示例#1
0
        public static double EclipticLongitude(double JD)
        {
            double Ldash        = MeanLongitude(JD);
            double LdashDegrees = Ldash;

            Ldash = AASCoordinateTransformation.DegreesToRadians(Ldash);
            double D = MeanElongation(JD);

            D = AASCoordinateTransformation.DegreesToRadians(D);
            double M = AASEarth.SunMeanAnomaly(JD);

            M = AASCoordinateTransformation.DegreesToRadians(M);
            double Mdash = MeanAnomaly(JD);

            Mdash = AASCoordinateTransformation.DegreesToRadians(Mdash);
            double F = ArgumentOfLatitude(JD);

            F = AASCoordinateTransformation.DegreesToRadians(F);

            double E        = AASEarth.Eccentricity(JD);
            double Esquared = E * E;
            double T        = (JD - 2451545) / 36525;

            double A1 = AASCoordinateTransformation.MapTo0To360Range(119.75 + 131.849 * T);

            A1 = AASCoordinateTransformation.DegreesToRadians(A1);
            double A2 = AASCoordinateTransformation.MapTo0To360Range(53.09 + 479264.290 * T);

            A2 = AASCoordinateTransformation.DegreesToRadians(A2);

            int    nLCoefficients = g_MoonCoefficients1.Length;
            double SigmaL         = 0;

            for (int i = 0; i < nLCoefficients; i++)
            {
                double ThisSigma = g_MoonCoefficients2[i].A * Math.Sin(g_MoonCoefficients1[i].D * D + g_MoonCoefficients1[i].M * M +
                                                                       g_MoonCoefficients1[i].Mdash * Mdash + g_MoonCoefficients1[i].F * F);

                if ((g_MoonCoefficients1[i].M == 1) || (g_MoonCoefficients1[i].M == -1))
                {
                    ThisSigma *= E;
                }
                else if ((g_MoonCoefficients1[i].M == 2) || (g_MoonCoefficients1[i].M == -2))
                {
                    ThisSigma *= Esquared;
                }

                SigmaL += ThisSigma;
            }

            //Finally the additive terms
            SigmaL += 3958 * Math.Sin(A1);
            SigmaL += 1962 * Math.Sin(Ldash - F);
            SigmaL += 318 * Math.Sin(A2);

            //And finally apply the nutation in longitude
            double NutationInLong = AASNutation.NutationInLongitude(JD);

            return(AASCoordinateTransformation.MapTo0To360Range(LdashDegrees + SigmaL / 1000000 + NutationInLong / 3600));
        }
示例#2
0
        public static double RadiusVector(double JD)
        {
            double D = MeanElongation(JD);

            D = AASCoordinateTransformation.DegreesToRadians(D);
            double M = AASEarth.SunMeanAnomaly(JD);

            M = AASCoordinateTransformation.DegreesToRadians(M);
            double Mdash = MeanAnomaly(JD);

            Mdash = AASCoordinateTransformation.DegreesToRadians(Mdash);
            double F = ArgumentOfLatitude(JD);

            F = AASCoordinateTransformation.DegreesToRadians(F);
            double E = AASEarth.Eccentricity(JD);

            int    nRCoefficients = g_MoonCoefficients1.Length;
            double SigmaR         = 0;

            for (int i = 0; i < nRCoefficients; i++)
            {
                double ThisSigma = g_MoonCoefficients2[i].B * Math.Cos(g_MoonCoefficients1[i].D * D + g_MoonCoefficients1[i].M * M + g_MoonCoefficients1[i].Mdash * Mdash + g_MoonCoefficients1[i].F * F);
                if (g_MoonCoefficients1[i].M == 1)
                {
                    // in the C++, this was "if (g_MoonCoefficients1[i].M)", because 0 and 1 are used to represent false and true in C++
                    ThisSigma *= E;
                }

                SigmaR += ThisSigma;
            }

            return(385000.56 + SigmaR / 1000);
        }
示例#3
0
        public static double EclipticLatitude(double JD)
        {
            double Ldash = MeanLongitude(JD);

            Ldash = AASCoordinateTransformation.DegreesToRadians(Ldash);
            double D = MeanElongation(JD);

            D = AASCoordinateTransformation.DegreesToRadians(D);
            double M = AASEarth.SunMeanAnomaly(JD);

            M = AASCoordinateTransformation.DegreesToRadians(M);
            double Mdash = MeanAnomaly(JD);

            Mdash = AASCoordinateTransformation.DegreesToRadians(Mdash);
            double F = ArgumentOfLatitude(JD);

