Example #1
0
        public EclipticCoords ToEclipticSpherical()
        {
            var ecl = new EclipticCoords(
                Math.Atan2(z, Math.Sqrt(x * x + y * y)) * StarMath.rad2deg,
                Math.Atan2(y, x) * StarMath.rad2deg,
                this.Length());

            ecl.longitude = StarMath.WrapDeg(ecl.longitude);            //nesecary?
            return(ecl);
        }
Example #2
0
        public static double LocalSiderealTime(Astrobodies bodies, GeographicCoords geographicCoords, double day)
        {
            double sunL    = bodies.sun.orbitalElements.L;
            double gmst0   = StarMath.WrapDeg(sunL * StarMath.deg2hours + 12);
            double utcHour = (day % 1) * 24;
            // if (debug) Debug.Log($"Topocentric - day: {astrobodies.day.ToString("0.00")}\t utcHour: {utcHour.ToString("0.00")}");
            double lonHr = geographicCoords.longitude * StarMath.deg2hours;

            return(gmst0 + utcHour + lonHr);            //local siderial time
        }
Example #3
0
        public static void UpdateElements(Astrobody body, double day)
        {
            var el = body.orbitalElements;

            el.N = StarMath.WrapDeg(body.constants.N_offset + body.constants.N_scalar * day);
            el.i = StarMath.WrapDeg(body.constants.i_offset + body.constants.i_scalar * day);
            el.w = StarMath.WrapDeg(body.constants.w_offset + body.constants.w_scalar * day);
            el.a = StarMath.WrapDeg(body.constants.a_offset + body.constants.a_scalar * day);
            el.e = StarMath.WrapDeg(body.constants.e_offset + body.constants.e_scalar * day);
            el.M = StarMath.WrapDeg(body.constants.M_offset + body.constants.M_scalar * day);
            //CALCULATE SECONDARY ELEMENTS


            el.L = StarMath.WrapDeg(el.N + el.w + el.M);

            double E0 = el.M + StarMath.rad2deg * el.e * StarMath.Sin_d(el.M) * (1 + el.e * StarMath.Cos_d(el.M));
            double E1 = 0;

            do
            {
                double temp = E0;
                E0 = E1;
                E1 = temp - (temp - StarMath.rad2deg * el.e * StarMath.Sin_d(temp) - el.M) / (1 - el.e * StarMath.Cos_d(temp));
                // console.log(`${planetType} ecc diff: ${Math.abs(E1 - E0)}`);
            }while (Math.Abs(E1 - E0) > 0.005);
            el.E = E1;

            el.x = el.a * (StarMath.Cos_d(el.E) - el.e);
            el.y = el.a * Math.Sqrt(1 - el.e * el.e) * StarMath.Sin_d(el.E);
            el.r = Math.Sqrt(el.x * el.x + el.y * el.y);
            el.v = StarMath.WrapDeg(StarMath.Atan2_d(el.y, el.x));            //is StarMath.WrapDeg nessecary? ie is negative bad?

            el.unpertubatedEclitpticCart.x =
                el.r * (StarMath.Cos_d(el.N) * StarMath.Cos_d(el.v + el.w) - StarMath.Sin_d(el.N) * StarMath.Sin_d(el.v + el.w) * StarMath.Cos_d(el.i));
            el.unpertubatedEclitpticCart.y =
                el.r * (StarMath.Sin_d(el.N) * StarMath.Cos_d(el.v + el.w) + StarMath.Cos_d(el.N) * StarMath.Sin_d(el.v + el.w) * StarMath.Cos_d(el.i));
            el.unpertubatedEclitpticCart.z =
                el.r * StarMath.Sin_d(el.v + el.w) * StarMath.Sin_d(el.i);
            // el.eclipticSphere = el.eclitpticCart.ToEcliptic();
            // el.eclipticSphere.longitude = StarMath.WrapDeg(el.eclipticSphere.longitude)//nesecary?
        }