public static double epsiln_owen_1986(JulianDayNumber tjd)
{
int i;
double[] k = new double[10], tau = new double[10];
var(t0, icof) = get_owen_t0_icof(tjd);
double eps = 0;
tau[0] = 0;
tau[1] = (tjd - t0).Raw / 36525.0 / 40.0;
for (i = 2; i <= 9; i++)
{
tau[i] = tau[1] * tau[i - 1];
}
k[0] = 1;
k[1] = tau[1];
k[2] = 2 * tau[2] - 1;
k[3] = 4 * tau[3] - 3 * tau[1];
k[4] = 8 * tau[4] - 8 * tau[2] + 1;
k[5] = 16 * tau[5] - 20 * tau[3] + 5 * tau[1];
k[6] = 32 * tau[6] - 48 * tau[4] + 18 * tau[2] - 1;
k[7] = 64 * tau[7] - 112 * tau[5] + 56 * tau[3] - 7 * tau[1];
k[8] = 128 * tau[8] - 256 * tau[6] + 160 * tau[4] - 32 * tau[2] + 1;
k[9] = 256 * tau[9] - 576 * tau[7] + 432 * tau[5] - 120 * tau[3] + 9 * tau[1];
for (i = 0; i < 10; i++)
{
eps += (k[i] * owen_eps0_coef[icof][i]);
}
return(eps);
}
private Epsilon(JulianDayNumber date, double eps)
{
Date = date;
Eps = eps;
SinEps = Math.Sin(eps);
CosEps = Math.Cos(eps);
}
/// <see cref="deltat_longterm_morrison_stephenson"/>
public static double Calc(JulianDayNumber tjd)
{
var gregorianYear = tjd.GetGregorianYear();
double u = (gregorianYear - 1820) / 100.0;
return(-20 + 32 * u * u);
}
private void ReadPlanetConstants(SEFileData data)
{
foreach (var ipli in data.PlanetNumbers)
{
var pdp = new PlanetData();
pdp.InternalBodyNumber = ipli;
pdp.FileIndexStart = ReadInt32();
pdp.Flags = (PlanetFlags)_stream.ReadByte();
pdp.CoefficientsNumber = _stream.ReadByte();
pdp.NormalizationFactor = ReadInt32() / 1000.0;
var doubles = ReadDoubles(10);
pdp.StartDate = JulianDayNumber.FromRaw(doubles[0]);
pdp.EndDate = JulianDayNumber.FromRaw(doubles[1]);
pdp.SegmentSize = doubles[2];
pdp.IndexEntriesCount = (int)((doubles[1] - doubles[0] + 0.1) / doubles[2]);
pdp.ElementsEpoch = doubles[3];
pdp.Prot = doubles[4];
pdp.Dprot = doubles[5];
pdp.Qrot = doubles[6];
pdp.Dqrot = doubles[7];
pdp.Perigee = doubles[8];
pdp.DPerigee = doubles[9];
if (pdp.Flags.HasFlag(PlanetFlags.Ellipse))
{
pdp.ReferenceEllipseCoefficients = ReadDoubles(2 * pdp.CoefficientsNumber);
}
var index = ipli >= SEConsts.AseroidOffset
? InternalPlanets.AnyBody
: (InternalPlanets)ipli;
data.PlanetsData[index] = pdp;
}
}
public static (double dpre, double deps) swi_ldp_peps(JulianDayNumber tjd)
{
int i;
int npol = NPOL_PEPS;
int nper = NPER_PEPS;
double t, p, q, w, a, s, c;
t = (tjd - JulianDayNumber.J2000).Raw / 36525.0;
p = 0;
q = 0;
/* periodic terms */
for (i = 0; i < nper; i++)
{
w = Consts.TwoPi * t;
a = w / peper[0][i];
s = Math.Sin(a);
c = Math.Cos(a);
p += c * peper[1][i] + s * peper[3][i];
q += c * peper[2][i] + s * peper[4][i];
}
/* polynomial terms */
w = 1;
for (i = 0; i < npol; i++)
{
p += pepol[i][0] * w;
q += pepol[i][1] * w;
w *= t;
}
/* both to radians */
p *= AS2R;
q *= AS2R;
return(p, q);
}
/* precession matrix */
public static double[] pre_pmat(JulianDayNumber tjd)
{
//tjd = 1219339.078000;
/*equator pole */
var peqr = pre_pequ(tjd);
/* ecliptic pole */
var pecl = pre_pecl(tjd);
/* equinox */
var v = Calculus.CrossProduct(peqr, pecl);
var w = Math.Sqrt(v[0] * v[0] + v[1] * v[1] + v[2] * v[2]);
double[] eqx = new[]
{
v[0] / w,
v[1] / w,
v[2] / w,
};
v = Calculus.CrossProduct(peqr, eqx);
return(new[]
{
eqx[0],
eqx[1],
eqx[2],
v[0],
v[1],
v[2],
peqr[0],
peqr[1],
peqr[2],
});
}
public static double Calc(JulianDayNumber julianDay, double tidalAcceleration)
{
var gregorianYear = julianDay.GetGregorianYear();
double dt = 0.0;
if (julianDay >= J2016 || julianDay < JMinus720)
{
var t = (gregorianYear - 1825) / 100.0;
dt = -320 + 32.5 * t * t;
