3436 lines
117 KiB
C
3436 lines
117 KiB
C
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/* SWISSEPH
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$Header: /home/dieter/sweph/RCS/swehel.c,v 1.1 2009/04/21 06:05:59 dieter Exp dieter $
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Heliacal risings and related calculations
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Author: Victor Reijs
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This program code is a translation of part of:
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Victor Reijs' software ARCHAEOCOSMO (archaeoastronomy and
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geodesy functions),
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http://www.iol.ie/~geniet/eng/archaeocosmoprocedures.htm
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Translation from VB into C by Dieter Koch
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Problem reports can be sent to victor.reijs@gmail.com or dieter@astro.ch
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Copyright (c) Victor Reijs, 2008
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License conditions
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------------------
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This file is part of Swiss Ephemeris.
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Swiss Ephemeris is distributed with NO WARRANTY OF ANY KIND. No author
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or distributor accepts any responsibility for the consequences of using it,
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or for whether it serves any particular purpose or works at all, unless he
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or she says so in writing.
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Swiss Ephemeris is made available by its authors under a dual licensing
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system. The software developer, who uses any part of Swiss Ephemeris
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in his or her software, must choose between one of the two license models,
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which are
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a) GNU public license version 2 or later
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b) Swiss Ephemeris Professional License
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The choice must be made before the software developer distributes software
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containing parts of Swiss Ephemeris to others, and before any public
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service using the developed software is activated.
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If the developer choses the GNU GPL software license, he or she must fulfill
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the conditions of that license, which includes the obligation to place his
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or her whole software project under the GNU GPL or a compatible license.
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See http://www.gnu.org/licenses/old-licenses/gpl-2.0.html
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If the developer choses the Swiss Ephemeris Professional license,
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he must follow the instructions as found in http://www.astro.com/swisseph/
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and purchase the Swiss Ephemeris Professional Edition from Astrodienst
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and sign the corresponding license contract.
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The License grants you the right to use, copy, modify and redistribute
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Swiss Ephemeris, but only under certain conditions described in the License.
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Among other things, the License requires that the copyright notices and
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this notice be preserved on all copies.
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The authors of Swiss Ephemeris have no control or influence over any of
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the derived works, i.e. over software or services created by other
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programmers which use Swiss Ephemeris functions.
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The names of the authors or of the copyright holder must not
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be used for promoting any software, product or service which uses or contains
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the Swiss Ephemeris. This copyright notice is the ONLY place where the
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names of the authors can legally appear, except in cases where they have
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given special permission in writing.
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The trademarks 'Swiss Ephemeris' and 'Swiss Ephemeris inside' may be used
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for promoting such software, products or services.
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*/
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#include "swephexp.h"
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#include "sweph.h"
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#include "swephlib.h"
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#include <sys/stat.h>
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#define PLSV 0 /*if Planet, Lunar and Stellar Visibility formula is needed PLSV=1*/
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#define criticalangle 0.0 /*[deg]*/
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#define BNIGHT 1479.0 /*[nL]*/
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#define BNIGHT_FACTOR 1.0
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#define PI M_PI
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#define Min2Deg (1.0 / 60.0)
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#define DEBUG 0
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#define DONE 1
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#define MaxTryHours 4
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#define TimeStepDefault 1
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#define LocalMinStep 8
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/* time constants */
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#define Y2D 365.25 /*[Day]*/
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#define D2Y (1 / Y2D) /*[Year]*/
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#define D2H 24.0 /*[Hour]*/
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#define H2S 3600.0 /*[sec]*/
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#define D2S (D2H * H2S) /*[sec]*/
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#define S2H (1.0 / H2S) /*[Hour]*/
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#define JC2D 36525.0 /*[Day]*/
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#define M2S 60.0 /*[sec]*/
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/* Determines which algorimths are used*/
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#define USE_DELTA_T_VR 0
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#define REFR_SINCLAIR 0
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#define REFR_BENNETTH 1
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#define FormAstroRefrac REFR_SINCLAIR /*for Astronomical refraction can be "bennetth" or "sinclair"*/
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#define GravitySource 2 /*0=RGO, 1=Wikipedia,2=Exp. Suppl. 1992,3=van der Werf*/
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#define REarthSource 1 /*0=RGO (constant), 1=WGS84 method*/
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#define StartYear 1820 /*[year]*/
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#define Average 1.80546834626888 /*[msec/cy]*/
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#define Periodicy 1443.67123144531 /*[year]*/
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#define Amplitude 3.75606495492684 /*[msec]*/
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#define phase 0 /*[deg]*/
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#define MAX_COUNT_SYNPER 5 /* search within 10 synodic periods */
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#define MAX_COUNT_SYNPER_MAX 1000000 /* high, so there is not max count */
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#define AvgRadiusMoon (15.541 / 60) /* '[Deg] at 2007 CE or BCE*/
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/* WGS84 ellipsoid constants
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* http://w3sli.wcape.gov.za/Surveys/Mapping/wgs84.htm*/
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#define Ra 6378136.6 /*'[m]*/
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#define Rb 6356752.314 /*'[m]*/
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/* choices in Schaefer's model */
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#define nL2erg (1.02E-15)
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#define erg2nL (1 / nL2erg) /*erg2nL to nLambert*/
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#define MoonDistance 384410.4978 /*[km]*/
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#define scaleHwater 3000.0 /*[m] Ricchiazzi [1997] 8200 Schaefer [2000]*/
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#define scaleHrayleigh 8515.0 /*[m] Su [2003] 8200 Schaefer [2000]*/
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#define scaleHaerosol 3745.0 /*m Su [2003] 1500 Schaefer [2000]*/
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#define scaleHozone 20000.0 /*[m] Schaefer [2000]*/
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#define astr2tau 0.921034037197618 /*LN(10 ^ 0.4)*/
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#define tau2astr 1 / astr2tau
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/* meteorological constants*/
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#define C2K 273.15 /*[K]*/
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#define DELTA 18.36
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#define TempNulDiff 0.000001
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#define PressRef 1000 /*[mbar]*/
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#define MD 28.964 /*[kg] Mol weight of dry air van der Werf*/
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#define MW 18.016 /*[kg] Mol weight of water vapor*/
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#define GCR 8314.472 /*[L/kmol/K] van der Werf*/
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#define LapseSA 0.0065 /*[K/m] standard atmosphere*/
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#define LapseDA 0.0098 /*[K/m] dry adiabatic*/
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/* lowest apparent altitude to provide*/
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#define LowestAppAlt -3.5 /*[Deg]*/
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/*optimization delta*/
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#define epsilon 0.001
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/* for Airmass usage*/
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#define staticAirmass 0 /* use staticAirmass=1 instead depending on difference k's*/
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/* optic stuff */
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#define GOpticMag 1 /*telescope magnification*/
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#define GOpticTrans 0.8 /*telescope transmission*/
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#define GBinocular 1 /*1-binocular 0=monocular*/
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#define GOpticDia 50 /*telescope diameter [mm]*/
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static double mymin(double a, double b)
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{
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if (a <= b)
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return a;
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return b;
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}
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static double mymax(double a, double b)
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{
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if (a >= b)
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return a;
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return b;
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}
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/*###################################################################*/
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static double Tanh(double x)
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{
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return (exp(x) - exp(-x)) / (exp(x) + exp(-x));
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}
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/*
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' B [nL]
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' SN [-]
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' CVA [deg]
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*/
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static double CVA(double B, double SN)
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{
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/*Schaefer, Astronomy and the limits of vision, Archaeoastronomy, 1993*/
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if (B > BNIGHT)
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return (40.0 / SN) * pow(10, (8.28 * pow(B, (-0.29)))) / 60.0 / 60.0;
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else
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return mymin(900, 380 / SN * pow(10, (0.3 * pow(B, (-0.29))))) / 60.0 / 60.0;
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}
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/*
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' age [year]
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' B [nL]
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' PupilDia [mm]
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*/
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static double PupilDia(double Age, double B)
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{
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/* age dependancy from Garstang [2000]*/
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return (0.534 - 0.00211 * Age - (0.236 - 0.00127 * Age) * Tanh(0.4 * log(B) / log(10) - 2.2)) * 10;
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}
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/*
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'Input
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' Bback [nL]
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' kX [-]
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' Binocular [-]
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' OpticMag [-]
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' OpticDia [mm]
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' OpticTrans [-]
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' JDNDaysUT [JDN]
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' Age [Year]
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' SN [-]
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' ObjectName
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' TypeFactor [0=itensity factor 1=background factor]
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'Output
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' OpticFactor [-]
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*/
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static double OpticFactor(double Bback, double kX, double *dobs, double JDNDaysUT, char *ObjectName, int TypeFactor, int helflag)
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{
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double Pst, CIb, CIi, ObjectSize, Fb, Fe, Fsc, Fci, Fcb, Ft, Fp, Fa, Fr, Fm;
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double Age = dobs[0];
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double SN = dobs[1], SNi;
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double Binocular = dobs[2];
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double OpticMag = dobs[3];
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double OpticDia = dobs[4];
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double OpticTrans = dobs[5];
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SNi = SN;
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if (SNi <= 0.00000001) SNi = 0.00000001;
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/* 23 jaar as standard from Garstang*/
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Pst = PupilDia(23, Bback);
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if (OpticMag == 1) { /*OpticMagn=1 means using eye*/
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OpticTrans = 1;
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OpticDia = Pst;
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}
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#if 0 /*is done in default_heliacal_parameters()*/
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if (OpticMag == 0) { /*OpticMagn=0 (undefined) using eye*/
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OpticTrans = 1;
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OpticDia = Pst;
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Binocular = 1;
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OpticMag = 1;
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}
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#endif
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/* Schaefer, Astronomy and the limits of vision, Archaeoastronomy, 1993*/
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CIb = 0.7; /* color of background (from Ben Sugerman)*/
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CIi = 0.5; /* Color index for white (from Ben Sugerman), should be function of ObjectName*/
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ObjectSize = 0;
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if (strcmp(ObjectName, "moon") == 0) {
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/*ObjectSize and CI needs to be determined (depending on JDNDaysUT)*/
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;
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}
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Fb = 1;
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if (Binocular == 0) Fb = 1.41;
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if (Bback < BNIGHT && !(helflag & SE_HELFLAG_VISLIM_PHOTOPIC)) {
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Fe = pow(10, (0.48 * kX));
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Fsc = mymin(1, (1 - pow(Pst / 124.4, 4)) / (1 - pow((OpticDia / OpticMag / 124.4), 4)));
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Fci = pow(10, (-0.4 * (1 - CIi / 2.0)));
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Fcb = pow(10, (-0.4 * (1 - CIb / 2.0)));
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} else {
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Fe = pow(10, (0.4 * kX));
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Fsc = mymin(1, pow((OpticDia / OpticMag / Pst), 2) * (1 - exp(-pow((Pst / 6.2), 2))) / (1 - exp(-pow((OpticDia / OpticMag / 6.2), 2))));
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Fci = 1;
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Fcb = 1;
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}
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Ft = 1 / OpticTrans;
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Fp = mymax(1, pow((Pst / (OpticMag * PupilDia(Age, Bback))), 2));
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Fa = pow((Pst / OpticDia), 2);
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Fr = (1 + 0.03 * pow((OpticMag * ObjectSize / CVA(Bback, SNi)), 2)) / pow(SNi, 2);
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Fm = pow(OpticMag, 2);
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#if DEBUG
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fprintf(stderr, "Pst=%f\n", Pst);
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fprintf(stderr, "Fb =%f\n", Fb);
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fprintf(stderr, "Fe =%f\n", Fe);
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fprintf(stderr, "Ft =%f\n", Ft);
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fprintf(stderr, "Fp =%f\n", Fp);
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fprintf(stderr, "Fa =%f\n", Fa);
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fprintf(stderr, "Fm =%f\n", Fm);
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fprintf(stderr, "Fsc=%f\n", Fsc);
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fprintf(stderr, "Fci=%f\n", Fci);
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fprintf(stderr, "Fcb=%f\n", Fcb);
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fprintf(stderr, "Fr =%f\n", Fr );
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#endif
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if (TypeFactor == 0)
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return Fb * Fe * Ft * Fp * Fa * Fr * Fsc * Fci;
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else
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return Fb * Ft * Fp * Fa * Fm * Fsc * Fcb;
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}
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/*###################################################################
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*/
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static int32 DeterObject(char *ObjectName)
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{
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char s[AS_MAXCH];
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char *sp;
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int32 ipl;
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strcpy(s, ObjectName);
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for (sp = s; *sp != '\0'; sp++)
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*sp = tolower(*sp);
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if (strncmp(s, "sun", 3) == 0)
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return SE_SUN;
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if (strncmp(s, "venus", 5) == 0)
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return SE_VENUS;
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if (strncmp(s, "mars", 4) == 0)
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return SE_MARS;
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if (strncmp(s, "mercur", 6) == 0)
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return SE_MERCURY;
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if (strncmp(s, "jupiter", 7) == 0)
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return SE_JUPITER;
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if (strncmp(s, "saturn", 6) == 0)
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return SE_SATURN;
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if (strncmp(s, "uranus", 6) == 0)
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return SE_URANUS;
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if (strncmp(s, "neptun", 6) == 0)
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return SE_NEPTUNE;
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if (strncmp(s, "moon", 4) == 0)
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return SE_MOON;
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if ((ipl = atoi(s)) > 0) {
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ipl += SE_AST_OFFSET;
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return ipl;
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}
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return -1;
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}
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#if 0
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int32 call_swe_calc(double tjd, int32 ipl, int32 iflag, double *x, char *serr)
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{
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int32 retval = OK, ipli, i;
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double dtjd;
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static double tjdsv[3];
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static double xsv[3][6];
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static int32 iflagsv[3];
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ipli = ipl;
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if (ipli > SE_MOON)
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ipli = 2;
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dtjd = tjd - tjdsv[ipli];
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if (tjdsv[ipli] != 0 && iflag == iflagsv[ipli] && fabs(dtjd) < 5.0 / 1440.0) {
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for (i = 0; i < 3; i++)
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x[i] = xsv[ipli][i] + dtjd * xsv[ipli][i+3];
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for (i = 3; i < 6; i++)
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x[i] = xsv[ipli][i];
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} else {
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retval = swe_calc(tjd, ipl, iflag, x, serr);
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tjdsv[ipli] = tjd;
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iflagsv[ipli] = iflag;
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for (i = 0; i < 6; i++)
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xsv[ipli][i] = x[i];
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}
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return retval;
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}
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#endif
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/* avoids problems with star name string that may be overwritten by
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swe_fixstar() */
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int32 call_swe_fixstar(char *star, double tjd, int32 iflag, double *xx, char *serr)
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{
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int32 retval;
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char star2[AS_MAXCH];
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strcpy(star2, star);
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retval = swe_fixstar(star2, tjd, iflag, xx, serr);
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return retval;
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}
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/* avoids problems with star name string that may be overwritten by
|
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swe_fixstar_mag() */
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int32 call_swe_fixstar_mag(char *star, double *mag, char *serr)
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{
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int32 retval;
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char star2[AS_MAXCH];
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static double dmag;
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static char star_save[AS_MAXCH];
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if (strcmp(star, star_save) == 0) {
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*mag = dmag;
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return OK;
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}
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strcpy(star_save, star);
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strcpy(star2, star);
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retval = swe_fixstar_mag(star2, &dmag, serr);
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*mag = dmag;
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return retval;
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}
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/* avoids problems with star name string that may be overwritten by
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swe_fixstar() */
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int32 call_swe_rise_trans(double tjd, int32 ipl, char *star, int32 helflag, int32 eventtype, double *dgeo, double atpress, double attemp, double *tret, char *serr)
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{
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int32 retval;
|
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int32 iflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
char star2[AS_MAXCH];
|
||
|
strcpy(star2, star);
|
||
|
retval = swe_rise_trans(tjd, ipl, star2, iflag, eventtype, dgeo, atpress, attemp, tret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
/*
|
||
|
* Written by Dieter Koch:
|
||
|
* Fast function for risings and settings of planets, can be used instead of
|
||
|
* swe_rise_trans(), which is much slower.
