi_coortrf2(x2, x2, -seps2000, ceps2000);
embofs_mosh(tjd - Sweph.PLAN_SPEED_INTV, x2);/**/
for (i = 0; i <= 2; i++)
{
dx[i] = (xe[i] - x2[i]) / Sweph.PLAN_SPEED_INTV;
}
/* store speed */
for (i = 0; i <= 2; i++)
{
xe[i + 3] = dx[i];
}
}
if (xeret != null)
{
for (i = 0; i <= 5; i++)
{
xeret[i] = xe[i];
}
}
}
/* earth is the planet wanted */
if (ipli == Sweph.SEI_EARTH)
{
xp = xe;
}
else
{
/* other planet */
/* if planet has already been computed, return */
if (tjd == pdp.teval && pdp.iephe == SwissEph.SEFLG_MOSEPH)
{
xp = pdp.x;
}
else
{
swi_moshplan2(tjd, iplm, xp);
SE.SwephLib.swi_polcart(xp, xp);
SE.SwephLib.swi_coortrf2(xp, xp, -seps2000, ceps2000);
if (do_save)
{
pdp.teval = tjd;/**/
pdp.xflgs = -1;
pdp.iephe = SwissEph.SEFLG_MOSEPH;
}
/* one more position for speed.
* the following dt gives good speed for light-time correction
*/
//#if 0
// for (i = 0; i <= 2; i++)
//dx[i] = xp[i] - pedp.x[i];
// dt = LIGHTTIME_AUNIT * Math.Sqrt(square_sum(dx));
//#endif
dt = Sweph.PLAN_SPEED_INTV;
swi_moshplan2(tjd - dt, iplm, x2);
SE.SwephLib.swi_polcart(x2, x2);
SE.SwephLib.swi_coortrf2(x2, x2, -seps2000, ceps2000);
for (i = 0; i <= 2; i++)
{
dx[i] = (xp[i] - x2[i]) / dt;
}
/* store speed */
for (i = 0; i <= 2; i++)
{
xp[i + 3] = dx[i];
}
}
if (xpret != null)
{
for (i = 0; i <= 5; i++)
{
xpret[i] = xp[i];
}
}
}
return(SwissEph.OK);
}
/* Prepare lookup table of sin and cos ( i*Lj )
* for required multiple angles
*/
void plan_sscc(int k, double arg, int n)
{
double cu, su, cv, sv, s;
int i;
su = Math.Sin(arg);
cu = Math.Cos(arg);
plan_ss[k, 0] = su; /* sin(L) */
plan_cc[k, 0] = cu; /* cos(L) */
sv = 2.0 * su * cu;
cv = cu * cu - su * su;
plan_ss[k, 1] = sv; /* sin(2L) */
plan_cc[k, 1] = cv;
for (i = 2; i < n; i++)
{
s = su * cv + cu * sv;
cv = cu * cv - su * sv;
sv = s;
plan_ss[k, i] = sv; /* sin( i+1 L ) */
plan_cc[k, i] = cv;
}
}
/* Adjust position from Earth-Moon barycenter to Earth
*
* J = Julian day number
* xemb = rectangular equatorial coordinates of Earth
*/
void embofs_mosh(double tjd, CPointer <double> xemb)
{
double T, M, a, L, B, p;
double smp, cmp, s2mp, c2mp, s2d, c2d, sf, cf;
double s2f, sx, cx; double[] xyz = new double[6];
double seps = SE.Sweph.swed.oec.seps;
double ceps = SE.Sweph.swed.oec.ceps;
int i;
/* Short series for position of the Moon
*/
T = (tjd - Sweph.J1900) / 36525.0;
/* Mean anomaly of moon (MP) */
a = SE.swe_degnorm(((1.44e-5 * T + 0.009192) * T + 477198.8491) * T + 296.104608);
a *= SwissEph.DEGTORAD;
smp = Math.Sin(a);
cmp = Math.Cos(a);
s2mp = 2.0 * smp * cmp; /* sin(2MP) */
c2mp = cmp * cmp - smp * smp; /* cos(2MP) */
/* Mean elongation of moon (D) */
a = SE.swe_degnorm(((1.9e-6 * T - 0.001436) * T + 445267.1142) * T + 350.737486);
a = 2.0 * SwissEph.DEGTORAD * a;
s2d = Math.Sin(a);
c2d = Math.Cos(a);
/* Mean distance of moon from its ascending node (F) */
a = SE.swe_degnorm(((-3.0e-7 * T - 0.003211) * T + 483202.0251) * T + 11.250889);
a *= SwissEph.DEGTORAD;
sf = Math.Sin(a);
cf = Math.Cos(a);
s2f = 2.0 * sf * cf; /* sin(2F) */
sx = s2d * cmp - c2d * smp; /* sin(2D - MP) */
cx = c2d * cmp + s2d * smp; /* cos(2D - MP) */
/* Mean longitude of moon (LP) */
L = ((1.9e-6 * T - 0.001133) * T + 481267.8831) * T + 270.434164;
/* Mean anomaly of sun (M) */
M = SE.swe_degnorm(((-3.3e-6 * T - 1.50e-4) * T + 35999.0498) * T + 358.475833);
/* Ecliptic longitude of the moon */
L = L
+ 6.288750 * smp
+ 1.274018 * sx
+ 0.658309 * s2d
+ 0.213616 * s2mp
- 0.185596 * Math.Sin(SwissEph.DEGTORAD * M)
- 0.114336 * s2f;
/* Ecliptic latitude of the moon */
a = smp * cf;
sx = cmp * sf;
B = 5.128189 * sf
+ 0.280606 * (a + sx) /* sin(MP+F) */
+ 0.277693 * (a - sx) /* sin(MP-F) */
+ 0.173238 * (s2d * cf - c2d * sf); /* sin(2D-F) */
B *= SwissEph.DEGTORAD;
/* Parallax of the moon */
p = 0.950724
+ 0.051818 * cmp
+ 0.009531 * cx
+ 0.007843 * c2d
+ 0.002824 * c2mp;
p *= SwissEph.DEGTORAD;
/* Elongation of Moon from Sun
*/
L = SE.swe_degnorm(L);
L *= SwissEph.DEGTORAD;
/* Distance in au */
a = 4.263523e-5 / Math.Sin(p);
/* Convert to rectangular ecliptic coordinates */
xyz[0] = L;
xyz[1] = B;
xyz[2] = a;
SE.SwephLib.swi_polcart(xyz, xyz);
/* Convert to equatorial */
SE.SwephLib.swi_coortrf2(xyz, xyz, -seps, ceps);
/* Precess to equinox of J2000.0 */
SE.SwephLib.swi_precess(xyz, tjd, 0, Sweph.J_TO_J2000);/**/
/* now emb -> earth */
for (i = 0; i <= 2; i++)
{
xemb[i] -= xyz[i] / (Sweph.EARTH_MOON_MRAT + 1.0);
}
}