if (julianDay >= J2016)
{
dt += 269.4790417; // to make curve continous on 1 Jan 2016 (D. Koch)
}
else
{
dt -= 179.7337208; // to make curve continous on 1 Jan -720 (D. Koch)
}
}
else
{
for (int i = 0; i < _coefficients.Length; i++)
{
ref var data = ref _coefficients[i];
if (julianDay < data.End)
{
var t = (double)(julianDay - data.Begin) / (double)(data.End - data.Begin);
dt = data.Coef1 + data.Coef2 * t + data.Coef3 * t * t + data.Coef4 * t * t * t;
}
}
}
/// <summary>
/// start and end epoch of file
/// </summary>
private (JulianDayNumber, JulianDayNumber) ReadFilePeriod()
{
var buff = ReadDoubles(2);
double start = buff[0];
double end = buff[1];
return(JulianDayNumber.FromRaw(start), JulianDayNumber.FromRaw(end));
}
public SEFileSegment(JulianDayNumber start, JulianDayNumber size, double[] coefficients, int evaluateCoefficientsCount)
{
Start = start;
Size = size;
_coefficients = coefficients;
var partSize = coefficients.Length / 3;
LongitudeCoefficients = new ArraySegment <double>(_coefficients, 0, evaluateCoefficientsCount);
LatitudeCoefficients = new ArraySegment <double>(_coefficients, partSize, evaluateCoefficientsCount);
DistanceCoefficients = new ArraySegment <double>(_coefficients, partSize * 2, evaluateCoefficientsCount);
}
/// <summary>
/// Stephenson & Morrison (2004)
/// </summary>
public static double Calc(JulianDayNumber tjd, double tid_acc)
{
double ans = 0, ans2, ans3;
double p, B, dd;
double tjd0;
int iy;
double Y = tjd.GetGregorianYear();
/* before -1000:
* formula by Stephenson & Morrison (2004; p. 335) but adjusted to fit the
* starting point of table dt2. */
if (Y < DeltaTTabulated.Tab2Start)
{
// before -1000
ans = DeltaTLongtermMorrisonStephenson.Calc(tjd);
ans = TidalAcceleration.AdjustForTidalAcceleration(ans, Y, tid_acc, TidalAccelerationMode.Const26, false);
/* transition from formula to table over 100 years */
if (Y >= DeltaTTabulated.Tab2Start - 100)
{
/* starting value of table dt2: */
ans2 = TidalAcceleration.AdjustForTidalAcceleration(DeltaTTabulated.dt2[0], DeltaTTabulated.Tab2Start, tid_acc, TidalAccelerationMode.Const26, false);
/* value of formula at epoch TAB2_START */
/* B = (TAB2_START - LTERM_EQUATION_YSTART) * 0.01;
* ans3 = -20 + LTERM_EQUATION_COEFF * B * B;*/
tjd0 = (DeltaTTabulated.Tab2Start - 2000) * 365.2425 + (double)JulianDayNumber.J2000;
ans3 = DeltaTLongtermMorrisonStephenson.Calc(JulianDayNumber.FromRaw(tjd0));
ans3 = TidalAcceleration.AdjustForTidalAcceleration(ans3, Y, tid_acc, TidalAccelerationMode.Const26, false);
dd = ans3 - ans2;
B = (Y - (DeltaTTabulated.Tab2Start - 100)) * 0.01;
/* fit to starting point of table dt2. */
ans -= dd * B;
}
}
/* between -1000 and 1600:
* linear interpolation between values of table dt2 (Stephenson & Morrison 2004) */
if (Y >= DeltaTTabulated.Tab2Start && Y < DeltaTTabulated.Tab2End)
{
double Yjul = tjd.GetJulianYear();
p = Math.Floor(Yjul);
iy = (int)((p - DeltaTTabulated.Tab2Start) / DeltaTTabulated.Tab2Step);
dd = (Yjul - (DeltaTTabulated.Tab2Start + DeltaTTabulated.Tab2Step * iy)) / DeltaTTabulated.Tab2Step;
ans = DeltaTTabulated.dt2[iy] + (DeltaTTabulated.dt2[iy + 1] - DeltaTTabulated.dt2[iy]) * dd;
/* correction for tidal acceleration used by our ephemeris */
ans = TidalAcceleration.AdjustForTidalAcceleration(ans, Y, tid_acc, TidalAccelerationMode.Const26, false);
}
ans /= 86400.0;
return(ans);
}
/*
* Long term high precision precession,
* according to Vondrak/Capitaine/Wallace, "New precession expressions, valid
* for long time intervals", in A&A 534, A22(2011).