|
||
|
* For circumpolar and near-circumpolar planets use swe_rise_trans(), or
|
||
|
* generally use it for geographical latitudes higher than 58N/S.
|
||
|
* For fixed stars, swe_rise_trans() is fast enough.
|
||
|
*/
|
||
|
static int32 calc_rise_and_set(double tjd_start, int32 ipl, double *dgeo, double *datm, int32 eventflag, int32 helflag, double *trise, char *serr)
|
||
|
{
|
||
|
int retc = OK, i;
|
||
|
double sda, xs[6], xx[6], xaz[6], xaz2[6], dfac = 1/365.25;
|
||
|
double rdi, rh;
|
||
|
double tjd0 = tjd_start, tjdrise;
|
||
|
double tjdnoon = (int) tjd0 - dgeo[0] / 15.0 / 24.0;
|
||
|
int32 iflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
iflag |= SEFLG_EQUATORIAL;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT|SEFLG_TRUEPOS;
|
||
|
if (swe_calc_ut(tjd0, SE_SUN, iflag, xs, serr) == 0) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error in calc_rise_and_set(): calc(sun) failed ");
|
||
|
return ERR;
|
||
|
}
|
||
|
if (swe_calc_ut(tjd0, ipl, iflag, xx, serr) == 0) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error in calc_rise_and_set(): calc(sun) failed ");
|
||
|
return ERR;
|
||
|
}
|
||
|
tjdnoon -= swe_degnorm(xs[0] - xx[0])/360.0 + 0;
|
||
|
/* is planet above horizon or below? */
|
||
|
swe_azalt(tjd0, SE_EQU2HOR, dgeo, datm[0], datm[1], xx, xaz);
|
||
|
if (eventflag & SE_CALC_RISE) {
|
||
|
if (xaz[2] > 0) {
|
||
|
while (tjdnoon - tjd0 < 0.5) {/*printf("e");*/tjdnoon += 1;}
|
||
|
while (tjdnoon - tjd0 > 1.5) {/*printf("f");*/tjdnoon -= 1;}
|
||
|
} else {
|
||
|
while (tjdnoon - tjd0 < 0.0) {/*printf("g");*/tjdnoon += 1;}
|
||
|
while (tjdnoon - tjd0 > 1.0) {/*printf("h");*/tjdnoon -= 1;}
|
||
|
}
|
||
|
} else {
|
||
|
if (xaz[2] > 0) {
|
||
|
while (tjd0 - tjdnoon > 0.5) {/*printf("a");*/ tjdnoon += 1;}
|
||
|
while (tjd0 - tjdnoon < -0.5) {/*printf("b");*/ tjdnoon -= 1;}
|
||
|
} else {
|
||
|
while (tjd0 - tjdnoon > 0.0) {/*printf("c");*/ tjdnoon += 1;}
|
||
|
while (tjd0 - tjdnoon < -1.0) {/*printf("d");*/ tjdnoon -= 1;}
|
||
|
}
|
||
|
}
|
||
|
/* position of planet */
|
||
|
if (swe_calc_ut(tjdnoon, ipl, iflag, xx, serr) == ERR) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error in calc_rise_and_set(): calc(sun) failed ");
|
||
|
return ERR;
|
||
|
}
|
||
|
/* apparent radius of solar disk (ignoring refraction) */
|
||
|
rdi = asin(696000000.0 / 1.49597870691e+11 / xx[2]) / DEGTORAD;
|
||
|
if (eventflag & SE_BIT_DISC_CENTER)
|
||
|
rdi = 0;
|
||
|
/* true altitude of sun, when it appears at the horizon */
|
||
|
/* refraction for a body visible at the horizon at 0m above sea,
|
||
|
* atmospheric temperature 10 deg C, atmospheric pressure 1013.25 is 34.5 arcmin*/
|
||
|
rh = -(34.5 / 60.0 + rdi);
|
||
|
/* semidiurnal arc of sun */
|
||
|
sda = acos(-tan(dgeo[1] * DEGTORAD) * tan(xx[1] * DEGTORAD)) * RADTODEG;
|
||
|
/* rough rising and setting times */
|
||
|
if (eventflag & SE_CALC_RISE)
|
||
|
tjdrise = tjdnoon - sda / 360.0;
|
||
|
else
|
||
|
tjdrise = tjdnoon + sda / 360.0;
|
||
|
/*ph->tset = tjd_start + sda / 360.0;*/
|
||
|
/* now calculate more accurate rising and setting times.
|
||
|
* use vertical speed in order to determine crossing of the horizon
|
||
|
* refraction of 34' and solar disk diameter of 16' = 50' = 0.84 deg */
|
||
|
iflag = SEFLG_SPEED|SEFLG_EQUATORIAL;
|
||
|
if (ipl == SE_MOON)
|
||
|
iflag |= SEFLG_TOPOCTR;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT|SEFLG_TRUEPOS;
|
||
|
for (i = 0; i < 2; i++) {
|
||
|
if (swe_calc_ut(tjdrise, ipl, iflag, xx, serr) == ERR)
|
||
|
return ERR;
|
||
|
swe_azalt(tjdrise, SE_EQU2HOR, dgeo, datm[0], datm[1], xx, xaz);
|
||
|
xx[0] -= xx[3] * dfac;
|
||
|
xx[1] -= xx[4] * dfac;
|
||
|
swe_azalt(tjdrise - dfac, SE_EQU2HOR, dgeo, datm[0], datm[1], xx, xaz2);
|
||
|
tjdrise -= (xaz[1] - rh) / (xaz[1] - xaz2[1]) * dfac;
|
||
|
/*fprintf(stderr, "%f\n", ph->trise);*/
|
||
|
}
|
||
|
*trise = tjdrise;
|
||
|
return retc;
|
||
|
}
|
||
|
|
||
|
static int32 my_rise_trans(double tjd, int32 ipl, char* starname, int32 eventtype, int32 helflag, double *dgeo, double *datm, double *tret, char *serr)
|
||
|
{
|
||
|
int retc = OK;
|
||
|
if (starname != NULL && *starname != '\0')
|
||
|
ipl = DeterObject(starname);
|
||
|
/* for non-circumpolar planets we can use a faster algorithm */
|
||
|
/*if (!(helflag & SE_HELFLAG_HIGH_PRECISION) && ipl != -1 && fabs(dgeo[1]) < 58) {*/
|
||
|
if (ipl != -1 && fabs(dgeo[1]) < 63) {
|
||
|
retc = calc_rise_and_set(tjd, ipl, dgeo, datm, eventtype, helflag, tret, serr);
|
||
|
/* for stars and circumpolar planets we use a rigorous algorithm */
|
||
|
} else {
|
||
|
retc = call_swe_rise_trans(tjd, ipl, starname, helflag, eventtype, dgeo, datm[0], datm[1], tret, serr);
|
||
|
}
|
||
|
/* printf("%f, %f\n", tjd, *tret);*/
|
||
|
return retc;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [Days]
|
||
|
' dgeo [array: longitude, latitude, eye height above sea m]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' ObjectName (string)
|
||
|
' RSEvent (1=rise, 2=set,3=up transit,4=down transit)
|
||
|
' Rim [0=center,1=top]
|
||
|
' RiseSet [Day]
|
||
|
*/
|
||
|
static int32 RiseSet(double JDNDaysUT, double *dgeo, double *datm, char *ObjectName, int32 RSEvent, int32 helflag, int32 Rim, double *tret, char *serr)
|
||
|
{
|
||
|
int32 eventtype = RSEvent, Planet, retval;
|
||
|
if (Rim == 0)
|
||
|
eventtype |= SE_BIT_DISC_CENTER;
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
if (Planet != -1)
|
||
|
retval = my_rise_trans(JDNDaysUT, Planet, "", eventtype, helflag, dgeo, datm, tret, serr);
|
||
|
else
|
||
|
retval = my_rise_trans(JDNDaysUT, -1, ObjectName, eventtype, helflag, dgeo, datm, tret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [Days]
|
||
|
' actual [0= approximation, 1=actual]
|
||
|
' SunRA [deg]
|
||
|
*/
|
||
|
static double SunRA(double JDNDaysUT, int32 helflag, char *serr)
|
||
|
{
|
||
|
int imon, iday, iyar, calflag = SE_GREG_CAL;
|
||
|
double dut;
|
||
|
static double tjdlast;
|
||
|
static double ralast;
|
||
|
if (JDNDaysUT == tjdlast)
|
||
|
return ralast;
|
||
|
#ifndef SIMULATE_VICTORVB
|
||
|
if (1) { /*helflag & SE_HELFLAG_HIGH_PRECISION) {*/
|
||
|
double tjd_tt;
|
||
|
double x[6];
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
int32 iflag = epheflag | SEFLG_EQUATORIAL;
|
||
|
iflag |= SEFLG_NONUT | SEFLG_TRUEPOS;
|
||
|
tjd_tt = JDNDaysUT + swe_deltat(JDNDaysUT);
|
||
|
if (swe_calc(tjd_tt, SE_SUN, iflag, x, serr) != ERR) {
|
||
|
ralast = x[0];
|
||
|
tjdlast = JDNDaysUT;
|
||
|
return ralast;
|
||
|
}
|
||
|
}
|
||
|
#endif
|
||
|
swe_revjul(JDNDaysUT, calflag, &iyar, &imon, &iday, &dut); /* this seems to be much faster than calling swe_revjul() ! Note: only because SunRA is called 1000s of times */
|
||
|
tjdlast = JDNDaysUT;
|
||
|
ralast = swe_degnorm((imon + (iday - 1) / 30.4 - 3.69) * 30);
|
||
|
/*ralast = (DatefromJDut(JDNDaysUT, 2) + (DatefromJDut(JDNDaysUT, 3) - 1) / 30.4 - 3.69) * 30;*/
|
||
|
return ralast;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Temp [C]
|
||
|
' Kelvin [K]
|
||
|
*/
|
||
|
static double Kelvin(double Temp)
|
||
|
{
|
||
|
/*' http://en.wikipedia.org/wiki/Kelvin*/
|
||
|
return Temp + C2K;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AppAlt [deg]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' TopoAltitudefromAppAlt [deg]
|
||
|
*/
|
||
|
static double TopoAltfromAppAlt(double AppAlt, double TempE, double PresE)
|
||
|
{
|
||
|
double R = 0;
|
||
|
double retalt = 0;
|
||
|
if (AppAlt >= LowestAppAlt) {
|
||
|
if (AppAlt > 17.904104638432)
|
||
|
R = 0.97 / tan(AppAlt * DEGTORAD);
|
||
|
else
|
||
|
R = (34.46 + 4.23 * AppAlt + 0.004 * AppAlt * AppAlt) / (1 + 0.505 * AppAlt + 0.0845 * AppAlt * AppAlt);
|
||
|
R = (PresE - 80) / 930 / (1 + 0.00008 * (R + 39) * (TempE - 10)) * R;
|
||
|
retalt = AppAlt - R * Min2Deg;
|
||
|
} else {
|
||
|
retalt = AppAlt;
|
||
|
}
|
||
|
return retalt;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' TopoAlt [deg]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' AppAltfromTopoAlt [deg]
|
||
|
' call this instead of swe_azalt(), because it is faster (lower precision
|
||
|
' is required)
|
||
|
*/
|
||
|
static double AppAltfromTopoAlt(double TopoAlt, double TempE, double PresE, int32 helflag)
|
||
|
{
|
||
|
/* using methodology of Newtown derivatives (analogue to what Swiss Emphemeris uses)*/
|
||
|
int i, nloop = 2;
|
||
|
double newAppAlt = TopoAlt;
|
||
|
double newTopoAlt = 0.0;
|
||
|
double oudAppAlt = newAppAlt;
|
||
|
double oudTopoAlt = newTopoAlt;
|
||
|
double verschil, retalt;
|
||
|
if (helflag & SE_HELFLAG_HIGH_PRECISION)
|
||
|
nloop = 5;
|
||
|
for (i = 0; i <= nloop; i++) {
|
||
|
newTopoAlt = newAppAlt - TopoAltfromAppAlt(newAppAlt, TempE, PresE);
|
||
|
/*newTopoAlt = newAppAlt - swe_refrac(newAppAlt, PresE, TempE, SE_CALC_APP_TO_TRUE);*/
|
||
|
verschil = newAppAlt - oudAppAlt;
|
||
|
oudAppAlt = newTopoAlt - oudTopoAlt - verschil;
|
||
|
if ((verschil != 0) && (oudAppAlt != 0))
|
||
|
verschil = newAppAlt - verschil * (TopoAlt + newTopoAlt - newAppAlt) / oudAppAlt;
|
||
|
else
|
||
|
verschil = TopoAlt + newTopoAlt;
|
||
|
oudAppAlt = newAppAlt;
|
||
|
oudTopoAlt = newTopoAlt;
|
||
|
newAppAlt = verschil;
|
||
|
}
|
||
|
retalt = TopoAlt + newTopoAlt;
|
||
|
if (retalt < LowestAppAlt)
|
||
|
retalt = TopoAlt;
|
||
|
return retalt;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' TopoAlt [deg]
|
||
|
' TopoDecl [deg]
|
||
|
' Lat [deg]
|
||
|
' HourAngle [hour]
|
||
|
*/
|
||
|
static double HourAngle(double TopoAlt, double TopoDecl, double Lat)
|
||
|
{
|
||
|
double Alti = TopoAlt * DEGTORAD;
|
||
|
double decli = TopoDecl * DEGTORAD;
|
||
|
double Lati = Lat * DEGTORAD;
|
||
|
double ha = (sin(Alti) - sin(Lati) * sin(decli)) / cos(Lati) / cos(decli);
|
||
|
if (ha < -1) ha = -1;
|
||
|
if (ha > 1) ha = 1;
|
||
|
/* from http://star-www.st-and.ac.uk/~fv/webnotes/chapt12.htm*/
|
||
|
return acos(ha) / DEGTORAD / 15.0;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDays [Days]
|
||
|
' COD [msec/cy]
|
||
|
' DeltaTSE [Sec]
|
||
|
*/
|
||
|
static double DeltaTSE(double JDNDays, int COD)
|
||
|
{
|
||
|
double OffSetYear;
|
||
|
int gregflag = SE_GREG_CAL;
|
||
|
if (StartYear < 1583)
|
||
|
gregflag = SE_JUL_CAL;
|
||
|
/* from Swiss Emphemeris */
|
||
|
if (COD != 0) {
|
||
|
/* Determined by V. Reijs*/
|
||
|
OffSetYear = (swe_julday((int) StartYear, 1, 1, 0, gregflag) - JDNDays) / 365.25;
|
||
|
return (OffSetYear * OffSetYear / 100.0 / 2.0 * COD * Y2D) / 1000.0;
|
||
|
}
|
||
|
return swe_deltat(JDNDays) * D2S;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDays [Day]
