Ejemplo n.º 1
0
        //return Ecliptic Coordinates with necessary orbital corrections
        //T - Time in Julian centuries since J2000
        Vector <double> GetMoonCoor(double T)
        {
            double Arcs = 3600.0 * 180.0 / Math.PI;

            double L_0, l, ls, F, D, dL, S, h, N;

            // Mean elements of lunar orbit
            L_0 = Astro.Frac(0.606433 + 1336.855225 * T);              // mean longitude [rev]

            l  = 2 * Math.PI * Astro.Frac(0.374897 + 1325.552410 * T); // Moon's mean anomaly
            ls = 2 * Math.PI * Astro.Frac(0.993133 + 99.997361 * T);   // Sun's mean anomaly
            D  = 2 * Math.PI * Astro.Frac(0.827361 + 1236.853086 * T); // Diff. long. Moon-Sun
            F  = 2 * Math.PI * Astro.Frac(0.259086 + 1342.227825 * T); // Dist. from ascending node


            // Perturbations in longitude and latitude
            dL = +22640 * Math.Sin(l) - 4586 * Math.Sin(l - 2 * D) + 2370 * Math.Sin(2 * D) + 769 * Math.Sin(2 * l)
                 - 668 * Math.Sin(ls) - 412 * Math.Sin(2 * F) - 212 * Math.Sin(2 * l - 2 * D) - 206 * Math.Sin(l + ls - 2 * D)
                 + 192 * Math.Sin(l + 2 * D) - 165 * Math.Sin(ls - 2 * D) - 125 * Math.Sin(D) - 110 * Math.Sin(l + ls)
                 + 148 * Math.Sin(l - ls) - 55 * Math.Sin(2 * F - 2 * D);
            S = F + (dL + 412 * Math.Sin(2 * F) + 541 * Math.Sin(ls)) / Arcs;
            h = F - 2 * D;
            N = -526 * Math.Sin(h) + 44 * Math.Sin(l + h) - 31 * Math.Sin(-l + h) - 23 * Math.Sin(ls + h)
                + 11 * Math.Sin(-ls + h) - 25 * Math.Sin(-2 * l + F) + 21 * Math.Sin(-l + F);

            // Ecliptic longitude and latitude
            Vector <double> v = new Vector <double>();

            v.X = 2 * Math.PI * Astro.Frac(L_0 + dL / 1296.0e3); // [rad]
            v.Y = (18520.0 * Math.Sin(S) + N) / Arcs;            // [rad]
            return(v);
        }
Ejemplo n.º 2
0
        //return Ecliptic Coordinates with necessary orbital corrections
        //T - Time in Julian centuries since J2000
        Vector <double> GetSunCoor(double T)
        {
            // Mean anomaly and ecliptic longitude
            double M = 2 * Math.PI * Astro.Frac(0.993133 + 99.997361 * T);
            double L = 2 * Math.PI * Astro.Frac(0.7859453 + M / (Math.PI * 2) +
                                                (6893.0 * Math.Sin(M) + 72.0 * Math.Sin(2.0 * M) + 6191.2 * T) / 1296.0e3);

            return(new Vector <double> {
                X = L, Y = 0
            });
        }
Ejemplo n.º 3
0
        int GetMoonDay(DateTime date)
        {
            double eq, eq1, eq2;
            int    monthH = date.Month;
            int    yearH  = date.Year;

            if (date.Month <= 2)
            {
                monthH += 12;
                yearH--;
            }
            eq  = Math.Floor(yearH / 100.0);
            eq1 = Math.Floor(eq / 3) + Math.Floor(eq / 4) + 6 - eq;
            eq2 = (Math.Round(Astro.Frac(yearH / eq) * 209) + monthH + eq1 + date.Day) / 30;
            return((int)(Astro.Frac(eq2) * 30 + 1));
        }