*/
/* precession of the ecliptic */
public static double[] pre_pecl(JulianDayNumber tjd)
{
int i;
int npol = NPOL_PECL;
int nper = NPER_PECL;
double t, p, q, w, a, s, c, z;
t = (tjd - JulianDayNumber.J2000).Raw / 36525.0;
p = 0;
q = 0;
/* periodic terms */
for (i = 0; i < nper; i++)
{
w = Consts.TwoPi * t;
a = w / pqper[0][i];
s = Math.Sin(a);
c = Math.Cos(a);
p += c * pqper[1][i] + s * pqper[3][i];
q += c * pqper[2][i] + s * pqper[4][i];
}
/* polynomial terms */
w = 1;
for (i = 0; i < npol; i++)
{
p += pqpol[i][0] * w;
q += pqpol[i][1] * w;
w *= t;
}
/* both to radians */
p *= AS2R;
q *= AS2R;
/* ecliptic pole vector */
z = 1 - p * p - q * q;
if (z < 0)
{
z = 0;
}
else
{
z = Math.Sqrt(z);
}
s = Math.Sin(EPS0);
c = Math.Cos(EPS0);
return(new[]
{
p,
-q * c - z * s,
-q * s + z * c,
});
}
private static (JulianDayNumber, int) get_owen_t0_icof(JulianDayNumber tjd)
{
int j = 0;
var t0 = t0s[0];
for (int i = 1; i < 5; i++)
{
if (tjd.Raw < (t0s[i - 1] + t0s[i]).Raw / 2)
{
;
}
else
{
t0 = t0s[i];
j++;
}
}
return(t0, j);
}
/* precession of the equator */
public static double[] pre_pequ(JulianDayNumber tjd)
{
int i;
int npol = NPOL_PEQU;
int nper = NPER_PEQU;
double t, x, y, w, a, s, c;
t = (tjd - JulianDayNumber.J2000).Raw / 36525.0;
x = 0;
y = 0;
for (i = 0; i < nper; i++)
{
w = Consts.TwoPi * t;
a = w / xyper[0][i];
s = Math.Sin(a);
c = Math.Cos(a);
x += c * xyper[1][i] + s * xyper[3][i];
y += c * xyper[2][i] + s * xyper[4][i];
}
/* polynomial terms */
w = 1;
for (i = 0; i < npol; i++)
{
x += xypol[i][0] * w;
y += xypol[i][1] * w;
w *= t;
}
x *= AS2R;
y *= AS2R;
/* equator pole vector */
w = x * x + y * y;
return(new[]
{
x,
y,
w < 1 ? Math.Sqrt(1 - w) : 0
});
}
/// <summary>
/// Calculate DeltaT
/// </summary>
/// <remarks>
/// delta t is adjusted to the tidal acceleration that is compatible
/// with the ephemeris mode contained in ephemerisMode and with the ephemeris
/// files made accessible through swe_set_ephe_path() or swe_set_jplfile().
/// If ephemerisMode is null, then the default tidal acceleration is ussed(i.e. that of DE431).
/// </remarks>
/// <see cref="calc_deltat"/>
/// <returns>DeltaT (ET - UT) in days</returns>
public static double Calc(JulianDayNumber julianDay, DeltaTMode deltaTMode, EphemerisMode?ephemerisMode)
{
var tidalAcceleration = ephemerisMode is null
? TidalAcceleration.Get(JPLDENumber.Default)
: TidalAcceleration.Calculate(ephemerisMode.Value, julianDay, JPLDENumber.Auto);
if (deltaTMode == DeltaTMode.Stephenson_Etc_2016 && julianDay < JulianDayNumber.J1955)
{
double deltaT = DeltaTStephensonEtc2016.Calc(julianDay, tidalAcceleration);
if (julianDay >= JulianDayNumber.J1952_05_04)
{
deltaT += (1.0 - (double)(JulianDayNumber.J1955 - julianDay) / 1000.0) * 0.6610218 / 86400.0;
}
return(deltaT);
}
if (deltaTMode == DeltaTMode.Espenak_Meeus_2006 && julianDay < J1633)
{
return(DeltaTEspenakMeeus1620.Calc(julianDay, tidalAcceleration));
}
var year = julianDay.GetYear();
// delta t model used in SE 1.72 - 1.76: Stephenson & Morrison 2004; before 1620
if (deltaTMode == DeltaTMode.Stephenson_Morrison_2004 && year < DeltaTTabulated.TabStart)
{
// before 1600:
if (year < DeltaTTabulated.Tab2End)
{
return(DeltaTStephensonMorrison2004_1600.Calc(julianDay, tidalAcceleration));
}
else
{
// between 1600 and 1620:
// linear interpolation between end of table dt2 and start of table dt
return(DeltaTTabulated.CalcInterpolated(year, julianDay.GetGregorianYear(), tidalAcceleration));
}
}
/* delta t model used before SE 1.64:
* Stephenson/Morrison 1984 with Borkowski 1988;
* before 1620 */
if (deltaTMode == DeltaTMode.Stephenson_Morrison_1984 && year < DeltaTTabulated.TabStart)
{
double B;
double ans;
if (year >= 948.0)
{
/* Stephenson and Morrison, stated domain is 948 to 1600:
* 25.5(centuries from 1800)^2 - 1.9159(centuries from 1955)^2 */
B = 0.01 * (year - 2000.0);
ans = (23.58 * B + 100.3) * B + 101.6;
}
else
{
/* Borkowski, before 948 and between 1600 and 1620 */
B = 0.01 * (year - 2000.0) + 3.75;
ans = 35.0 * B * B + 40.0;
}
return(ans / 86400.0);
}
/* 1620 - today + a few years (tabend):
* Tabulated values of deltaT from Astronomical Almanac
* (AA 1997etc., pp. K8-K9) and from IERS
* (http://maia.usno.navy.mil/ser7/deltat.data).