|
||
|
' COD [msec/cy]
|
||
|
' DeltaTVR [Sec]
|
||
|
*/
|
||
|
static double DeltaTVR(double JDNDays, int COD)
|
||
|
{
|
||
|
/* Determined by V. Reijs */
|
||
|
double DeltaTVR;
|
||
|
int gregflag = SE_GREG_CAL;
|
||
|
double OffSetYear;
|
||
|
if (StartYear < 1583)
|
||
|
gregflag = SE_JUL_CAL;
|
||
|
OffSetYear = (swe_julday((int) StartYear, 1, 1, 0, gregflag) - JDNDays) / 365.25;
|
||
|
if (COD == 0) {
|
||
|
DeltaTVR = (OffSetYear * OffSetYear / 100.0 / 2.0 * Average + Periodicy / 2.0 / PI * Amplitude * (cos((2 * PI * OffSetYear / Periodicy)) - 1)) * Y2D;
|
||
|
} else {
|
||
|
DeltaTVR = OffSetYear * OffSetYear / 100.0 / 2.0 * COD * Y2D;
|
||
|
}
|
||
|
return DeltaTVR / 1000.0;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDays [Days]
|
||
|
' COD [msec/cy]
|
||
|
' DeltaT [Sec]
|
||
|
*/
|
||
|
static double DeltaT(double JDNDays, int COD)
|
||
|
{
|
||
|
if (USE_DELTA_T_VR)
|
||
|
return DeltaTVR(JDNDays, COD);
|
||
|
return DeltaTSE(JDNDays, COD);
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [Days]
|
||
|
' dgeo [array: longitude, latitude, eye height above sea m]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' ObjectName [-]
|
||
|
' Angle (0 = TopoAlt, 1 = Azi, 2=Topo Declination, 3=Topo Rectascension, 4=AppAlt,5=Geo Declination, 6=Geo Rectascension)
|
||
|
' ObjectLoc [deg]
|
||
|
*/
|
||
|
static int32 ObjectLoc(double JDNDaysUT, double *dgeo, double *datm, char *ObjectName, int32 Angle, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
double x[6], xin[3], xaz[3], tjd_tt;
|
||
|
int32 Planet;
|
||
|
int32 epheflag;
|
||
|
int32 iflag = SEFLG_EQUATORIAL;
|
||
|
epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
iflag |= epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT | SEFLG_TRUEPOS;
|
||
|
if (Angle < 5) iflag = iflag | SEFLG_TOPOCTR;
|
||
|
if (Angle == 7) Angle = 0;
|
||
|
tjd_tt = JDNDaysUT + DeltaT(JDNDaysUT, 0) / D2S;
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
if (Planet != -1) {
|
||
|
if (swe_calc(tjd_tt, Planet, iflag, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
} else {
|
||
|
if (call_swe_fixstar(ObjectName, tjd_tt, iflag, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
if (Angle == 2 || Angle == 5) {
|
||
|
*dret = x[1];
|
||
|
} else {
|
||
|
if (Angle == 3 || Angle == 6) {
|
||
|
*dret = x[0];
|
||
|
} else {
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNDaysUT, SE_EQU2HOR, dgeo, datm[0], datm[1], xin, xaz);
|
||
|
if (Angle == 0)
|
||
|
*dret = xaz[1];
|
||
|
if (Angle == 4)
|
||
|
*dret = AppAltfromTopoAlt(xaz[1], datm[0], datm[1], helflag);
|
||
|
if (Angle == 1) {
|
||
|
xaz[0] += 180;
|
||
|
if (xaz[0] >= 360)
|
||
|
xaz[0] -= 360;
|
||
|
*dret = xaz[0];
|
||
|
}
|
||
|
}
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [Days]
|
||
|
' dgeo [array: longitude, latitude, eye height above sea m]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' ObjectName [-]
|
||
|
' Angle (0 = TopoAlt, 1 = Azi, 2=Topo Declination, 3=Topo Rectascension, 4=AppAlt,5=Geo Declination, 6=Geo Rectascension)
|
||
|
' ObjectLoc [deg]
|
||
|
*/
|
||
|
static int32 azalt_cart(double JDNDaysUT, double *dgeo, double *datm, char *ObjectName, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
double x[6], xin[3], xaz[3], tjd_tt;
|
||
|
int32 Planet;
|
||
|
int32 epheflag;
|
||
|
int32 iflag = SEFLG_EQUATORIAL;
|
||
|
epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
iflag |= epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT | SEFLG_TRUEPOS;
|
||
|
iflag = iflag | SEFLG_TOPOCTR;
|
||
|
tjd_tt = JDNDaysUT + DeltaT(JDNDaysUT, 0) / D2S;
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
if (Planet != -1) {
|
||
|
if (swe_calc(tjd_tt, Planet, iflag, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
} else {
|
||
|
if (call_swe_fixstar(ObjectName, tjd_tt, iflag, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNDaysUT, SE_EQU2HOR, dgeo, datm[0], datm[1], xin, xaz);
|
||
|
dret[0] = xaz[0];
|
||
|
dret[1] = xaz[1]; /* true altitude */
|
||
|
dret[2] = xaz[2]; /* apparent altitude */
|
||
|
/* also return cartesian coordinates, for apparent altitude */
|
||
|
xaz[1] = xaz[2];
|
||
|
xaz[2] = 1;
|
||
|
swi_polcart(xaz, xaz);
|
||
|
dret[3] = xaz[0];
|
||
|
dret[4] = xaz[1];
|
||
|
dret[5] = xaz[2];
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' LatA [rad]
|
||
|
' LongA [rad]
|
||
|
' LatB [rad]
|
||
|
' LongB [rad]
|
||
|
' DistanceAngle [rad]
|
||
|
*/
|
||
|
static double DistanceAngle(double LatA, double LongA, double LatB, double LongB)
|
||
|
{
|
||
|
double dlon = LongB - LongA;
|
||
|
double dlat = LatB - LatA;
|
||
|
/* Haversine formula
|
||
|
* http://www.movable-type.co.uk/scripts/GIS-FAQ-5.1.html
|
||
|
* R.W. Sinnott, Virtues of the Haversine, Sky and Telescope, vol. 68, no. 2, 1984, p. 159
|
||
|
*/
|
||
|
double sindlat2 = sin(dlat / 2);
|
||
|
double sindlon2 = sin(dlon / 2);
|
||
|
double corde = sindlat2 * sindlat2 + cos(LatA) * cos(LatB) * sindlon2 *sindlon2;
|
||
|
if (corde > 1) corde = 1;
|
||
|
return 2 * asin(sqrt(corde));
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' RH [%]
|
||
|
' kW [-]
|
||
|
*/
|
||
|
static double kW(double HeightEye, double TempS, double RH)
|
||
|
{
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128*/
|
||
|
double WT = 0.031;
|
||
|
WT *= 0.94 * (RH / 100.0) * exp(TempS / 15) * exp(-1 * HeightEye / scaleHwater);
|
||
|
return WT;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' lat [deg]
|
||
|
' kOZ [-]
|
||
|
*/
|
||
|
static double kOZ(double AltS, double sunra, double Lat)
|
||
|
{
|
||
|
double CHANGEKO, OZ, LT, kOZret;
|
||
|
static double koz_last, alts_last, sunra_last;
|
||
|
if (AltS == alts_last && sunra == sunra_last)
|
||
|
return koz_last;
|
||
|
alts_last = AltS; sunra_last = sunra;
|
||
|
OZ = 0.031;
|
||
|
LT = Lat * DEGTORAD;
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128*/
|
||
|
kOZret = OZ * (3.0 + 0.4 * (LT * cos(sunra * DEGTORAD) - cos(3 * LT))) / 3.0;
|
||
|
/* depending on day/night vision (altitude of sun < start astronomical twilight), KO changes from 100% to 30%
|
||
|
* see extinction section of Vistas in Astronomy page 343*/
|
||
|
CHANGEKO = (100 - 11.6 * mymin(6, mymax(-AltS - 12, 0))) / 100;
|
||
|
koz_last = kOZret * CHANGEKO;
|
||
|
return koz_last;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AltS [deg]
|
||
|
' heighteye [m]
|
||
|
' kR [-]
|
||
|
*/
|
||
|
static double kR(double AltS, double HeightEye)
|
||
|
{
|
||
|
/* depending on day/night vision (altitude of sun < start astronomical twilight),
|
||
|
* lambda eye sensibility changes
|
||
|
* see extinction section of Vistas in Astronomy page 343*/
|
||
|
double CHANGEK, LAMBDA;
|
||
|
double val = -AltS - 12;
|
||
|
if (val < 0) val = 0;
|
||
|
if (val > 6) val = 6;
|
||
|
/*CHANGEK = (1 - 0.166667 * Min(6, Max(-AltS - 12, 0)));*/
|
||
|
CHANGEK = (1 - 0.166667 * val );
|
||
|
LAMBDA = 0.55 + (CHANGEK - 1) * 0.04;
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128 */
|
||
|
return 0.1066 * exp(-1 * HeightEye / scaleHrayleigh) * pow(LAMBDA / 0.55 , -4);
|
||
|
}
|
||
|
|
||
|
static int Sgn(double x)
|
||
|
{
|
||
|
if (x < 0)
|
||
|
return -1;
|
||
|
return 1;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' ka [-]
|
||
|
*/
|
||
|
static double ka(double AltS, double sunra, double Lat, double HeightEye, double TempS, double RH, double VR, char *serr)
|
||
|
{
|
||
|
double CHANGEKA, LAMBDA, BetaVr, Betaa, kaact;
|
||
|
double SL = Sgn(Lat);
|
||
|
/* depending on day/night vision (altitude of sun < start astronomical twilight),
|
||
|
* lambda eye sensibility changes
|
||
|
* see extinction section of Vistas in Astronomy page 343 */
|
||
|
static double alts_last, sunra_last, ka_last;
|
||
|
if (AltS == alts_last && sunra == sunra_last)
|
||
|
return ka_last;
|
||
|
alts_last = AltS; sunra_last = sunra;
|
||
|
CHANGEKA = (1 - 0.166667 * mymin(6, mymax(-AltS - 12, 0)));
|
||
|
LAMBDA = 0.55 + (CHANGEKA - 1) * 0.04;
|
||
|
if (VR != 0) {
|
||
|
if (VR >= 1) {
|
||
|
/* Visbility range from http://www1.cs.columbia.edu/CAVE/publications/pdfs/Narasimhan_CVPR03.pdf
|
||
|
* http://www.icao.int/anb/SG/AMOSSG/meetings/amossg3/wp/SN11Rev.pdf where MOR=2.995/ke
|
||
|
* factor 1.3 is the relation between "prevailing visibility" and
|
||
|
* meteorological range was derived by Koshmeider in the 1920's */
|
||
|
BetaVr = 3.912 / VR;
|
||
|
Betaa = BetaVr - (kW(HeightEye, TempS, RH) / scaleHwater + kR(AltS, HeightEye) / scaleHrayleigh) * 1000 * astr2tau;
|
||
|
kaact = Betaa * scaleHaerosol / 1000 * tau2astr;
|
||
|
if (kaact < 0) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "The provided Meteorological range is too long, when taking into acount other atmospheric parameters"); /* is a warning */
|
||
|
/* return 0; * return "#HIGHVR"; */
|
||
|
}
|
||
|
} else {
|
||
|
kaact = VR - kW(HeightEye, TempS, RH) - kR(AltS, HeightEye) - kOZ(AltS, sunra, Lat);
|
||
|
if (kaact < 0) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "The provided atmosphic coeefficent (ktot) is too low, when taking into acount other atmospheric parameters"); /* is a warning */
|
||
|
/* return 0; * "#LOWktot"; */
|
||
|
}
|
||
|
}
|
||
|
} else {
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128 */
|
||
|
#ifdef SIMULATE_VICTORVB
|
||
|
if (RH <= 0.00000001) RH = 0.00000001;
|
||
|
if (RH >= 99.99999999) RH = 99.99999999;
|
||
|
#endif
|
||
|
kaact = 0.1 * exp(-1 * HeightEye / scaleHaerosol) * pow(1 - 0.32 / log(RH / 100.0), 1.33) * (1 + 0.33 * SL * sin(sunra * DEGTORAD));
|
||
|
kaact = kaact * pow(LAMBDA / 0.55, -1.3);
|
||
|
}
|
||
|
ka_last = kaact;
|
||
|
return kaact;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' ExtType [0=ka,1=kW,2=kR,3=kOZ,4=ktot]
|
||
|
' kt [-]
|
||
|
*/
|
||
|
static double kt(double AltS, double sunra, double Lat, double HeightEye, double TempS, double RH, double VR, int32 ExtType, char *serr)
|
||
|
{
|
||
|
double kRact = 0;
|
||
|
double kWact = 0;
|
||
|
double kOZact = 0;
|
||
|
double kaact = 0;
|
||
|
if (ExtType == 2 || ExtType == 4)
|
||
|
kRact = kR(AltS, HeightEye);
|
||
|
if (ExtType == 1 || ExtType == 4)
|
||
|
kWact = kW(HeightEye, TempS, RH);
|
||
|
if (ExtType == 3 || ExtType == 4)
|
||
|
kOZact = kOZ(AltS, sunra, Lat);
|
||
|
if (ExtType == 0 || ExtType == 4)
|
||
|
kaact = ka(AltS, sunra, Lat, HeightEye, TempS, RH, VR, serr);
|
||
|
if (kaact < 0)
|
||
|
kaact = 0;
|
||
|
return kWact + kRact + kOZact + kaact;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AppAlt0 [deg]
|
||
|
' PresS [mbar]
|
||
|
' Airmass [??]