            F = AASCoordinateTransformation.DegreesToRadians(F);

            double E        = AASEarth.Eccentricity(JD);
            double Esquared = E * E;
            double T        = (JD - 2451545) / 36525;

            double A1 = AASCoordinateTransformation.MapTo0To360Range(119.75 + 131.849 * T);

            A1 = AASCoordinateTransformation.DegreesToRadians(A1);
            double A3 = AASCoordinateTransformation.MapTo0To360Range(313.45 + 481266.484 * T);

            A3 = AASCoordinateTransformation.DegreesToRadians(A3);

            int    nBCoefficients = g_MoonCoefficients3.Length;
            double SigmaB         = 0;

            for (int i = 0; i < nBCoefficients; i++)
            {
                double ThisSigma = g_MoonCoefficients4[i] * Math.Sin(g_MoonCoefficients3[i].D * D + g_MoonCoefficients3[i].M * M +
                                                                     g_MoonCoefficients3[i].Mdash * Mdash + g_MoonCoefficients3[i].F * F);

                if ((g_MoonCoefficients3[i].M == 1) || (g_MoonCoefficients3[i].M == -1))
                {
                    ThisSigma *= E;
                }
                else if ((g_MoonCoefficients3[i].M == 2) || (g_MoonCoefficients3[i].M == -2))
                {
                    ThisSigma *= Esquared;
                }

                SigmaB += ThisSigma;
            }

            //Finally the additive terms
            SigmaB -= 2235 * Math.Sin(Ldash);
            SigmaB += 382 * Math.Sin(A3);
            SigmaB += 175 * Math.Sin(A1 - F);
            SigmaB += 175 * Math.Sin(A1 + F);
            SigmaB += 127 * Math.Sin(Ldash - Mdash);
            SigmaB -= 115 * Math.Sin(Ldash + Mdash);

            return(SigmaB / 1000000);
        }
示例#4
0
        public static double RadiusVector(double JD)
        {
            double D = MeanElongation(JD);

            D = AASCoordinateTransformation.DegreesToRadians(D);
            double M = AASEarth.SunMeanAnomaly(JD);

            M = AASCoordinateTransformation.DegreesToRadians(M);
            double Mdash = MeanAnomaly(JD);

            Mdash = AASCoordinateTransformation.DegreesToRadians(Mdash);
            double F = ArgumentOfLatitude(JD);

            F = AASCoordinateTransformation.DegreesToRadians(F);
            double E        = AASEarth.Eccentricity(JD);
            double Esquared = E * E;

            int    nRCoefficients = g_MoonCoefficients1.Length;
            double SigmaR         = 0;

            for (int i = 0; i < nRCoefficients; i++)
            {
                double ThisSigma = g_MoonCoefficients2[i].B * Math.Cos(g_MoonCoefficients1[i].D * D + g_MoonCoefficients1[i].M * M +
                                                                       g_MoonCoefficients1[i].Mdash * Mdash + g_MoonCoefficients1[i].F * F);
                if ((g_MoonCoefficients1[i].M == 1) || (g_MoonCoefficients1[i].M == -1))
                {
                    ThisSigma *= E;
                }
                else if ((g_MoonCoefficients1[i].M == 2) || (g_MoonCoefficients1[i].M == -2))
                {
                    ThisSigma *= Esquared;
                }

                SigmaR += ThisSigma;
            }

            return(385000.56 + SigmaR / 1000);
        }
示例#5
0
        public static void CalculateOpticalLibration(double JD, double Lambda, double Beta, ref double ldash, ref double bdash, ref double ldash2, ref double bdash2, ref double epsilon, ref double omega, ref double DeltaU, ref double sigma, ref double I, ref double rho)
        {
            //Calculate the initial quantities
            double Lambdarad = AASCoordinateTransformation.DegreesToRadians(Lambda);
            double Betarad   = AASCoordinateTransformation.DegreesToRadians(Beta);

            I      = AASCoordinateTransformation.DegreesToRadians(1.54242);
            DeltaU = AASCoordinateTransformation.DegreesToRadians(AASNutation.NutationInLongitude(JD) / 3600);
            double F = AASCoordinateTransformation.DegreesToRadians(AASMoon.ArgumentOfLatitude(JD));

            omega   = AASCoordinateTransformation.DegreesToRadians(AASMoon.MeanLongitudeAscendingNode(JD));
            epsilon = AASNutation.MeanObliquityOfEcliptic(JD) + AASNutation.NutationInObliquity(JD) / 3600;