*/
if (year >= DeltaTTabulated.TabStart)
{
return(DeltaTTabulated.Calc(julianDay, tidalAcceleration, deltaTMode));
}
return(0);
}
/// <summary>
/// The tabulated values of deltaT, in hundredths of a second,
/// were taken from The Astronomical Almanac 1997etc., pp.K8-K9.
/// Some more recent values are taken from IERS
/// http://maia.usno.navy.mil/ser7/deltat.data .
/// </summary>
/// <remarks>
/// Bessel's interpolation formula is implemented to obtain fourth
/// order interpolated values at intermediate times.
/// The values are adjusted depending on the ephemeris used
/// and its inherent value of secular tidal acceleration ndot.
/// Note by Dieter Jan. 2017:
/// Bessel interpolation assumes equidistant sampling points. However the
/// sampling points are not equidistant, because they are for first January of
/// every year and years can have either 365 or 366 days.The interpolation uses
/// a step width of 365.25 days.As a consequence, in three out of four years
/// the interpolation does not reproduce the exact values of the sampling points
/// on the days they refer to.
/// </remarks>
/// <see cref="deltat_aa"/>
public static double Calc(JulianDayNumber tjd, double tid_acc, DeltaTMode mode)
{
double ans, ans2 = 0, ans3;
double p, B, B2, Y, dd;
double[] d = new double[6];
int i, iy, k;
Y = tjd.GetYear();
if (Y <= TabEnd)
{
// Index into the table.
p = Math.Floor(Y);
iy = (int)(p - TabStart);
/* Zeroth order estimate is value at start of year */
ans = dt[iy];
k = iy + 1;
if (k >= TabSize)
{
goto done; /* No data, can't go on. */
}
/* The fraction of tabulation interval */
p = Y - p;
/* First order interpolated value */
ans += p * (dt[k] - dt[iy]);
if ((iy - 1 < 0) || (iy + 2 >= TabSize))
{
goto done; /* can't do second differences */
}
/* Make table of first differences */
k = iy - 2;
for (i = 0; i < 5; i++)
{
if ((k < 0) || (k + 1 >= TabSize))
{
d[i] = 0;
}
else
{
d[i] = dt[k + 1] - dt[k];
}
k += 1;
}
/* Compute second differences */
for (i = 0; i < 4; i++)
{
d[i] = d[i + 1] - d[i];
}
B = 0.25 * p * (p - 1.0);
ans += B * (d[1] + d[2]);
if (iy + 2 >= TabSize)
{
goto done;
}
/* Compute third differences */
for (i = 0; i < 3; i++)
{
d[i] = d[i + 1] - d[i];
}
B = 2.0 * B / 3.0;
ans += (p - 0.5) * B * d[1];
if ((iy - 2 < 0) || (iy + 3 > TabSize))
{
goto done;
}
/* Compute fourth differences */
for (i = 0; i < 2; i++)
{
d[i] = d[i + 1] - d[i];
}
B = 0.125 * B * (p + 1.0) * (p - 2.0);
ans += B * (d[0] + d[1]);
done:
ans = TidalAcceleration.AdjustForTidalAcceleration(ans, Y, tid_acc, TidalAccelerationMode.Const26, false);
return(ans / 86400.0);
}
/* today - future:
* 3rd degree polynomial based on data given by
* Stephenson/Morrison/Hohenkerk 2016 here:
* http://astro.ukho.gov.uk/nao/lvm/
*/
if (mode == DeltaTMode.Stephenson_Etc_2016)
{
B = Y - 2000;
if (Y < 2500)
{
ans = B * B * B * 121.0 / 30000000.0 + B * B / 1250.0 + B * 521.0 / 3000.0 + 64.0;
/* for slow transition from tablulated data */
B2 = TabEnd - 2000;
ans2 = B2 * B2 * B2 * 121.0 / 30000000.0 + B2 * B2 / 1250.0 + B2 * 521.0 / 3000.0 + 64.0;
/* we use a parable after 2500 */
}
else
{
B = 0.01 * (Y - 2000);
ans = B * B * 32.5 + 42.5;
}
/*
* Formula Stephenson (1997; p. 507),
* with modification to avoid jump at end of AA table,
* similar to what Meeus 1998 had suggested.