|
||
|
*/
|
||
|
static double Airmass(double AppAltO, double Press)
|
||
|
{
|
||
|
double airm, zend;
|
||
|
zend = (90 - AppAltO) * DEGTORAD;
|
||
|
if (zend > PI / 2)
|
||
|
zend = PI / 2;
|
||
|
airm = 1 / (cos(zend) + 0.025 * exp(-11 * cos(zend)));
|
||
|
return Press / 1013 * airm;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' scaleH '[m]
|
||
|
' zend [rad]
|
||
|
' PresS [mbar]
|
||
|
' Xext [-]
|
||
|
*/
|
||
|
static double Xext(double scaleH, double zend, double Press)
|
||
|
{
|
||
|
return Press / 1013.0 / (cos(zend) + 0.01 * sqrt(scaleH / 1000.0) * exp(-30.0 / sqrt(scaleH / 1000.0) * cos(zend)));
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' scaleH '[m]
|
||
|
' zend [rad]
|
||
|
' PresS [mbar]
|
||
|
' Xlay [-]
|
||
|
*/
|
||
|
static double Xlay(double scaleH, double zend, double Press)
|
||
|
{
|
||
|
/*return Press / 1013.0 / sqrt(1.0 - pow(sin(zend) / (1.0 + (scaleH / Ra)), 2));*/
|
||
|
double a = sin(zend) / (1.0 + (scaleH / Ra));
|
||
|
return Press / 1013.0 / sqrt(1.0 - a * a);
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Meteorological formula
|
||
|
'###################################################################
|
||
|
' TempS [C]
|
||
|
' HeightEye [m]
|
||
|
' TempEfromTempS [C]
|
||
|
*/
|
||
|
static double TempEfromTempS(double TempS, double HeightEye, double Lapse)
|
||
|
{
|
||
|
return TempS - Lapse * HeightEye;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' TempS [C]
|
||
|
' PresS [mbar]
|
||
|
' HeightEye [m]
|
||
|
' PresEfromPresS [mbar]
|
||
|
*/
|
||
|
static double PresEfromPresS(double TempS, double Press, double HeightEye)
|
||
|
{
|
||
|
return Press * exp(-9.80665 * 0.0289644 / (Kelvin(TempS) + 3.25 * HeightEye / 1000) / 8.31441 * HeightEye);
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AltO [deg]
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' PresS [mbar]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' Deltam [-]
|
||
|
*/
|
||
|
static double Deltam(double AltO, double AltS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double zend, xR, XW, Xa, XOZ;
|
||
|
double PresE = PresEfromPresS(datm[1], datm[0], HeightEye);
|
||
|
double TempE = TempEfromTempS(datm[1], HeightEye, LapseSA);
|
||
|
double AppAltO = AppAltfromTopoAlt(AltO, TempE, PresE, helflag);
|
||
|
double deltam;
|
||
|
static double alts_last, alto_last, sunra_last, deltam_last;
|
||
|
if (AltS == alts_last && AltO == alto_last && sunra == sunra_last)
|
||
|
return deltam_last;
|
||
|
alts_last = AltS; alto_last = AltO; sunra_last = sunra;
|
||
|
if (staticAirmass == 0) {
|
||
|
zend = (90 - AppAltO) * DEGTORAD;
|
||
|
if (zend > PI / 2)
|
||
|
zend = PI / 2;
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128*/
|
||
|
xR = Xext(scaleHrayleigh, zend, datm[0]);
|
||
|
XW = Xext(scaleHwater, zend, datm[0]);
|
||
|
Xa = Xext(scaleHaerosol, zend, datm[0]);
|
||
|
XOZ = Xlay(scaleHozone, zend, datm[0]);
|
||
|
deltam = kR(AltS, HeightEye) * xR + kt(AltS, sunra, Lat, HeightEye, datm[1], datm[2], datm[3], 0, serr) * Xa + kOZ(AltS, sunra, Lat) * XOZ + kW(HeightEye, datm[1], datm[2]) * XW;
|
||
|
} else {
|
||
|
deltam = kt(AltS, sunra, Lat, HeightEye, datm[1], datm[2], datm[3], 4, serr) * Airmass(AppAltO, datm[0]);
|
||
|
}
|
||
|
deltam_last = deltam;
|
||
|
return deltam;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AltO [deg]
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' PresS [mbar]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' Bn [nL]
|
||
|
*/
|
||
|
static double Bn(double AltO, double JDNDayUT, double AltS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double PresE = PresEfromPresS(datm[1], datm[0], HeightEye);
|
||
|
double TempE = TempEfromTempS(datm[1], HeightEye, LapseSA);
|
||
|
double AppAltO = AppAltfromTopoAlt(AltO, TempE, PresE, helflag);
|
||
|
double zend, YearB, MonthB, DayB, Bna, kX, Bnb;
|
||
|
double B0 = 0.0000000000001, dut;
|
||
|
int iyar, imon, iday;
|
||
|
/* Below altitude of 10 degrees, the Bn stays the same (see page 343 Vistas in Astronomy) */
|
||
|
if (AppAltO < 10)
|
||
|
AppAltO = 10;
|
||
|
zend = (90 - AppAltO) * DEGTORAD;
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 128 and adjusted for sunspot period*/
|
||
|
/*YearB = DatefromJDut(JDNDayUT, 1);
|
||
|
MonthB = DatefromJDut(JDNDayUT, 2);
|
||
|
DayB = DatefromJDut(JDNDayUT, 3);*/
|
||
|
swe_revjul(JDNDayUT, SE_GREG_CAL, &iyar, &imon, &iday, &dut);
|
||
|
YearB = iyar; MonthB = imon; DayB = iday;
|
||
|
Bna = B0 * (1 + 0.3 * cos(6.283 * (YearB + ((DayB - 1) / 30.4 + MonthB - 1) / 12 - 1990.33) / 11.1));
|
||
|
kX = Deltam(AltO, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 129 */
|
||
|
Bnb = Bna * (0.4 + 0.6 / sqrt(1 - 0.96 * pow(sin(zend), 2))) * pow(10, -0.4 * kX);
|
||
|
return mymax(Bnb, 0) * erg2nL;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [-]
|
||
|
' dgeo [array: longitude, latitude, eye height above sea m]
|
||
|
' TempE [C]
|
||
|
' PresE [mbar]
|
||
|
' ObjectName [-]
|
||
|
' Magnitude [-]
|
||
|
*/
|
||
|
static int32 Magnitude(double JDNDaysUT, double *dgeo, char *ObjectName, int32 helflag, double *dmag, char *serr)
|
||
|
{
|
||
|
double x[20];
|
||
|
int32 Planet, iflag, epheflag;
|
||
|
epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
*dmag = -99.0;
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
iflag = SEFLG_TOPOCTR | SEFLG_EQUATORIAL | epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT|SEFLG_TRUEPOS;
|
||
|
if (Planet != -1) {
|
||
|
/**dmag = Phenomena(JDNDaysUT, Lat, Longitude, HeightEye, TempE, PresE, ObjectName, 4);*/
|
||
|
swe_set_topo(dgeo[0], dgeo[1], dgeo[2]);
|
||
|
if (swe_pheno_ut(JDNDaysUT, Planet, iflag, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
*dmag = x[4];
|
||
|
} else {
|
||
|
if (call_swe_fixstar_mag(ObjectName, dmag, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
static int32 fast_magnitude(double tjd, double *dgeo, char *ObjectName, int32 helflag, double *dmag, char *serr)
|
||
|
{
|
||
|
int32 retval = OK, ipl, ipli;
|
||
|
double dtjd;
|
||
|
static double tjdsv[3];
|
||
|
static double dmagsv[3];
|
||
|
static int32 helflagsv[3];
|
||
|
ipl = DeterObject(ObjectName);
|
||
|
ipli = ipl;
|
||
|
if (ipli > SE_MOON)
|
||
|
ipli = 2;
|
||
|
dtjd = tjd - tjdsv[ipli];
|
||
|
if (tjdsv[ipli] != 0 && helflag == helflagsv[ipli] && fabs(dtjd) < 5.0 / 1440.0) {
|
||
|
*dmag = dmagsv[ipli];
|
||
|
} else {
|
||
|
retval = Magnitude(tjd, dgeo, ObjectName, helflag, dmag, serr);
|
||
|
tjdsv[ipli] = tjd;
|
||
|
helflagsv[ipli] = helflag;
|
||
|
dmagsv[ipli] = *dmag;
|
||
|
}
|
||
|
return retval;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
/*###################################################################
|
||
|
' dist [km]
|
||
|
' phasemoon [-]
|
||
|
' MoonsBrightness [-]
|
||
|
*/
|
||
|
static double MoonsBrightness(double dist, double phasemoon)
|
||
|
{
|
||
|
double log10 = 2.302585092994;
|
||
|
/*Moon's brightness changes with distance: http://hem.passagen.se/pausch/comp/ppcomp.html#15 */
|
||
|
return -21.62 + 5 * log(dist / (Ra / 1000)) / log10 + 0.026 * fabs(phasemoon) + 0.000000004 * pow(phasemoon, 4);
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AltM [deg]
|
||
|
' AziM [deg]
|
||
|
' AziS [deg]
|
||
|
' MoonPhase [deg]
|
||
|
*/
|
||
|
static double MoonPhase(double AltM, double AziM, double AziS)
|
||
|
{
|
||
|
double AltMi = AltM * DEGTORAD;
|
||
|
double AziMi = AziM * DEGTORAD;
|
||
|
double AziSi = AziS * DEGTORAD;
|
||
|
return 180 - acos(cos(AziSi - AziMi) * cos(AltMi + 0.95 * DEGTORAD)) / DEGTORAD;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Pressure [mbar]
|
||
|
*/
|
||
|
static double Bm(double AltO, double AziO, double AltM, double AziM, double AltS, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double M0 = -11.05;
|
||
|
double Bm = 0;
|
||
|
double RM, kXM, kX, C3, FM, phasemoon, MM;
|
||
|
if (AltM > -0.26) {
|
||
|
/* moon only adds light when (partly) above horizon
|
||
|
* From Schaefer , Archaeoastronomy, XV, 2000, page 129*/
|
||
|
RM = DistanceAngle(AltO * DEGTORAD, AziO * DEGTORAD, AltM * DEGTORAD, AziM * DEGTORAD) / DEGTORAD;
|
||
|
kXM = Deltam(AltM, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
kX = Deltam(AltO, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
C3 = pow(10, -0.4 * kXM);
|
||
|
FM = (62000000.0) / RM / RM + pow(10, 6.15 - RM / 40) + pow(10, 5.36) * (1.06 + pow(cos(RM * DEGTORAD), 2));
|
||
|
Bm = FM * C3 + 440000 * (1 - C3);
|
||
|
phasemoon = MoonPhase(AltM, AziM, AziS);
|
||
|
MM = MoonsBrightness(MoonDistance, phasemoon);
|
||
|
Bm = Bm * pow(10, -0.4 * (MM - M0 + 43.27));
|
||
|
Bm = Bm * (1 - pow(10, -0.4 * kX));
|
||
|
}
|
||
|
Bm = mymax(Bm, 0) * erg2nL;
|
||
|
return Bm;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Pressure [mbar]
|
||
|
*/
|
||
|
static double Btwi(double AltO, double AziO, double AltS, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double M0 = -11.05;
|
||
|
double MS = -26.74;
|
||
|
double PresE = PresEfromPresS(datm[1], datm[0], HeightEye);
|
||
|
double TempE = TempEfromTempS(datm[1], HeightEye, LapseSA);
|
||
|
double AppAltO = AppAltfromTopoAlt(AltO, TempE, PresE, helflag);
|
||
|
double ZendO = 90 - AppAltO;
|
||
|
double RS = DistanceAngle(AltO * DEGTORAD, AziO * DEGTORAD, AltS * DEGTORAD, AziS * DEGTORAD) / DEGTORAD;
|
||
|
double kX = Deltam(AltO, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
double k = kt(AltS, sunra, Lat, HeightEye, datm[1], datm[2], datm[3], 4, serr);
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 129*/
|
||
|
double Btwi = pow(10, -0.4 * (MS - M0 + 32.5 - AltS - (ZendO / (360 * k))));
|
||
|
Btwi = Btwi * (100 / RS) * (1 - pow(10, -0.4 * kX));
|
||
|
Btwi = mymax(Btwi, 0) * erg2nL;
|
||
|
return Btwi;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Pressure [mbar]
|
||
|
*/
|
||
|
static double Bday(double AltO, double AziO, double AltS, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double M0 = -11.05;
|
||
|
double MS = -26.74;
|
||
|
double RS = DistanceAngle(AltO * DEGTORAD, AziO * DEGTORAD, AltS * DEGTORAD, AziS * DEGTORAD) / DEGTORAD;
|
||
|
double kXS = Deltam(AltS, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
double kX = Deltam(AltO, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 129*/
|
||
|
double C4 = pow(10, -0.4 * kXS);
|
||
|
double FS = (62000000.0) / RS / RS + pow(10, (6.15 - RS / 40)) + pow(10, 5.36) * (1.06 + pow(cos(RS * DEGTORAD), 2));
|
||
|
double Bday = FS * C4 + 440000.0 * (1 - C4);
|
||
|
Bday = Bday * pow(10, (-0.4 * (MS - M0 + 43.27)));
|
||
|
Bday = Bday * (1 - pow(10, -0.4 * kX));
|
||
|
Bday = mymax(Bday, 0) * erg2nL;
|
||
|
return Bday;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Value [nL]
|
||
|
' PresS [mbar]
|
||
|
' Bcity [nL]
|
||
|
*/
|
||
|
static double Bcity(double Value, double Press)
|
||
|
{
|
||
|
double Bcity = Value;
|
||
|
Bcity = mymax(Bcity, 0);
|
||
|
return Bcity;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Pressure [mbar]
|
||
|
*/
|
||
|
static double Bsky(double AltO, double AziO, double AltM, double AziM, double JDNDaysUT, double AltS, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, char *serr)
|
||
|
{
|
||
|
double Bsky = 0;
|
||
|
if (AltS < -3) {
|
||
|
Bsky += Btwi(AltO, AziO, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
} else {
|
||
|
if (AltS > 4) {
|
||
|
Bsky += Bday(AltO, AziO, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
} else {
|
||
|
Bsky += mymin(Bday(AltO, AziO, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr), Btwi(AltO, AziO, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr));
|
||
|
}
|
||
|
}
|
||
|
/* if max. Bm [1E7] <5% of Bsky don't add Bm*/
|
||
|
if (Bsky < 200000000.0)
|
||
|
Bsky += Bm(AltO, AziO, AltM, AziM, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
if (AltS <= 0)
|
||
|
Bsky += Bcity(0, datm[0]);
|
||
|
/* if max. Bn [250] <5% of Bsky don't add Bn*/
|
||
|
if (Bsky < 5000)
|
||
|
Bsky = Bsky + Bn(AltO, JDNDaysUT, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
/* if max. Bm [1E7] <5% of Bsky don't add Bm*/
|
||
|
return Bsky;
|
||
|
}
|
||
|
|
||
|
/* default handling:
|
||
|
* 1. datm (atmospheric conditions):
|
||
|
* datm consists of
|
||
|
* [0] atmospheric pressure
|
||
|
* [1] temperature
|
||
|
* [2] relative humidity
|
||
|
* [3] extinction coefficient
|
||
|
* In order to get default values for [0..2], set datm[0] = 0.
|
||
|
* Default values for [1-2] are only provided if [0] == 0.
|
||
|
* [3] defaults outside this function, depending on [0-2].