            //Calculate the optical librations
            double W = Lambdarad - DeltaU / 3600 - omega;
            double A = Math.Atan2(Math.Sin(W) * Math.Cos(Betarad) * Math.Cos(I) - Math.Sin(Betarad) * Math.Sin(I), Math.Cos(W) * Math.Cos(Betarad));

            ldash = AASCoordinateTransformation.MapTo0To360Range(AASCoordinateTransformation.RadiansToDegrees(A) - AASCoordinateTransformation.RadiansToDegrees(F));
            if (ldash > 180)
            {
                ldash -= 360;
            }
            bdash = Math.Asin(-Math.Sin(W) * Math.Cos(Betarad) * Math.Sin(I) - Math.Sin(Betarad) * Math.Cos(I));

            //Calculate the physical librations
            double T  = (JD - 2451545.0) / 36525;
            double K1 = 119.75 + 131.849 * T;

            K1 = AASCoordinateTransformation.DegreesToRadians(K1);
            double K2 = 72.56 + 20.186 * T;

            K2 = AASCoordinateTransformation.DegreesToRadians(K2);

            double M = AASEarth.SunMeanAnomaly(JD);

            M = AASCoordinateTransformation.DegreesToRadians(M);
            double Mdash = AASMoon.MeanAnomaly(JD);

            Mdash = AASCoordinateTransformation.DegreesToRadians(Mdash);
            double D = AASMoon.MeanElongation(JD);

            D = AASCoordinateTransformation.DegreesToRadians(D);
            double E = AASEarth.Eccentricity(JD);

            rho = -0.02752 * Math.Cos(Mdash) +
                  -0.02245 * Math.Sin(F) +
                  0.00684 * Math.Cos(Mdash - 2 * F) +
                  -0.00293 * Math.Cos(2 * F) +
                  -0.00085 * Math.Cos(2 * F - 2 * D) +
                  -0.00054 * Math.Cos(Mdash - 2 * D) +
                  -0.00020 * Math.Sin(Mdash + F) +
                  -0.00020 * Math.Cos(Mdash + 2 * F) +
                  -0.00020 * Math.Cos(Mdash - F) +
                  0.00014 * Math.Cos(Mdash + 2 * F - 2 * D);

            sigma = -0.02816 * Math.Sin(Mdash) +
                    0.02244 * Math.Cos(F) +
                    -0.00682 * Math.Sin(Mdash - 2 * F) +
                    -0.00279 * Math.Sin(2 * F) +
                    -0.00083 * Math.Sin(2 * F - 2 * D) +
                    0.00069 * Math.Sin(Mdash - 2 * D) +
                    0.00040 * Math.Cos(Mdash + F) +
                    -0.00025 * Math.Sin(2 * Mdash) +
                    -0.00023 * Math.Sin(Mdash + 2 * F) +
                    0.00020 * Math.Cos(Mdash - F) +
                    0.00019 * Math.Sin(Mdash - F) +
                    0.00013 * Math.Sin(Mdash + 2 * F - 2 * D) +
                    -0.00010 * Math.Cos(Mdash - 3 * F);

            double tau = 0.02520 * E * Math.Sin(M) +
                         0.00473 * Math.Sin(2 * Mdash - 2 * F) +
                         -0.00467 * Math.Sin(Mdash) +
                         0.00396 * Math.Sin(K1) +
                         0.00276 * Math.Sin(2 * Mdash - 2 * D) +
                         0.00196 * Math.Sin(omega) +
                         -0.00183 * Math.Cos(Mdash - F) +
                         0.00115 * Math.Sin(Mdash - 2 * D) +
                         -0.00096 * Math.Sin(Mdash - D) +
                         0.00046 * Math.Sin(2 * F - 2 * D) +
                         -0.00039 * Math.Sin(Mdash - F) +
                         -0.00032 * Math.Sin(Mdash - M - D) +
                         0.00027 * Math.Sin(2 * Mdash - M - 2 * D) +
                         0.00023 * Math.Sin(K2) +
                         -0.00014 * Math.Sin(2 * D) +
                         0.00014 * Math.Cos(2 * Mdash - 2 * F) +
                         -0.00012 * Math.Sin(Mdash - 2 * F) +
                         -0.00012 * Math.Sin(2 * Mdash) +
                         0.00011 * Math.Sin(2 * Mdash - 2 * M - 2 * D);

            ldash2 = -tau + (rho * Math.Cos(A) + sigma * Math.Sin(A)) * Math.Tan(bdash);
            bdash  = AASCoordinateTransformation.RadiansToDegrees(bdash);
            bdash2 = sigma * Math.Cos(A) - rho * Math.Sin(A);
        }