import swisseph.*; public class Sw1 { int pl[] = { 0, 1, 2, 3, 4, 5, 6, 11,12 }; static String plNams[] = {"Sun","Moon","Budha","Sukra","Mars","Guru","Sani","Rahu","Kethu","Asc"}; public static void main(String[] p) { SwissEph sw=new SwissEph(); Sw1 sw1 = new Sw1(); double time = (1 + (44.00/60.00)) - 5.5 ; SweDate sd=new SweDate(1980,12,11,time); /*double time = (14 + (6.00/60.00)) - 5.5 ; SweDate sd=new SweDate(1900,1,1,0);*/ // In this array, the values will be returned: double[] res=new double[6]; StringBuffer sbErr=new StringBuffer(); int rc; //sw.swe_set_topo((77+(44.00/60.00)),(11+(22.00/60.00)),0.0D); sw.swe_set_sid_mode(1,0.0,0.0); double ayanamsa = sw.swe_get_ayanamsa(sd.getJulDay()); double longi = res[0]- ayanamsa; //sw.swe_set_ephe_path("d\\:\\\\AstroSoft"); System.out.print("Ayanamsa " + sw1.dms(ayanamsa)); //int iflag = 0x10102 ; int iflag = SweConst.SEFLG_SWIEPH | SweConst.SEFLG_SPEED | SweConst.SEFLG_SIDEREAL; System.out.println("IFlag: "+iflag); int planet; /* double xnasc[] = new double[12]; double xndsc[] = new double[12]; double xperi[] = new double[12]; double xaphe[] = new double[12];*/ for (planet=0;planet<9;planet++) { rc=sw.swe_calc_ut(sd.getJulDay() , sw1.pl[planet], iflag, res, sbErr); /*sw.swe_nod_aps_ut(sd.getJulDay(), sw1.pl[planet], iflag, SweConst.SE_NODBIT_MEAN, xnasc, xndsc, xperi, xaphe, sbErr) ;*/ System.out.println(plNams[planet]+" --> " + sw1.dms(res[0])+" Speed " + sw1.dms(res[3])+ " -- " ); // System.out.println(sbErr); /*for(int k=0; k < 6 ; k++){ System.out.println(" Asc " + xnasc[k]); System.out.println(" Dsc " + xndsc[k]); System.out.println(" Peri " + xperi[k]); System.out.println(" Aphe " + xaphe[k]); }*/ } double cusp[]=new double[20]; double ac[]=new double[20]; sw.swe_houses(sd.getJulDay(), 0x10000, (11+(22.00/60.00)),(77+(44.00/60)), 'O', cusp, ac); System.out.print("Sidereal Time : "); //for(int i=0;i<8;i++) System.out.print(sw1.dms(ac[2]/15)); /*for(int i=0;i<13;i++) System.out.println("cusp: "+ i + "--> " + sw1.dms(cusp[i]));*/ DblObj E = new DblObj(); int diff = sw.swe_time_equ(sd.getJulDay() + sd.getDeltaT(),E,sbErr); System.out.println("\nDiff : " + diff + " E: " + sw1.dms(E.val * 24 * -1) + sbErr); //////////////// Transit routines //////////////////// iflag = SweConst.SEFLG_TRANSIT_LONGITUDE | SweConst.SEFLG_SIDEREAL; TransitCalculator tc = new TCPlanet( sw, SweConst.SE_MOON, iflag, 300); SweDate d1 = new SweDate(2005,10,1,0.0); SweDate d2 = new SweDate(2006,11,1,0.0); double nextTransit = sw.getTransitUT(tc, d1.getJulDay(), false); System.out.println("Next Transit of moon ->" + SweDate.getDate(nextTransit)); nextTransit = sw.getTransitUT(tc, nextTransit, false); System.out.println("Next Transit of moon ->" + SweDate.getDate(nextTransit)); } private String dms(double val){ String res = new String(); if (val < 0){ val = Math.abs(val); res = res + "-"; } int deg = (int)val; //System.out.print(deg+" : "); double mindob = (val-deg)* 60; int min = (int)(mindob); int sec = (int)((mindob - min)*60); //System.out.println(min+" : "+sec); res = res + deg+" : "+min+" : "+sec; return res; } }