|
||
|
*
|
||
|
* 2. dobs (observer definition):
|
||
|
* [0] age (default 36)
|
||
|
* [1] Snellen ratio or visual acuity of observer (default 1)
|
||
|
*/
|
||
|
static void default_heliacal_parameters(double *datm, double *dgeo, double *dobs, int helflag)
|
||
|
{
|
||
|
int i;
|
||
|
if (datm[0] <= 0) {
|
||
|
/* estimate atmospheric pressure, according to the
|
||
|
* International Standard Atmosphere (ISA) */
|
||
|
datm[0] = 1013.25 * pow(1 - 0.0065 * dgeo[2] / 288, 5.255);
|
||
|
/* temperature */
|
||
|
if (datm[1] == 0)
|
||
|
datm[1] = 15 - 0.0065 * dgeo[2];
|
||
|
/* relative humidity, independent of atmospheric pressure and altitude */
|
||
|
if (datm[2] == 0)
|
||
|
datm[2] = 40;
|
||
|
/* note: datm[3] / VR defaults outside this function */
|
||
|
} else {
|
||
|
#ifndef SIMULATE_VICTORVB
|
||
|
if (datm[2] <= 0.00000001) datm[2] = 0.00000001;
|
||
|
if (datm[2] >= 99.99999999) datm[2] = 99.99999999;
|
||
|
#endif
|
||
|
}
|
||
|
/* age of observer */
|
||
|
if (dobs[0] == 0)
|
||
|
dobs[0] = 36;
|
||
|
/* SN Snellen factor of the visual acuity of the observer */
|
||
|
if (dobs[1] == 0)
|
||
|
dobs[1] = 1;
|
||
|
if (!(helflag & SE_HELFLAG_OPTICAL_PARAMS)) {
|
||
|
for (i = 2; i <= 5; i++)
|
||
|
dobs[i] = 0;
|
||
|
}
|
||
|
/* OpticMagn undefined -> use eye */
|
||
|
if (dobs[3] == 0) {
|
||
|
dobs[2] = 1; /* Binocular = 1 */
|
||
|
dobs[3] = 1; /* OpticMagn = 1: use eye */
|
||
|
/* dobs[4] and dobs[5] (OpticDia and OpticTrans) will be defaulted in
|
||
|
* OpticFactor() */
|
||
|
}
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' age [Year]
|
||
|
' SN [-]
|
||
|
' AltO [deg]
|
||
|
' AziO [deg]
|
||
|
' AltM [deg]
|
||
|
' AziM [deg]
|
||
|
' MoonDistance [km]
|
||
|
' JDNDaysUT [-]
|
||
|
' AltS [deg]
|
||
|
' AziS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' TempS [C]
|
||
|
' PresS [mbar]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' VisLimMagn [-]
|
||
|
*/
|
||
|
static double VisLimMagn(double *dobs, double AltO, double AziO, double AltM, double AziM, double JDNDaysUT, double AltS, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, int32 *scotopic_flag, char *serr)
|
||
|
{
|
||
|
double C1, C2, Th, kX, Bsk, CorrFactor1, CorrFactor2;
|
||
|
double log10 = 2.302585092994;
|
||
|
/*double Age = dobs[0];*/
|
||
|
/*double SN = dobs[1];*/
|
||
|
Bsk = Bsky(AltO, AziO, AltM, AziM, JDNDaysUT, AltS, AziS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
/* Schaefer, Astronomy and the limits of vision, Archaeoastronomy, 1993 Verder:*/
|
||
|
kX = Deltam(AltO, AltS, sunra, Lat, HeightEye, datm, helflag, serr);
|
||
|
/* influence of age*/
|
||
|
/*Fa = mymax(1, pow(p(23, Bsk) / p(Age, Bsk), 2)); */
|
||
|
CorrFactor1 = OpticFactor(Bsk, kX, dobs, JDNDaysUT, "", 1, helflag);
|
||
|
CorrFactor2 = OpticFactor(Bsk, kX, dobs, JDNDaysUT, "", 0, helflag);
|
||
|
/* From Schaefer , Archaeoastronomy, XV, 2000, page 129*/
|
||
|
if (Bsk < BNIGHT && !(helflag & SE_HELFLAG_VISLIM_PHOTOPIC)) {
|
||
|
C1 = 1.5848931924611e-10; /*pow(10, -9.8);*/ /* C1 = 10 ^ (-9.8);*/
|
||
|
C2 = 0.012589254117942; /*pow(10, -1.9);*/ /* C2 = 10 ^ (-1.9);*/
|
||
|
if (scotopic_flag != NULL)
|
||
|
*scotopic_flag = 1;
|
||
|
} else {
|
||
|
C1 = 4.4668359215096e-9; /*pow(10, -8.35);*/ /* C1 = 10 ^ (-8.35);*/
|
||
|
C2 = 1.2589254117942e-6; /*pow(10, -5.9);*/ /* C2 = 10 ^ (-5.9);*/
|
||
|
if (scotopic_flag != NULL)
|
||
|
*scotopic_flag = 0;
|
||
|
}
|
||
|
if (scotopic_flag != NULL) {
|
||
|
if (BNIGHT * BNIGHT_FACTOR > Bsk && BNIGHT / BNIGHT_FACTOR < Bsk)
|
||
|
*scotopic_flag |= 2;
|
||
|
}
|
||
|
/*Th = C1 * pow(1 + sqrt(C2 * Bsk), 2) * Fa;*/
|
||
|
Bsk = Bsk / CorrFactor1;
|
||
|
Th = C1 * pow(1 + sqrt(C2 * Bsk), 2) * CorrFactor2;
|
||
|
#if DEBUG
|
||
|
fprintf(stderr, "Bsk=%f\n", Bsk);
|
||
|
fprintf(stderr, "kX =%f\n", kX);
|
||
|
fprintf(stderr, "Th =%f\n", Th);
|
||
|
fprintf(stderr, "CorrFactor1=%f\n", CorrFactor1);
|
||
|
fprintf(stderr, "CorrFactor2=%f\n", CorrFactor2);
|
||
|
#endif
|
||
|
/* Visual limiting magnitude of point source*/
|
||
|
#if 0
|
||
|
if (SN <= 0.00000001)
|
||
|
SN = 0.00000001;
|
||
|
return -16.57 - 2.5 * (log(Th) / log10) - kX + 5.0 * (log(SN) / log10);*/
|
||
|
#endif
|
||
|
return -16.57 - 2.5 * (log(Th) / log10);
|
||
|
}
|
||
|
|
||
|
/* Limiting magnitude in dark skies
|
||
|
* function returns:
|
||
|
* -1 Error
|
||
|
* -2 Object is below horizon
|
||
|
* 0 OK, photopic vision
|
||
|
* |1 OK, scotopic vision
|
||
|
* |2 OK, near limit photopic/scotopic
|
||
|
*/
|
||
|
int32 FAR PASCAL_CONV swe_vis_limit_mag(double tjdut, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
int32 retval = OK, i, scotopic_flag = 0;
|
||
|
double AltO, AziO, AltM, AziM, AltS, AziS;
|
||
|
double sunra = SunRA(tjdut, helflag, serr);
|
||
|
default_heliacal_parameters(datm, dgeo, dobs, helflag);
|
||
|
swe_set_topo(dgeo[0], dgeo[1], dgeo[2]);
|
||
|
for (i = 0; i < 7; i++)
|
||
|
dret[i] = 0;
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, ObjectName, 0, helflag, &AltO, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (AltO < 0 && serr != NULL) {
|
||
|
strcpy(serr, "object is below local horizon");
|
||
|
*dret = -100;
|
||
|
return -2;
|
||
|
}
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, ObjectName, 1, helflag, &AziO, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (helflag & SE_HELFLAG_VISLIM_DARK) {
|
||
|
AltS = -90;
|
||
|
AziS = 0;
|
||
|
} else {
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, "sun", 0, helflag, &AltS, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, "sun", 1, helflag, &AziS, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
if (strncmp(ObjectName, "moon", 4) == 0 ||
|
||
|
(helflag & SE_HELFLAG_VISLIM_DARK) ||
|
||
|
(helflag & SE_HELFLAG_VISLIM_NOMOON)
|
||
|
) {
|
||
|
AltM = -90; AziM = 0;
|
||
|
} else {
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, "moon", 0, helflag, &AltM, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(tjdut, dgeo, datm, "moon", 1, helflag, &AziM, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
#if DEBUG
|
||
|
{
|
||
|
int i;
|
||
|
for (i = 0; i < 6;i++)
|
||
|
printf("dobs[%d] = %f\n", i, dobs[i]);
|
||
|
printf("AltO = %.10f, AziO = %.10f\n", AltO, AziO);
|
||
|
printf("AltM = %.10f, AziM = %.10f\n", AltM, AziM);
|
||
|
printf("AltS = %.10f, AziS = %.10f\n", AltS, AziS);
|
||
|
printf("JD = %.10f\n", tjdut);
|
||
|
printf("lat = %f, eyeh = %f\n", dgeo[1], dgeo[2]);
|
||
|
for (i = 0; i < 4;i++)
|
||
|
printf("datm[%d] = %f\n", i, datm[i]);
|
||
|
printf("helflag = %d\n", helflag);
|
||
|
}
|
||
|
#endif
|
||
|
dret[0] = VisLimMagn(dobs, AltO, AziO, AltM, AziM, tjdut, AltS, AziS, sunra, dgeo[1], dgeo[2], datm, helflag, &scotopic_flag, serr);
|
||
|
dret[1] = AltO;
|
||
|
dret[2] = AziO;
|
||
|
dret[3] = AltS;
|
||
|
dret[4] = AziS;
|
||
|
dret[5] = AltM;
|
||
|
dret[6] = AziM;
|
||
|
if (Magnitude(tjdut, dgeo, ObjectName, helflag, &(dret[7]), serr) == ERR)
|
||
|
return ERR;
|
||
|
retval = scotopic_flag;
|
||
|
/*dret[8] = (double) is_scotopic;*/
|
||
|
/*if (*serr != '\0') * in VisLimMagn(), serr is only a warning *
|
||
|
retval = ERR; */
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' Magn [-]
|
||
|
' age [Year]
|
||
|
' SN [-]
|
||
|
' AltO [deg]
|
||
|
' AziO [deg]
|
||
|
' AltM [deg]
|
||
|
' AziM [deg]
|
||
|
' MoonDistance [km]
|
||
|
' JDNDaysUT [-]
|
||
|
' AziS [deg]
|
||
|
' lat [deg]
|
||
|
' heighteye [m]
|
||
|
' Temperature [C]
|
||
|
' Pressure [mbar]
|
||
|
' RH [%]
|
||
|
' VR [km]
|
||
|
' TopoArcVisionis [deg]
|
||
|
*/
|
||
|
static int32 TopoArcVisionis(double Magn, double *dobs, double AltO, double AziO, double AltM, double AziM, double JDNDaysUT, double AziS, double sunra, double Lat, double HeightEye, double *datm, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
double Xm, Ym, AltSi, AziSi;
|
||
|
double xR = 0;
|
||
|
double Xl = 45;
|
||
|
double Yl, Yr;
|
||
|
Yl = Magn - VisLimMagn(dobs, AltO, AziO, AltM, AziM, JDNDaysUT, AltO - Xl, AziS, sunra, Lat, HeightEye, datm, helflag, NULL, serr);
|
||
|
/* if (*serr != '\0') return ERR; * serr is only a warning */
|
||
|
Yr = Magn - VisLimMagn(dobs, AltO, AziO, AltM, AziM, JDNDaysUT, AltO - xR, AziS, sunra, Lat, HeightEye, datm, helflag, NULL, serr);
|
||
|
/* if (*serr != '\0') return ERR; * serr is only a warning */
|
||
|
/* http://en.wikipedia.org/wiki/Bisection_method*/
|
||
|
if ((Yl * Yr) <= 0) {
|
||
|
while(fabs(xR - Xl) > epsilon) {
|
||
|
/*Calculate midpoint of domain*/
|
||
|
Xm = (xR + Xl) / 2.0;
|
||
|
AltSi = AltO - Xm;
|
||
|
AziSi = AziS;
|
||
|
Ym = Magn - VisLimMagn(dobs, AltO, AziO, AltM, AziM, JDNDaysUT, AltSi, AziSi, sunra, Lat, HeightEye, datm, helflag, NULL, serr);
|
||
|
/* if (*serr != '\0') return ERR; * serr is only a warning */
|
||
|
if ((Yl * Ym) > 0) {
|
||
|
/* Throw away left half*/
|
||
|
Xl = Xm;
|
||
|
Yl = Ym;
|
||
|
} else {
|
||
|
/* Throw away right half */
|
||
|
xR = Xm;
|
||
|
Yr = Ym;
|
||
|
}
|
||
|
}
|
||
|
Xm = (xR + Xl) / 2.0;
|
||
|
} else {
|
||
|
Xm = 99;
|
||
|
}
|
||
|
if (Xm < AltO)
|
||
|
Xm = AltO;
|
||
|
*dret = Xm;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
int32 FAR PASCAL_CONV swe_topo_arcus_visionis(double tjdut, double *dgeo, double *datm, double *dobs, int32 helflag, double mag, double azi_obj, double alt_obj, double azi_sun, double azi_moon, double alt_moon, double *dret, char *serr)
|
||
|
{
|
||
|
double sunra = SunRA(tjdut, helflag, serr);
|
||
|
if (serr != NULL && *serr != '\0')
|
||
|
return ERR;
|
||
|
return TopoArcVisionis(mag, dobs, alt_obj, azi_obj, alt_moon, azi_moon, tjdut, azi_sun, sunra, dgeo[1], dgeo[2], datm, helflag, dret, serr);
|
||
|
}
|
||
|
|
||
|
/*###################################################################*/
|
||
|
/*' Magn [-]
|
||
|
' age [Year]
|
||
|
' SN Snellen factor of the visual aquity of the observer
|
||
|
see: http://www.i-see.org/eyecharts.html#make-your-own
|
||
|
' AziO [deg]
|
||
|
' AltM [deg]
|
||
|
' AziM [deg]
|
||
|
' MoonDistance [km]
|
||
|
' JDNDaysUT [-]
|
||
|
' AziS [deg]
|
||
|
' Lat [deg]
|
||
|
' HeightEye [m]
|
||
|
' Temperature [C]
|
||
|
' Pressure [mbar]
|
||
|
' RH [%] relative humidity
|
||
|
' VR [km] Meteorological Range,
|
||
|
see http://www.iol.ie/~geniet/eng/atmoastroextinction.htm
|
||
|
' TypeAngle
|
||
|
' [0=Object's altitude,
|
||
|
' 1=Arcus Visonis (Object's altitude - Sun's altitude),
|
||
|
' 2=Sun's altitude]
|
||
|
' HeliacalAngle [deg]
|
||
|
*/
|
||
|
static int32 HeliacalAngle(double Magn, double *dobs, double AziO, double AltM, double AziM, double JDNDaysUT, double AziS, double *dgeo, double *datm, int32 helflag, double *dangret, char *serr)
|
||
|
{
|
||
|
double x, minx, maxx, xmin, ymin, Xl, xR, Yr, Yl, Xm, Ym, xmd, ymd;
|
||
|
double Arc, DELTAx;
|
||
|
double sunra = SunRA(JDNDaysUT, helflag, serr);
|
||
|
double Lat = dgeo[1];
|
||
|
double HeightEye = dgeo[2];
|
||
|
if (PLSV == 1) {
|
||
|
dangret[0] = criticalangle;
|
||
|
dangret[1] = criticalangle + Magn * 2.492 + 13.447;
|
||
|
dangret[2] = -(Magn * 2.492 + 13.447); /* Magn * 1.1 + 8.9;*/
|
||
|
return OK;
|
||
|
}
|
||
|
minx = 2;
|
||
|
maxx = 20;
|
||
|
xmin = 0;
|
||
|
ymin = 10000;
|
||
|
for (x = minx; x <= maxx; x++) {