* Slow transition within 100 years.
*/
}
else
{
B = 0.01 * (Y - 1820);
ans = -20 + 31 * B * B;
/* for slow transition from tablulated data */
B2 = 0.01 * (TabEnd - 1820);
ans2 = -20 + 31 * B2 * B2;
}
/* slow transition from tabulated values to Stephenson formula: */
if (Y <= TabEnd + 100)
{
ans3 = dt[TabSize - 1];
dd = (ans2 - ans3);
ans += dd * (Y - (TabEnd + 100)) * 0.01;
}
return(ans / 86400.0);
}
/// <summary> /// Fetch chebyshew coefficients from sweph file /// </summary> /// <param name="pdp">Planet</param> /// <param name="jd">Time</param> /// <param name="epsilonJ2000">Epsilon for J2000</param> /// <see cref="get_new_segment"/> internal SEFileSegment ReadSegment(PlanetData pdp, JulianDayNumber jd, Epsilon epsilonJ2000) => _reader.ReadSegment(pdp, jd, epsilonJ2000);
/// <summary>
/// Model used SE 1.77 - 2.05.01, for epochs before 1633:
/// Polynomials by Espenak & Meeus 2006, derived from Stephenson & Morrison 2004.
/// deltat_model == SEMOD_DELTAT_ESPENAK_MEEUS_2006:
/// This method is used only for epochs before 1633.
/// (For more recent epochs, we use the data provided by Astronomical Almanac K8-K9.)
/// </summary>
/// <see cref="deltat_espenak_meeus_1620"/>
public static double Calc(JulianDayNumber tjd, double tidalAcceleration)
{
double ans = 0;
double u;
double Ygreg = tjd.GetGregorianYear();
if (Ygreg < -500)
{
ans = DeltaTLongtermMorrisonStephenson.Calc(tjd);
}
else if (Ygreg < 500)
{
u = Ygreg / 100.0;
ans = (((((0.0090316521 * u + 0.022174192) * u - 0.1798452) * u - 5.952053) * u + 33.78311) * u - 1014.41) * u + 10583.6;
}
else if (Ygreg < 1600)
{
u = (Ygreg - 1000) / 100.0;
ans = (((((0.0083572073 * u - 0.005050998) * u - 0.8503463) * u + 0.319781) * u + 71.23472) * u - 556.01) * u + 1574.2;
}
else if (Ygreg < 1700)
{
u = Ygreg - 1600;
ans = 120 - 0.9808 * u - 0.01532 * u * u + u * u * u / 7129.0;
}
else if (Ygreg < 1800)
{
u = Ygreg - 1700;
ans = (((-u / 1174000.0 + 0.00013336) * u - 0.0059285) * u + 0.1603) * u + 8.83;
}
else if (Ygreg < 1860)
{
u = Ygreg - 1800;
ans = ((((((0.000000000875 * u - 0.0000001699) * u + 0.0000121272) * u - 0.00037436) * u + 0.0041116) * u + 0.0068612) * u - 0.332447) * u + 13.72;
}
else if (Ygreg < 1900)
{
u = Ygreg - 1860;
ans = ((((u / 233174.0 - 0.0004473624) * u + 0.01680668) * u - 0.251754) * u + 0.5737) * u + 7.62;
}
else if (Ygreg < 1920)
{
u = Ygreg - 1900;
ans = (((-0.000197 * u + 0.0061966) * u - 0.0598939) * u + 1.494119) * u - 2.79;
}
else if (Ygreg < 1941)
{
u = Ygreg - 1920;
ans = 21.20 + 0.84493 * u - 0.076100 * u * u + 0.0020936 * u * u * u;
}
else if (Ygreg < 1961)
{
u = Ygreg - 1950;
ans = 29.07 + 0.407 * u - u * u / 233.0 + u * u * u / 2547.0;
}
else if (Ygreg < 1986)
{
u = Ygreg - 1975;
ans = 45.45 + 1.067 * u - u * u / 260.0 - u * u * u / 718.0;
}
else if (Ygreg < 2005)
{
u = Ygreg - 2000;
ans = ((((0.00002373599 * u + 0.000651814) * u + 0.0017275) * u - 0.060374) * u + 0.3345) * u + 63.86;
}
ans = TidalAcceleration.AdjustForTidalAcceleration(ans, Ygreg, tidalAcceleration, TidalAccelerationMode.Const26, false);
ans /= 86400.0;
return(ans);
}
/// <summary>
/// Fetch chebyshew coefficients from sweph file
/// </summary>
/// <param name="pdp">Planet</param>
/// <param name="jd">Time</param>
/// <param name="epsilonJ2000">Epsilon for J2000</param>