|
||
|
if (TopoArcVisionis(Magn, dobs, x, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, Lat, HeightEye, datm, helflag, &Arc, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (Arc < ymin) {
|
||
|
ymin = Arc;
|
||
|
xmin = x;
|
||
|
}
|
||
|
}
|
||
|
Xl = xmin - 1;
|
||
|
xR = xmin + 1;
|
||
|
if (TopoArcVisionis(Magn, dobs, xR, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, Lat, HeightEye, datm, helflag, &Yr, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (TopoArcVisionis(Magn, dobs, Xl, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, Lat, HeightEye, datm, helflag, &Yl, serr) == ERR)
|
||
|
return ERR;
|
||
|
/* http://en.wikipedia.org/wiki/Bisection_method*/
|
||
|
while(fabs(xR - Xl) > 0.1) {
|
||
|
/* Calculate midpoint of domain */
|
||
|
Xm = (xR + Xl) / 2.0;
|
||
|
DELTAx = 0.025;
|
||
|
xmd = Xm + DELTAx;
|
||
|
if (TopoArcVisionis(Magn, dobs, Xm, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, Lat, HeightEye, datm, helflag, &Ym, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (TopoArcVisionis(Magn, dobs, xmd, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, Lat, HeightEye, datm, helflag, &ymd, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (Ym >= ymd) {
|
||
|
/* Throw away left half */
|
||
|
Xl = Xm;
|
||
|
Yl = Ym;
|
||
|
} else {
|
||
|
/*Throw away right half */
|
||
|
xR = Xm;
|
||
|
Yr = Ym;
|
||
|
}
|
||
|
}
|
||
|
Xm = (xR + Xl) / 2.0;
|
||
|
Ym = (Yr + Yl) / 2.0;
|
||
|
dangret[1] = Ym;
|
||
|
dangret[2] = Xm - Ym;
|
||
|
dangret[0] = Xm;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
int32 FAR PASCAL_CONV swe_heliacal_angle(double tjdut, double *dgeo, double *datm, double *dobs, int32 helflag, double mag, double azi_obj, double azi_sun, double azi_moon, double alt_moon, double *dret, char *serr)
|
||
|
{
|
||
|
return HeliacalAngle(mag, dobs, azi_obj, alt_moon, azi_moon, tjdut, azi_sun, dgeo, datm, helflag, dret, serr);
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' AltO [deg]
|
||
|
' AziO [deg]
|
||
|
' AltS [deg]
|
||
|
' AziS [deg]
|
||
|
' parallax [deg]
|
||
|
' WidthMoon [deg]
|
||
|
*/
|
||
|
static double WidthMoon(double AltO, double AziO, double AltS, double AziS, double parallax)
|
||
|
{
|
||
|
/* Yallop 1998, page 3*/
|
||
|
double GeoAltO = AltO + parallax;
|
||
|
return 0.27245 * parallax * (1 + sin(GeoAltO * DEGTORAD) * sin(parallax * DEGTORAD)) * (1 - cos((AltS - GeoAltO) * DEGTORAD) * cos((AziS - AziO) * DEGTORAD));
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' W [deg]
|
||
|
' LengthMoon [deg]
|
||
|
*/
|
||
|
static double LengthMoon(double W, double Diamoon)
|
||
|
{
|
||
|
double Wi, D;
|
||
|
if (Diamoon == 0) Diamoon = AvgRadiusMoon * 2;
|
||
|
Wi = W * 60;
|
||
|
D = Diamoon * 60;
|
||
|
/* Crescent length according: http://calendar.ut.ac.ir/Fa/Crescent/Data/Sultan2005.pdf*/
|
||
|
return (D - 0.3 * (D + Wi) / 2.0 / Wi) / 60.0;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' W [deg]
|
||
|
' GeoARCVact [deg]
|
||
|
' q [-]
|
||
|
*/
|
||
|
static double qYallop(double W, double GeoARCVact)
|
||
|
{
|
||
|
double Wi = W * 60;
|
||
|
return (GeoARCVact - (11.8371 - 6.3226 * Wi + 0.7319 * Wi * Wi - 0.1018 * Wi * Wi * Wi)) / 10;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
'A (0,p)
|
||
|
'B (1,q)
|
||
|
'C (0,r)
|
||
|
'D (1,s)
|
||
|
*/
|
||
|
static double crossing(double A, double B, double C, double D)
|
||
|
{
|
||
|
return (C - A) / ((B - A) - (D - C));
|
||
|
}
|
||
|
|
||
|
/*###################################################################*/
|
||
|
static int32 DeterTAV(double *dobs, double JDNDaysUT, double *dgeo, double *datm, char *ObjectName, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
double Magn, AltO, AziS, AziO, AziM, AltM;
|
||
|
double sunra = SunRA(JDNDaysUT, helflag, serr);
|
||
|
if (Magnitude(JDNDaysUT, dgeo, ObjectName, helflag, &Magn, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(JDNDaysUT, dgeo, datm, ObjectName, 0, helflag, &AltO, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(JDNDaysUT, dgeo, datm, ObjectName, 1, helflag, &AziO, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (strncmp(ObjectName, "moon", 4) == 0) {
|
||
|
AltM = -90;
|
||
|
AziM = 0;
|
||
|
} else {
|
||
|
if (ObjectLoc(JDNDaysUT, dgeo, datm, "moon", 0, helflag, &AltM, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(JDNDaysUT, dgeo, datm, "moon", 1, helflag, &AziM, serr) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
if (ObjectLoc(JDNDaysUT, dgeo, datm, "sun", 1, helflag, &AziS, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (TopoArcVisionis(Magn, dobs, AltO, AziO, AltM, AziM, JDNDaysUT, AziS, sunra, dgeo[1], dgeo[2], datm, helflag, dret, serr) == ERR)
|
||
|
return ERR;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' A y-value at x=1
|
||
|
' B y-value at x=0
|
||
|
' C y-value at x=-1
|
||
|
' x2min minimum for the quadratic function
|
||
|
*/
|
||
|
static double x2min(double A, double B, double C)
|
||
|
{
|
||
|
double term = A + C - 2 * B;
|
||
|
if (term == 0)
|
||
|
return 0;
|
||
|
return -(A - C) / 2.0 / term;
|
||
|
}
|
||
|
|
||
|
|
||
|
/*###################################################################
|
||
|
' A y-value at x=1
|
||
|
' B y-value at x=0
|
||
|
' C y-value at x=-1
|
||
|
' x
|
||
|
' y is y-value of quadratic function
|
||
|
*/
|
||
|
static double funct2(double A, double B, double C, double x)
|
||
|
{
|
||
|
return (A + C - 2 * B) / 2.0 * x * x + (A - C) / 2.0 * x + B;
|
||
|
}
|
||
|
|
||
|
static void strcpy_VBsafe(char *sout, char *sin)
|
||
|
{
|
||
|
char *sp, *sp2;
|
||
|
int iw = 0;
|
||
|
sp = sin;
|
||
|
sp2 = sout;
|
||
|
while((isalnum(*sp) || *sp == ' ' || *sp == '-') && iw < 30) {
|
||
|
*sp2 = *sp;
|
||
|
sp++; sp2++; iw++;
|
||
|
}
|
||
|
*sp2 = '\0';
|
||
|
}
|
||
|
|
||
|
/*###################################################################
|
||
|
' JDNDaysUT [JDN]
|
||
|
' HPheno
|
||
|
'0=AltO [deg] topocentric altitude of object (unrefracted)
|
||
|
'1=AppAltO [deg] apparent altitude of object (refracted)
|
||
|
'2=GeoAltO [deg] geocentric altitude of object
|
||
|
'3=AziO [deg] azimuth of object
|
||
|
'4=AltS [deg] topocentric altitude of Sun
|
||
|
'5=AziS [deg] azimuth of Sun
|
||
|
'6=TAVact [deg] actual topocentric arcus visionis
|
||
|
'7=ARCVact [deg] actual (geocentric) arcus visionis
|
||
|
'8=DAZact [deg] actual difference between object's and sun's azimuth
|
||
|
'9=ARCLact [deg] actual longitude difference between object and sun
|
||
|
'10=kact [-] extinction coefficient
|
||
|
'11=minTAV [deg] smallest topocentric arcus visionis
|
||
|
'12=TfistVR [JDN] first time object is visible, according to VR
|
||
|
'13=TbVR [JDN] optimum time the object is visible, according to VR
|
||
|
'14=TlastVR [JDN] last time object is visible, according to VR
|
||
|
'15=TbYallop[JDN] best time the object is visible, according to Yallop
|
||
|
'16=WMoon [deg] cresent width of moon
|
||
|
'17=qYal [-] q-test value of Yallop
|
||
|
'18=qCrit [-] q-test criterion of Yallop
|
||
|
'19=ParO [deg] parallax of object
|
||
|
'20 Magn [-] magnitude of object
|
||
|
'21=RiseO [JDN] rise/set time of object
|
||
|
'22=RiseS [JDN] rise/set time of sun
|
||
|
'23=Lag [JDN] rise/set time of object minus rise/set time of sun
|
||
|
'24=TvisVR [JDN] visibility duration
|
||
|
'25=LMoon [deg] cresent length of moon
|
||
|
'26=CVAact [deg]
|
||
|
'27=Illum [%] 'new
|
||
|
'28=CVAact [deg] 'new
|
||
|
'29=MSk [-]
|
||
|
*/
|
||
|
int32 FAR PASCAL_CONV swe_heliacal_pheno_ut(double JDNDaysUT, double *dgeo, double *datm, double *dobs, char *ObjectNameIn, int32 TypeEvent, int32 helflag, double *darr, char *serr)
|
||
|
{
|
||
|
double AziS, AltS, AltS2, AziO, AltO, AltO2, GeoAltO, AppAltO, DAZact, TAVact, ParO, MagnO;
|
||
|
double ARCVact, ARCLact, kact, WMoon, LMoon = 0, qYal, qCrit;
|
||
|
double RiseSetO, RiseSetS, Lag, TbYallop, TfirstVR, TlastVR, TbVR;
|
||
|
double MinTAV = 0, MinTAVact, Ta, Tc, TimeStep, TimePointer, MinTAVoud = 0, DeltaAltoud = 0, DeltaAlt, TvisVR, crosspoint;
|
||
|
double OldestMinTAV, extrax, illum;
|
||
|
double elong, attr[30];
|
||
|
double TimeCheck, LocalminCheck;
|
||
|
int32 retval = OK, RS, Planet;
|
||
|
AS_BOOL noriseO = FALSE;
|
||
|
char ObjectName[AS_MAXCH];
|
||
|
double sunra = SunRA(JDNDaysUT, helflag, serr);
|
||
|
int32 iflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
/* note, the fixed stars functions rewrite the star name. The input string
|
||
|
may be too short, so we have to make sure we have enough space */
|
||
|
strcpy_VBsafe(ObjectName, ObjectNameIn);
|
||
|
default_heliacal_parameters(datm, dgeo, dobs, helflag);
|
||
|
swe_set_topo(dgeo[0], dgeo[1], dgeo[2]);
|
||
|
retval = ObjectLoc(JDNDaysUT, dgeo, datm, "sun", 1, helflag, &AziS, serr);
|
||
|
if (retval == OK)
|
||
|
retval = ObjectLoc(JDNDaysUT, dgeo, datm, "sun", 0, helflag, &AltS, serr);
|
||
|
if (retval == OK)
|
||
|
retval = ObjectLoc(JDNDaysUT, dgeo, datm, ObjectName, 1, helflag, &AziO, serr);
|
||
|
if (retval == OK)
|
||
|
retval = ObjectLoc(JDNDaysUT, dgeo, datm, ObjectName, 0, helflag, &AltO, serr);
|
||
|
if (retval == OK)
|
||
|
retval = ObjectLoc(JDNDaysUT, dgeo, datm, ObjectName, 7, helflag, &GeoAltO, serr);
|
||
|
if (retval == ERR)
|
||
|
return ERR;
|
||
|
AppAltO = AppAltfromTopoAlt(AltO, datm[1], datm[0], helflag);
|
||
|
DAZact = AziS - AziO;
|
||
|
TAVact = AltO - AltS;
|
||
|
/*this parallax seems to be somewhat smaller then in Yallop and SkyMap! Needs to be studied*/
|
||
|
ParO = GeoAltO - AltO;
|
||
|
if (Magnitude(JDNDaysUT, dgeo, ObjectName, helflag, &MagnO, serr) == ERR)
|
||
|
return ERR;
|
||
|
ARCVact = TAVact + ParO;
|
||
|
ARCLact = acos(cos(ARCVact * DEGTORAD) * cos(DAZact * DEGTORAD)) / DEGTORAD;
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
if (Planet == -1) {
|
||
|
elong = ARCLact;
|
||
|
illum = 100;
|
||
|
} else {
|
||
|
retval = swe_pheno_ut(JDNDaysUT, Planet, iflag|(SEFLG_TOPOCTR|SEFLG_EQUATORIAL), attr, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
elong = attr[2];
|
||
|
illum = attr[1] * 100;
|
||
|
}
|
||
|
kact = kt(AltS, sunra, dgeo[1], dgeo[2], datm[1], datm[2], datm[3], 4, serr);
|
||
|
if (0) {
|
||
|
darr[26] = kR(AltS, dgeo[2]);
|
||
|
darr[27] = kW(dgeo[2], datm[1], datm[2]);
|
||
|
darr[28] = kOZ(AltS, sunra, dgeo[1]);
|
||
|
darr[29] = ka(AltS, sunra, dgeo[1], dgeo[2], datm[1], datm[2], datm[3], serr);
|
||
|
darr[30] = darr[26] + darr[27] + darr[28] + darr[29];
|
||
|
}
|
||
|
WMoon = 0;
|
||
|
qYal = 0;
|
||
|
qCrit = 0;
|
||
|
LMoon = 0;
|
||
|
if (Planet == SE_MOON) {
|
||
|
WMoon = WidthMoon(AltO, AziO, AltS, AziS, ParO);
|
||
|
LMoon = LengthMoon(WMoon, 0);
|
||
|
qYal = qYallop(WMoon, ARCVact);
|
||
|
if (qYal > 0.216) qCrit = 1; /* A */
|
||
|
if (qYal < 0.216 && qYal > -0.014) qCrit = 2; /* B */
|
||
|
if (qYal < -0.014 && qYal > -0.16) qCrit = 3; /* C */
|
||
|
if (qYal < -0.16 && qYal > -0.232) qCrit = 4; /* D */
|
||
|
if (qYal < -0.232 && qYal > -0.293) qCrit = 5; /* E */
|
||
|
if (qYal < -0.293) qCrit = 6; /* F */
|
||
|
}
|
||
|
/*determine if rise or set event*/
|
||
|
RS = 2;
|
||
|
if (TypeEvent == 1 || TypeEvent == 4) RS = 1;
|
||
|
retval = RiseSet(JDNDaysUT - 4.0 / 24.0, dgeo, datm, "sun", RS, helflag, 0, &RiseSetS, serr);
|
||
|
if (retval == ERR)
|
||
|
return ERR;
|
||
|
retval = RiseSet(JDNDaysUT - 4.0 / 24.0, dgeo, datm, ObjectName, RS, helflag, 0, &RiseSetO, serr);
|
||
|
if (retval == ERR)
|
||
|
return ERR;
|
||
|
TbYallop = TJD_INVALID;
|
||
|
if (retval == -2) { /* object does not rise or set */
|
||
|
Lag = 0;
|
||
|
noriseO = TRUE;
|
||
|
} else {
|
||
|
Lag = RiseSetO - RiseSetS;
|
||
|
if (Planet == SE_MOON)
|
||
|
TbYallop = (RiseSetO * 4 + RiseSetS * 5) / 9.0;
|
||
|
}
|
||
|
if ((TypeEvent == 3 || TypeEvent == 4) && (Planet == -1 || Planet >= SE_MARS)) {
|
||
|
TfirstVR = TJD_INVALID;
|
||
|
TbVR = TJD_INVALID;
|
||
|
TlastVR = TJD_INVALID;
|
||
|
TvisVR = 0;
|
||
|
MinTAV = 0;
|
||
|
goto output_heliacal_pheno;
|
||
|
}
|
||
|
/* If HPheno >= 11 And HPheno <= 14 Or HPheno = 24 Then*/
|
||
|
/*te bepalen m.b.v. walkthrough*/
|
||
|
MinTAVact = 199;
|
||
|
DeltaAlt = 0;
|
||
|
OldestMinTAV = 0;
|
||
|
Ta = 0;
|
||
|
Tc = 0;
|
||
|
TbVR = 0;
|
||
|
TimeStep = -TimeStepDefault / 24.0 / 60.0;
|
||
|
if (RS == 2) TimeStep = -TimeStep;
|
||
|
TimePointer = RiseSetS - TimeStep;
|
||
|
do {
|
||
|
TimePointer = TimePointer + TimeStep;
|
||
|
OldestMinTAV = MinTAVoud;
|
||
|
MinTAVoud = MinTAVact;
|
||
|
DeltaAltoud = DeltaAlt;
|
||
|
retval = ObjectLoc(TimePointer, dgeo, datm, "sun", 0, helflag, &AltS2, serr);
|
||
|
if (retval == OK)
|
||
|
retval = ObjectLoc(TimePointer, dgeo, datm, ObjectName, 0, helflag, &AltO2, serr);
|
||
|
if (retval != OK)
|
||
|
return ERR;
|
||
|
DeltaAlt = AltO2 - AltS2;
|
||
|
if (DeterTAV(dobs, TimePointer, dgeo, datm, ObjectName, helflag, &MinTAVact, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (MinTAVoud < MinTAVact && TbVR == 0) {
|
||
|
/* determine if this is a local minimum with object still above horizon*/
|
||
|
TimeCheck = TimePointer + Sgn(TimeStep) * LocalMinStep / 24.0 / 60.0;
|
||
|
if (RiseSetO != 0) {
|
||
|
if (TimeStep > 0)
|
||
|
TimeCheck = mymin(TimeCheck, RiseSetO);
|
||
|
else
|
||
|
TimeCheck = mymax(TimeCheck, RiseSetO);
|
||
|
}
|
||
|
if (DeterTAV(dobs, TimeCheck, dgeo, datm, ObjectName, helflag, &LocalminCheck, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (LocalminCheck > MinTAVact) {
|
||
|
extrax = x2min(MinTAVact, MinTAVoud, OldestMinTAV);
|
||
|
TbVR = TimePointer - (1 - extrax) * TimeStep;
|
||
|
MinTAV = funct2(MinTAVact, MinTAVoud, OldestMinTAV, extrax);
|
||
|
}
|
||
|
}
|
||
|
if (DeltaAlt > MinTAVact && Tc == 0 && TbVR == 0) {
|
||
|
crosspoint = crossing(DeltaAltoud, DeltaAlt, MinTAVoud, MinTAVact);
|
||
|
Tc = TimePointer - TimeStep * (1 - crosspoint);
|
||
|
}
|
||
|
if (DeltaAlt < MinTAVact && Ta == 0 && Tc != 0) {
|
||
|
crosspoint = crossing(DeltaAltoud, DeltaAlt, MinTAVoud, MinTAVact);
|
||
|
Ta = TimePointer - TimeStep * (1 - crosspoint);
|
||
|
}
|
||
|
} while (fabs(TimePointer - RiseSetS) <= MaxTryHours / 24.0 && Ta == 0 && !((TbVR != 0 && (TypeEvent == 3 || TypeEvent == 4) && (strncmp(ObjectName, "moon", 4) != 0 && strncmp(ObjectName, "venus", 5) != 0 && strncmp(ObjectName, "mercury", 7) != 0))));
|
||
|
if (RS == 2) {
|
||
|
TfirstVR = Tc;
|
||
|
TlastVR = Ta;
|
||
|
} else {
|
||
|
TfirstVR = Ta;
|
||
|
TlastVR = Tc;
|
||
|
}
|
||
|
if (TfirstVR == 0 && TlastVR == 0) {
|
||
|
if (RS == 1)
|
||
|
TfirstVR = TbVR - 0.000001;
|
||
|
else
|
||
|
TlastVR = TbVR + 0.000001;
|
||
|
}
|
||
|
if (!noriseO) {
|
||
|
if (RS == 1)
|
||
|
TfirstVR = mymax(TfirstVR, RiseSetO);
|
||
|
else
|
||
|
TlastVR = mymin(TlastVR, RiseSetO);
|
||
|
}
|
||
|
TvisVR = TJD_INVALID; /*"#NA!" */
|
||
|
if (TlastVR != 0 && TfirstVR != 0)
|
||
|
TvisVR = TlastVR - TfirstVR;
|
||
|
if (TlastVR == 0) TlastVR = TJD_INVALID; /*"#NA!" */
|
||
|
if (TbVR == 0) TbVR = TJD_INVALID; /*"#NA!" */
|
||
|
if (TfirstVR == 0) TfirstVR = TJD_INVALID; /*"#NA!" */
|
||
|
output_heliacal_pheno:
|
||
|
/*End If*/
|
||
|
darr[0] = AltO;
|
||
|
darr[1] = AppAltO;
|
||
|
darr[2] = GeoAltO;
|
||
|
darr[3] = AziO;
|
||
|
darr[4] = AltS;
|
||
|
darr[5] = AziS;
|
||
|
darr[6] = TAVact;
|
||
|
darr[7] = ARCVact;
|
||
|
darr[8] = DAZact;
|
||
|
darr[9] = ARCLact;
|
||
|
darr[10] = kact;
|
||
|
darr[11] = MinTAV;
|
||
|
darr[12] = TfirstVR;
|
||
|
darr[13] = TbVR;
|
||
|
darr[14] = TlastVR;
|
||
|
darr[15] = TbYallop;
|
||
|
darr[16] = WMoon;
|
||
|
darr[17] = qYal;
|
||
|
darr[18] = qCrit;
|
||
|
darr[19] = ParO;
|
||
|
darr[20] = MagnO;
|
||
|
darr[21] = RiseSetO;
|
||
|
darr[22] = RiseSetS;
|
||
|
darr[23] = Lag;
|
||
|
darr[24] = TvisVR;
|
||
|
darr[25] = LMoon;
|
||
|
darr[26] = elong;
|
||
|
darr[27] = illum;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
int32 FAR PASCAL_CONV HeliacalJDut(double JDNDaysUTStart, double Age, double SN, double Lat, double Longitude, double HeightEye, double Temperature, double Pressure, double RH, double VR, char *ObjectName, int TypeEvent, char *AVkind, double *dret, char *serr)
|
||
|
{
|
||
|
double dgeo[3], datm[4], dobs[6];
|
||
|
int32 helflag = SE_HELFLAG_HIGH_PRECISION;
|
||
|
helflag |= SE_HELFLAG_AVKIND_VR;
|
||
|
dgeo[0] = Longitude;
|
||
|
dgeo[1] = Lat;
|
||
|
dgeo[2] = HeightEye;
|
||
|
datm[0] = Pressure;
|
||
|
datm[1] = Temperature;
|
||
|
datm[2] = RH;
|
||
|
datm[3] = VR;
|
||
|
dobs[0] = Age;
|
||
|
dobs[1] = SN;
|
||
|
return swe_heliacal_ut(JDNDaysUTStart, dgeo, datm, dobs, ObjectName, TypeEvent, helflag, dret, serr);
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
static double get_synodic_period(int Planet)
|
||
|
{
|
||
|
/* synodic periods from:
|
||
|
* Kelley/Milone/Aveni, "Exploring ancient Skies", p. 43. */
|
||
|
switch(Planet) {
|
||
|
case SE_MOON: return 29.530588853;
|
||
|
case SE_MERCURY: return 115.8775;
|
||
|
case SE_VENUS: return 583.9214;
|
||
|
case SE_MARS: return 779.9361;
|
||
|
case SE_JUPITER: return 398.8840;
|
||
|
case SE_SATURN: return 378.0919;
|
||
|
case SE_URANUS: return 369.6560;
|
||
|
case SE_NEPTUNE: return 367.4867;
|
||
|
case SE_PLUTO: return 366.7207;
|
||
|
}
|
||
|
return 366; /* for stars and default for far away planets */
|
||
|
}
|
||
|
|
||
|
/*###################################################################*/
|
||
|
static int32 moon_event_arc_vis(double JDNDaysUTStart, double *dgeo, double *datm, double *dobs, int32 TypeEvent, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
double x[20], MinTAV, MinTAVoud, OldestMinTAV;
|
||
|
double phase1, phase2, JDNDaysUT, JDNDaysUTi;
|
||
|
double tjd_moonevent, tjd_moonevent_start;
|
||
|
double DeltaAltoud, TimeCheck, LocalminCheck;
|
||
|
double AltS, AltO, DeltaAlt = 90;
|
||
|
char ObjectName[30];
|
||
|
int32 iflag, Daystep, goingup, Planet, retval;
|
||
|
int32 avkind = helflag & SE_HELFLAG_AVKIND;
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
dret[0] = JDNDaysUTStart; /* will be returned in error case */
|
||
|
if (avkind == 0)
|
||
|
avkind = SE_HELFLAG_AVKIND_VR;
|
||
|
if (avkind != SE_HELFLAG_AVKIND_VR) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error: in valid AV kind for the moon");
|
||
|
return ERR;
|
||
|
}
|
||
|
if (TypeEvent == 1 || TypeEvent == 2) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error: the moon has no morning first or evening last");
|
||
|
return ERR;
|
||
|
}
|
||
|
strcpy(ObjectName, "moon");
|
||
|
Planet = SE_MOON;
|
||
|
iflag = SEFLG_TOPOCTR | SEFLG_EQUATORIAL | epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT|SEFLG_TRUEPOS;
|
||
|
Daystep = 1;
|
||
|
if (TypeEvent == 3) {
|
||
|
/*morning last */
|
||
|
TypeEvent = 2;
|
||
|
} else {
|
||
|
/*evening first*/
|
||
|
TypeEvent = 1;
|
||
|
Daystep = -Daystep;
|
||
|
}
|
||
|
/* check Synodic/phase Period */
|
||
|
JDNDaysUT = JDNDaysUTStart;
|
||
|
/* start 30 days later if TypeEvent=4 (1) */
|
||
|
if (TypeEvent == 1) JDNDaysUT = JDNDaysUT + 30;
|
||
|
/* determination of new moon date */
|
||
|
swe_pheno_ut(JDNDaysUT, Planet, iflag, x, serr);
|
||
|
phase2 = x[0];
|
||
|
goingup = 0;
|
||
|
do {
|
||
|
JDNDaysUT = JDNDaysUT + Daystep;
|
||
|
phase1 = phase2;
|
||
|
swe_pheno_ut(JDNDaysUT, Planet, iflag, x, serr);
|
||
|
phase2 = x[0];
|
||
|
if (phase2 > phase1)
|
||
|
goingup = 1;
|
||
|
} while (goingup == 0 || (goingup == 1 && (phase2 > phase1)));
|
||
|
/* fix the date to get the day with the smallest phase (nwest moon) */
|
||
|
JDNDaysUT = JDNDaysUT - Daystep;
|
||
|
/* initialize the date to look for set */
|
||
|
JDNDaysUTi = JDNDaysUT;
|
||
|
JDNDaysUT = JDNDaysUT - Daystep;
|
||
|
MinTAVoud = 199;
|
||
|
do {
|
||
|
JDNDaysUT = JDNDaysUT + Daystep;
|
||
|
if ((retval = RiseSet(JDNDaysUT, dgeo, datm, ObjectName, TypeEvent, helflag, 0, &tjd_moonevent, serr)) != OK)
|
||
|
return retval;
|
||
|
tjd_moonevent_start = tjd_moonevent;
|
||
|
MinTAV = 199;
|
||
|
OldestMinTAV = MinTAV;
|
||
|
do {
|
||
|
OldestMinTAV = MinTAVoud;
|
||
|
MinTAVoud = MinTAV;
|
||
|
DeltaAltoud = DeltaAlt;
|
||
|
tjd_moonevent = tjd_moonevent - 1.0 / 60.0 / 24.0 * Sgn(Daystep);
|
||
|
if (ObjectLoc(tjd_moonevent, dgeo, datm, "sun", 0, helflag, &AltS, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (ObjectLoc(tjd_moonevent, dgeo, datm, ObjectName, 0, helflag, &AltO, serr) == ERR)
|
||
|
return ERR;
|
||
|
DeltaAlt = AltO - AltS;
|
||
|
if (DeterTAV(dobs, tjd_moonevent, dgeo, datm, ObjectName, helflag, &MinTAV, serr) == ERR)
|
||
|
return ERR;
|
||
|
TimeCheck = tjd_moonevent - LocalMinStep / 60.0 / 24.0 * Sgn(Daystep);
|
||
|
if (DeterTAV(dobs, TimeCheck, dgeo, datm, ObjectName, helflag, &LocalminCheck, serr) == ERR)
|
||
|
return ERR;
|
||
|
/*printf("%f, %f <= %f\n", tjd_moonevent, MinTAV, MinTAVoud);*/
|
||
|
/* while (MinTAV <= MinTAVoud && fabs(tjd_moonevent - tjd_moonevent_start) < 120.0 / 60.0 / 24.0);*/
|
||
|
} while ((MinTAV <= MinTAVoud || LocalminCheck < MinTAV) && fabs(tjd_moonevent - tjd_moonevent_start) < 120.0 / 60.0 / 24.0);
|
||
|
/* while (DeltaAlt < MinTAVoud && fabs(JDNDaysUT - JDNDaysUTi) < 15);*/
|
||
|
} while (DeltaAltoud < MinTAVoud && fabs(JDNDaysUT - JDNDaysUTi) < 15);
|
||
|
if (fabs(JDNDaysUT - JDNDaysUTi) < 15) {
|
||
|
tjd_moonevent += (1 - x2min(MinTAV, MinTAVoud, OldestMinTAV)) * Sgn(Daystep) / 60.0 / 24.0;
|
||
|
} else {
|
||
|
strcpy(serr, "no date found for lunar event");
|
||
|
return ERR;
|
||
|
}
|
||
|
dret[0] = tjd_moonevent;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 heliacal_ut_arc_vis(double JDNDaysUTStart, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 TypeEventIn, int32 helflag, double *dret, char *serr_ret)
|
||
|
{
|
||
|
double x[6];
|
||
|
double xin[2];
|
||
|
double xaz[2];
|
||
|
double dang[3];
|
||
|
double objectmagn = 0, maxlength, DayStep;
|
||
|
double JDNDaysUT, JDNDaysUTfinal, JDNDaysUTstep, JDNDaysUTstepoud, JDNarcvisUT, tjd_tt, tret, OudeDatum, JDNDaysUTinp = JDNDaysUTStart, JDNDaysUTtijd;
|
||
|
double ArcusVis, ArcusVisDelta, ArcusVisPto, ArcusVisDeltaoud;
|
||
|
double Trise, sunsangle, Theliacal, Tdelta, Angle;
|
||
|
double TimeStep, TimePointer, OldestMinTAV, MinTAVoud, MinTAVact, extrax, TbVR = 0;
|
||
|
double AziS, AltS, AziO, AltO, DeltaAlt;
|
||
|
double direct, Pressure, Temperature, d;
|
||
|
int32 epheflag, retval = OK;
|
||
|
int32 iflag, Planet, eventtype;
|
||
|
int32 TypeEvent = TypeEventIn;
|
||
|
int doneoneday;
|
||
|
char serr[AS_MAXCH];