/// <see cref="get_new_segment"/>
internal SEFileSegment ReadSegment(PlanetData pdp, JulianDayNumber jd, Epsilon epsilonJ2000)
{
int segmentNumber = (int)((jd - pdp.StartDate).Raw / pdp.SegmentSize);
var segmentStart = pdp.StartDate + JulianDayNumber.FromRaw(pdp.SegmentSize * segmentNumber);
var fpos = pdp.FileIndexStart + segmentNumber * 3;
fpos = ReadInt32From3Bytes(fpos);
_stream.Seek(fpos, SeekOrigin.Begin);
var rmax = pdp.NormalizationFactor;
double[] segp = new double[pdp.CoefficientsNumber * 3];
// read coefficients for 3 coordinates
for (var icoord = 0; icoord < 3; icoord++)
{
var idbl = icoord * pdp.CoefficientsNumber;
// first read header
// first bit indicates number of sizes of packed coefficients
int nco;
int nsizes;
int[] nsize = new int[6];
var c = ReadData(1, 2);
if ((c[0] & 128) > 0)
{
var c2 = ReadData(1, 2);
nsizes = 6;
nsize[0] = c[1] / 16;
nsize[1] = c[1] % 16;
nsize[2] = c2[0] / 16;
nsize[3] = c2[0] % 16;
nsize[4] = c2[1] / 16;
nsize[5] = c2[1] % 16;
nco = nsize[0] + nsize[1] + nsize[2] + nsize[3] + nsize[4] + nsize[5];
}
else
{
nsizes = 4;
nsize[0] = c[0] / 16;
nsize[1] = c[0] % 16;
nsize[2] = c[1] / 16;
nsize[3] = c[1] % 16;
nco = nsize[0] + nsize[1] + nsize[2] + nsize[3];
}
// there may not be more coefficients than interpolation order + 1
if (nco > pdp.CoefficientsNumber)
{
throw new FormatException($"Error in ephemeris file: {nco} coefficients instead of {pdp.CoefficientsNumber}");
}
// now unpack
for (var i = 0; i < nsizes; i++)
{
if (nsize[i] == 0)
{
continue;
}
if (i < 4)
{
int j = 4 - i;
int k = nsize[i];
var longs = ReadUints(j, k);
for (int m = 0; m < k; m++)
{
if ((longs[m] & 1) > 0) // will be negative
{
segp[idbl] = -(((longs[m] + 1) / 2) / 1e+9 * rmax / 2);
}
else
{
segp[idbl] = (longs[m] / 2) / 1e+9 * rmax / 2;
}
idbl++;
}
}
else if (i == 4) // half byte packing
{
int k = (nsize[i] + 1) / 2;
var longs = ReadUints(1, k);
for (int m = 0, j = 0;
m < k && j < nsize[i];
m++)
{
for (int n = 0, o = 16;
n < 2 && j < nsize[i];
n++, j++, idbl++, longs[m] %= (uint)o, o /= 16)
{
if ((longs[m] & o) > 0)
{
segp[idbl] = -(((longs[m] + o) / o / 2) * rmax / 2 / 1e+9);
}
else
{
segp[idbl] = (longs[m] / o / 2) * rmax / 2 / 1e+9;
}
}
}
}
else if (i == 5) // quarter byte packing
{
int k = (nsize[i] + 3) / 4;
var longs = ReadUints(1, k);
for (int m = 0, j = 0;
m < k && j < nsize[i];
m++)
{
for (int n = 0, o = 64;
n < 4 && j < nsize[i];
n++, j++, idbl++, longs[m] %= (uint)o, o /= 4)
{
if ((longs[m] & o) > 0)
{
segp[idbl] = -(((longs[m] + o) / o / 2) * rmax / 2 / 1e+9);
}
else
{
segp[idbl] = (longs[m] / o / 2) * rmax / 2 / 1e+9;
}
}
}
}
}
}
int evaluateCoefficientsCount = pdp.Flags.HasFlag(PlanetFlags.Rotate)
? RotateBack(pdp, segmentStart, segp, epsilonJ2000)
: pdp.CoefficientsNumber;
var segment = new SEFileSegment(segmentStart, JulianDayNumber.FromRaw(pdp.SegmentSize), segp, evaluateCoefficientsCount);
return(segment);
}
public static Epsilon Calc(JulianDayNumber J, SEFLG iflag, SweData swed)
{
var prec_model = swed.LongtermPrecessionMode;
var prec_model_short = swed.ShorttermPrecessionMode;
var jplhora_model = swed.JplHorizonsMode;
bool is_jplhor = false;
if (iflag.HasFlag(SEFLG.JPLHOR))
{
is_jplhor = true;
}
if (iflag.HasFlag(SEFLG.JPLHOR_APPROX) &&
jplhora_model == JplHorizonsMode.Three &&
J <= HORIZONS_TJD0_DPSI_DEPS_IAU1980)
{
is_jplhor = true;
}
double T = (J - JulianDayNumber.J2000).Raw / 36525.0;
double eps;
if (is_jplhor)
{
if (J > JulianDayNumber.J1799_01_01 && J < JulianDayNumber.J2202_01_01)
{ // between 1.1.1799 and 1.1.2202
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.8150) * T + 84381.448) * DEGTORAD / 3600;
}
else
{
eps = OwenPrecession.epsiln_owen_1986(J);
eps *= DEGTORAD;
}
}
else if (iflag.HasFlag(SEFLG.JPLHOR_APPROX) && jplhora_model == JplHorizonsMode.Two)
{
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.8150) * T + 84381.448) * DEGTORAD / 3600;
}
else if (prec_model_short == PrecessionModel.IAU_1976 && Math.Abs(T) <= PREC_IAU_1976_CTIES)
{
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.8150) * T + 84381.448) * DEGTORAD / 3600;
}
else if (prec_model == PrecessionModel.IAU_1976)
{
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.8150) * T + 84381.448) * DEGTORAD / 3600;
}
else if (prec_model_short == PrecessionModel.IAU_2000 && Math.Abs(T) <= PREC_IAU_2000_CTIES)
{
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.84024) * T + 84381.406) * DEGTORAD / 3600;
}
else if (prec_model == PrecessionModel.IAU_2000)
{
eps = (((1.813e-3 * T - 5.9e-4) * T - 46.84024) * T + 84381.406) * DEGTORAD / 3600;
}
else if (prec_model_short == PrecessionModel.IAU_2006 && Math.Abs(T) <= PREC_IAU_2006_CTIES)
{
eps = (((((-4.34e-8 * T - 5.76e-7) * T + 2.0034e-3) * T - 1.831e-4) * T - 46.836769) * T + 84381.406) * DEGTORAD / 3600.0;
}
else if (prec_model == PrecessionModel.IAU_2006)
{
eps = (((((-4.34e-8 * T - 5.76e-7) * T + 2.0034e-3) * T - 1.831e-4) * T - 46.836769) * T + 84381.406) * DEGTORAD / 3600.0;
}
else if (prec_model == PrecessionModel.BRETAGNON_2003)
{
eps = ((((((-3e-11 * T - 2.48e-8) * T - 5.23e-7) * T + 1.99911e-3) * T - 1.667e-4) * T - 46.836051) * T + 84381.40880) * DEGTORAD / 3600.0;
}
else if (prec_model == PrecessionModel.SIMON_1994)
{
eps = (((((2.5e-8 * T - 5.1e-7) * T + 1.9989e-3) * T - 1.52e-4) * T - 46.80927) * T + 84381.412) * DEGTORAD / 3600.0; /* */
}
else if (prec_model == PrecessionModel.WILLIAMS_1994)
{
eps = ((((-1.0e-6 * T + 2.0e-3) * T - 1.74e-4) * T - 46.833960) * T + 84381.409) * DEGTORAD / 3600.0; /* */
}
else if (prec_model == PrecessionModel.LASKAR_1986 || prec_model == PrecessionModel.WILL_EPS_LASK)
{
T /= 10.0;
eps = (((((((((2.45e-10 * T + 5.79e-9) * T + 2.787e-7) * T
+ 7.12e-7) * T - 3.905e-5) * T - 2.4967e-3) * T
- 5.138e-3) * T + 1.99925) * T - 0.0155) * T - 468.093) * T
+ 84381.448;
eps *= DEGTORAD / 3600.0;
}
else if (prec_model == PrecessionModel.OWEN_1990)
{
eps = OwenPrecession.epsiln_owen_1986(J);
eps *= DEGTORAD;
}
else
{ /* SEMOD_PREC_VONDRAK_2011 */
(_, eps) = Vondrak.swi_ldp_peps(J);
if (iflag.HasFlag(SEFLG.JPLHOR_APPROX) && jplhora_model != JplHorizonsMode.Two)
{
double tofs = (J - DCOR_EPS_JPL_TJD0).Raw / 365.25;
double dofs;
if (tofs < 0)
{
dofs = dcor_eps_jpl[0];
}
else if (tofs >= dcor_eps_jpl.Length)
{
dofs = dcor_eps_jpl.Last();
}
else
{
int t0 = (int)tofs;
int t1 = t0 + 1;
dofs = (tofs - t0) * (dcor_eps_jpl[t0] - dcor_eps_jpl[t1]) + dcor_eps_jpl[t0];
}
dofs /= (1000.0 * 3600.0);
eps += dofs * DEGTORAD;
}
}
return(new Epsilon(J, eps));
}
/// <summary>
/// <c>rot_back</c>
/// Adds reference orbit to chebyshew series (if SEI_FLG_ELLIPSE),
/// rotates series to mean equinox of J2000
/// </summary>
private int RotateBack(PlanetData pdp, JulianDayNumber segmentStart, double[] coefficients, Epsilon epsilon)
{
int nco = pdp.CoefficientsNumber;
var t = segmentStart.Raw + pdp.SegmentSize / 2;
// data align: chcfx double[nco] + chcfy double[nco] + chcfz double[nco]
// allsize: nco * 3
var segp = coefficients;
var chcfx = new Span <double>(segp, 0, nco);
var chcfy = new Span <double>(segp, nco, nco);
var chcfz = new Span <double>(segp, nco * 2, nco);
var tdiff = (t - pdp.ElementsEpoch) / 365250.0;
double qav, pav;
if (pdp.InternalBodyNumber == (int)InternalPlanets.Moon)
{
var dn = pdp.Prot + tdiff * pdp.Dprot;
var i = (int)(dn / Consts.TwoPi);
dn -= i * Consts.TwoPi;
qav = (pdp.Qrot + tdiff * pdp.Dqrot) * Math.Cos(dn);
pav = (pdp.Qrot + tdiff * pdp.Dqrot) * Math.Sin(dn);
}
else
{
qav = pdp.Qrot + tdiff * pdp.Dqrot;
pav = pdp.Prot + tdiff * pdp.Dprot;
}
// calculate cosine and sine of average perihelion longitude.
var x = new double[nco, 3];
for (int i = 0; i < nco; i++)
{
x[i, 0] = chcfx[i];
x[i, 1] = chcfy[i];
x[i, 2] = chcfz[i];
}
if (pdp.Flags.HasFlag(PlanetFlags.Ellipse))
{
var refepx = new Span <double>(pdp.ReferenceEllipseCoefficients, 0, nco);
var refepy = new Span <double>(pdp.ReferenceEllipseCoefficients, nco, nco);
var omtild = pdp.Perigee + tdiff + pdp.DPerigee;
int i = (int)(omtild / Consts.TwoPi);
omtild -= i * Consts.TwoPi;
var com = Math.Cos(omtild);
var som = Math.Sin(omtild);
// add reference orbit.
for (i = 0; i < nco; i++)
{
x[i, 0] = chcfx[i] + com * refepx[i] - som * refepy[i];
x[i, 1] = chcfy[i] + com * refepy[i] + som * refepx[i];
}
}
/* construct right handed orthonormal system with first axis along
* origin of longitudes and third axis along angular momentum
* this uses the standard formulas for equinoctal variables
* (see papers by broucke and by cefola). */
var cosih2 = 1.0 / (1.0 + qav * qav + pav * pav);
// calculate orbit pole.
Span <double> uiz = stackalloc double[3];
uiz[0] = 2.0 * pav * cosih2;
uiz[1] = -2.0 * qav * cosih2;
uiz[2] = (1.0 - qav * qav - pav * pav) * cosih2;
// calculate origin of longitudes vector.
Span <double> uix = stackalloc double[3];
uix[0] = (1.0 + qav * qav - pav * pav) * cosih2;
uix[1] = 2.0 * qav * pav * cosih2;
uix[2] = -2.0 * pav * cosih2;
// calculate vector in orbital plane orthogonal to origin of longitudes.
Span <double> uiy = stackalloc double[3];
uiy[0] = 2.0 * qav * pav * cosih2;
uiy[1] = (1.0 - qav * qav + pav * pav) * cosih2;
uiy[2] = 2.0 * qav * cosih2;
int evaluateCoefficientsCount = 0;
// rotate to actual orientation in space.
for (var i = 0; i < nco; i++)
{
var xrot = x[i, 0] * uix[0] + x[i, 1] * uiy[0] + x[i, 2] * uiz[0];
var yrot = x[i, 0] * uix[1] + x[i, 1] * uiy[1] + x[i, 2] * uiz[1];
var zrot = x[i, 0] * uix[2] + x[i, 1] * uiy[2] + x[i, 2] * uiz[2];
if (Math.Abs(xrot) + Math.Abs(yrot) + Math.Abs(zrot) >= 1e-14)
{
evaluateCoefficientsCount = i;
}
x[i, 0] = xrot;
x[i, 1] = yrot;
x[i, 2] = zrot;
if (pdp.InternalBodyNumber == (int)InternalPlanets.Moon)
{
/* rotate to j2000 equator */
x[i, 1] = epsilon.CosEps * yrot - epsilon.SinEps * zrot;
x[i, 2] = epsilon.SinEps * yrot + epsilon.CosEps * zrot;
}
}
for (var i = 0; i < nco; i++)
{
chcfx[i] = x[i, 0];
chcfy[i] = x[i, 1];
chcfz[i] = x[i, 2];
}
return(evaluateCoefficientsCount);
}