|
||
|
*dret = JDNDaysUTStart;
|
||
|
*serr = '\0';
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
Pressure = datm[0];
|
||
|
Temperature = datm[1];
|
||
|
/* determine Magnitude of star*/
|
||
|
if ((retval = Magnitude(JDNDaysUTStart, dgeo, ObjectName, helflag, &objectmagn, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
iflag = SEFLG_TOPOCTR | SEFLG_EQUATORIAL | epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT | SEFLG_TRUEPOS;
|
||
|
/* start values for search of heliacal rise
|
||
|
* maxlength = phase period in days, smaller than minimal synodic period */
|
||
|
/* days per step (for heliacal rise) in power of two */
|
||
|
switch(Planet) {
|
||
|
case SE_MERCURY:
|
||
|
DayStep = 1; maxlength = 100; break;
|
||
|
case SE_VENUS:
|
||
|
DayStep = 64; maxlength = 384; break;
|
||
|
case SE_MARS:
|
||
|
DayStep = 128; maxlength = 640; break;
|
||
|
case SE_JUPITER:
|
||
|
DayStep = 64; maxlength = 384; break;
|
||
|
case SE_SATURN:
|
||
|
DayStep = 64; maxlength = 256; break;
|
||
|
default:
|
||
|
DayStep = 64; maxlength = 256; break;
|
||
|
}
|
||
|
/* heliacal setting */
|
||
|
eventtype = TypeEvent;
|
||
|
if (eventtype == 2) DayStep = -DayStep;
|
||
|
/* acronychal setting */
|
||
|
if (eventtype == 4) {
|
||
|
eventtype = 1;
|
||
|
DayStep = -DayStep;
|
||
|
}
|
||
|
/* acronychal rising */
|
||
|
if (eventtype == 3) eventtype = 2;
|
||
|
eventtype |= SE_BIT_DISC_CENTER;
|
||
|
/* normalize the maxlength to the step size */
|
||
|
{
|
||
|
/* check each Synodic/phase Period */
|
||
|
JDNDaysUT = JDNDaysUTStart;
|
||
|
/* make sure one can find an event on the just after the JDNDaysUTStart */
|
||
|
JDNDaysUTfinal = JDNDaysUT + maxlength;
|
||
|
JDNDaysUT = JDNDaysUT - 1;
|
||
|
if (DayStep < 0) {
|
||
|
JDNDaysUTtijd = JDNDaysUT;
|
||
|
JDNDaysUT = JDNDaysUTfinal;
|
||
|
JDNDaysUTfinal = JDNDaysUTtijd;
|
||
|
}
|
||
|
/* prepair the search */
|
||
|
JDNDaysUTstep = JDNDaysUT - DayStep;
|
||
|
doneoneday = 0;
|
||
|
ArcusVisDelta = 199;
|
||
|
ArcusVisPto = -5.55;
|
||
|
do { /* this is a do {} while() loop */
|
||
|
if (fabs(DayStep) == 1) doneoneday = 1;
|
||
|
do { /* this is a do {} while() loop */
|
||
|
/* init search for heliacal rise */
|
||
|
JDNDaysUTstepoud = JDNDaysUTstep;
|
||
|
ArcusVisDeltaoud = ArcusVisDelta;
|
||
|
JDNDaysUTstep = JDNDaysUTstep + DayStep;
|
||
|
/* determine rise/set time */
|
||
|
if ((retval = my_rise_trans(JDNDaysUTstep, SE_SUN, "", eventtype, helflag, dgeo, datm, &tret, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
/* determine time compensation to get Sun's altitude at heliacal rise */
|
||
|
tjd_tt = tret + DeltaT(tret, 0) / D2S;
|
||
|
if ((retval = swe_calc(tjd_tt, SE_SUN, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(tret, SE_EQU2HOR, dgeo, Pressure, Temperature, xin, xaz);
|
||
|
Trise = HourAngle(xaz[1], x[1], dgeo[1]);
|
||
|
sunsangle = ArcusVisPto;
|
||
|
if (helflag & SE_HELFLAG_AVKIND_MIN7) sunsangle = -7;
|
||
|
if (helflag & SE_HELFLAG_AVKIND_MIN9) sunsangle = -9;
|
||
|
Theliacal = HourAngle(sunsangle, x[1], dgeo[1]);
|
||
|
Tdelta = Theliacal - Trise;
|
||
|
if (TypeEvent == 2 || TypeEvent== 3) Tdelta = -Tdelta;
|
||
|
/* determine appr.time when sun is at the wanted Sun's altitude */
|
||
|
JDNarcvisUT = tret - Tdelta / 24;
|
||
|
tjd_tt = JDNarcvisUT + DeltaT(JDNarcvisUT, 0) / D2S;
|
||
|
/* determine Sun's position */
|
||
|
if ((retval = swe_calc(tjd_tt, SE_SUN, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNarcvisUT, SE_EQU2HOR, dgeo, Pressure, Temperature, xin, xaz);
|
||
|
AziS = xaz[0] + 180;
|
||
|
if (AziS >= 360) AziS = AziS - 360;
|
||
|
AltS = xaz[1];
|
||
|
/* determine Moon's position */
|
||
|
#if 0
|
||
|
double AltM, AziM;
|
||
|
if ((retval = swe_calc(tjd_tt, SE_MOON, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNarcvisUT, SE_EQU2HOR, dgeo, Pressure, Temperature, xin, xaz);
|
||
|
AziM = xaz[0] + 180;
|
||
|
if (AziM >= 360) AziM = AziM - 360;
|
||
|
AltM = xaz[1];
|
||
|
#endif
|
||
|
/* determine object's position */
|
||
|
if (Planet != -1) {
|
||
|
if ((retval = swe_calc(tjd_tt, Planet, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
/* determine magnitude of Planet */
|
||
|
if ((retval = Magnitude(JDNarcvisUT, dgeo, ObjectName, helflag, &objectmagn, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
} else {
|
||
|
if ((retval = call_swe_fixstar(ObjectName, tjd_tt, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNarcvisUT, SE_EQU2HOR, dgeo, Pressure, Temperature, xin, xaz);
|
||
|
AziO = xaz[0] + 180;
|
||
|
if (AziO >= 360) AziO = AziO - 360;
|
||
|
AltO = xaz[1];
|
||
|
/* determine arcusvisionis */
|
||
|
DeltaAlt = AltO - AltS;
|
||
|
/*if ((retval = HeliacalAngle(objectmagn, dobs, AziO, AltM, AziM, JDNarcvisUT, AziS, dgeo, datm, helflag, dang, serr)) == ERR)*/
|
||
|
if ((retval = HeliacalAngle(objectmagn, dobs, AziO, -1, 0, JDNarcvisUT, AziS, dgeo, datm, helflag, dang, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
ArcusVis = dang[1];
|
||
|
ArcusVisPto = dang[2];
|
||
|
ArcusVisDelta = DeltaAlt - ArcusVis;
|
||
|
/*} while (((ArcusVisDeltaoud > 0 && ArcusVisDelta < 0) || ArcusVisDelta < 0) && (JDNDaysUTfinal - JDNDaysUTstep) * Sgn(DayStep) > 0);*/
|
||
|
} while ((ArcusVisDeltaoud > 0 || ArcusVisDelta < 0) && (JDNDaysUTfinal - JDNDaysUTstep) * Sgn(DayStep) > 0);
|
||
|
if (doneoneday == 0 && (JDNDaysUTfinal - JDNDaysUTstep) * Sgn(DayStep) > 0) {
|
||
|
/* go back to date before heliacal altitude */
|
||
|
ArcusVisDelta = ArcusVisDeltaoud;
|
||
|
DayStep = ((int) (fabs(DayStep) / 2.0)) * Sgn(DayStep);
|
||
|
JDNDaysUTstep = JDNDaysUTstepoud;
|
||
|
}
|
||
|
} while (doneoneday == 0 && (JDNDaysUTfinal - JDNDaysUTstep) * Sgn(DayStep) > 0);
|
||
|
}
|
||
|
d = (JDNDaysUTfinal - JDNDaysUTstep) * Sgn(DayStep);
|
||
|
if (d <= 0 || d >= maxlength) {
|
||
|
dret[0] = JDNDaysUTinp; /* no date found, just return input */
|
||
|
retval = -2; /* marks "not found" within synodic period */
|
||
|
sprintf(serr, "heliacal event not found within maxlength %f\n", maxlength);
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
#if 0
|
||
|
if (helflag & SE_HELFLAG_AVKIND_VR) {
|
||
|
double darr[40];
|
||
|
if (swe_heliacal_pheno_ut(JDNarcvisUT, dgeo, datm, dobs, ObjectName, TypeEvent, helflag, darr, serr) != OK)
|
||
|
return ERR;
|
||
|
JDNarcvisUT = darr[13];
|
||
|
}
|
||
|
}
|
||
|
#endif
|
||
|
direct = TimeStepDefault / 24.0 / 60.0;
|
||
|
if (DayStep < 0) direct = -direct;
|
||
|
if (helflag & SE_HELFLAG_AVKIND_VR) {
|
||
|
/*te bepalen m.b.v. walkthrough*/
|
||
|
TimeStep = direct;
|
||
|
TbVR = 0;
|
||
|
TimePointer = JDNarcvisUT;
|
||
|
if (DeterTAV(dobs, TimePointer, dgeo, datm, ObjectName, helflag, &OldestMinTAV, serr) == ERR)
|
||
|
return ERR;
|
||
|
TimePointer = TimePointer + TimeStep;
|
||
|
if (DeterTAV(dobs, TimePointer, dgeo, datm, ObjectName, helflag, &MinTAVoud, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (MinTAVoud > OldestMinTAV) {
|
||
|
TimePointer = JDNarcvisUT;
|
||
|
TimeStep = -TimeStep;
|
||
|
MinTAVact = OldestMinTAV;
|
||
|
} else {
|
||
|
MinTAVact = MinTAVoud;
|
||
|
MinTAVoud = OldestMinTAV;
|
||
|
}
|
||
|
/*TimePointer = TimePointer - Timestep*/
|
||
|
do {
|
||
|
TimePointer = TimePointer + TimeStep;
|
||
|
OldestMinTAV = MinTAVoud;
|
||
|
MinTAVoud = MinTAVact;
|
||
|
if (DeterTAV(dobs, TimePointer, dgeo, datm, ObjectName, helflag, &MinTAVact, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (MinTAVoud < MinTAVact) {
|
||
|
extrax = x2min(MinTAVact, MinTAVoud, OldestMinTAV);
|
||
|
TbVR = TimePointer - (1 - extrax) * TimeStep;
|
||
|
}
|
||
|
} while (TbVR == 0);
|
||
|
JDNarcvisUT = TbVR;
|
||
|
}
|
||
|
/*if (strncmp(AVkind, "pto", 3) == 0) */
|
||
|
if (helflag & SE_HELFLAG_AVKIND_PTO) {
|
||
|
do {
|
||
|
OudeDatum = JDNarcvisUT;
|
||
|
JDNarcvisUT = JDNarcvisUT - direct;
|
||
|
tjd_tt = JDNarcvisUT + DeltaT(JDNarcvisUT, 0) / D2S;
|
||
|
if (Planet != -1) {
|
||
|
if ((retval = swe_calc(tjd_tt, Planet, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
} else {
|
||
|
if ((retval = call_swe_fixstar(ObjectName, tjd_tt, iflag, x, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
xin[0] = x[0];
|
||
|
xin[1] = x[1];
|
||
|
swe_azalt(JDNarcvisUT, SE_EQU2HOR, dgeo, Pressure, Temperature, xin, xaz);
|
||
|
Angle = xaz[1];
|
||
|
} while (Angle > 0);
|
||
|
JDNarcvisUT = (JDNarcvisUT + OudeDatum) / 2.0;
|
||
|
}
|
||
|
if (JDNarcvisUT < -9999999 || JDNarcvisUT > 9999999) {
|
||
|
dret[0] = JDNDaysUT; /* no date found, just return input */
|
||
|
strcpy(serr, "no heliacal date found");
|
||
|
retval = ERR;
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
dret[0] = JDNarcvisUT;
|
||
|
swe_heliacal_err:
|
||
|
if (serr_ret != NULL && *serr != '\0')
|
||
|
strcpy(serr_ret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
static int32 get_asc_obl(double tjd, int32 ipl, char *star, int32 iflag, double
|
||
|
*dgeo, AS_BOOL desc_obl, double *daop, char *serr)
|
||
|
{
|
||
|
int32 retval;
|
||
|
int32 epheflag = iflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
double x[6], adp;
|
||
|
char s[AS_MAXCH];
|
||
|
char star2[AS_MAXCH];
|
||
|
strcpy(star2, star);
|
||
|
if (ipl == -1) {
|
||
|
if ((retval = swe_fixstar(star2, tjd, epheflag | SEFLG_EQUATORIAL, x, serr)) == ERR)
|
||
|
return ERR;
|
||
|
} else {
|
||
|
if ((retval = swe_calc(tjd, ipl, epheflag | SEFLG_EQUATORIAL, x, serr)) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
adp = tan(dgeo[1] * DEGTORAD) * tan(x[1] * DEGTORAD);
|
||
|
if (fabs(adp) > 1) {
|
||
|
if (star != NULL && *star != '\0')
|
||
|
strcpy(s, star);
|
||
|
else
|
||
|
swe_get_planet_name(ipl, s);
|
||
|
sprintf(serr, "%s is circumpolar, cannot calculate heliacal event", s);
|
||
|
return -2;
|
||
|
}
|
||
|
adp = asin(adp) / DEGTORAD;
|
||
|
if (desc_obl)
|
||
|
*daop = x[0] + adp;
|
||
|
else
|
||
|
*daop = x[0] - adp;
|
||
|
*daop = swe_degnorm(*daop);
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
static int32 get_asc_obl_old(double tjd, int32 ipl, char *star, int32 iflag, double *dgeo, AS_BOOL desc_obl, double *daop, char *serr)
|
||
|
{
|
||
|
int32 retval;
|
||
|
int32 epheflag = iflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
double x[6], adp;
|
||
|
char s[AS_MAXCH];
|
||
|
if (star != NULL && *star != '\0') {
|
||
|
if ((retval = call_swe_fixstar(star, tjd, epheflag | SEFLG_EQUATORIAL, x, serr)) == ERR)
|
||
|
return ERR;
|
||
|
} else {
|
||
|
if ((retval = swe_calc(tjd, ipl, epheflag | SEFLG_EQUATORIAL, x, serr)) == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
adp = tan(dgeo[1] * DEGTORAD) * tan(x[1] * DEGTORAD);
|
||
|
if (fabs(adp) > 1) {
|
||
|
if (star != NULL && *star != '\0')
|
||
|
strcpy(s, star);
|
||
|
else
|
||
|
swe_get_planet_name(ipl, s);
|
||
|
sprintf(serr, "%s is circumpolar, cannot calculate heliacal event", s);
|
||
|
return -2;
|
||
|
}
|
||
|
adp = asin(adp) / DEGTORAD;
|
||
|
if (desc_obl)
|
||
|
*daop = x[0] + adp;
|
||
|
else
|
||
|
*daop = x[0] - adp;
|
||
|
*daop = swe_degnorm(*daop);
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
static int32 get_asc_obl_diff(double tjd, int32 ipl, char *star, int32 iflag, double *dgeo, AS_BOOL desc_obl, AS_BOOL is_acronychal, double *dsunpl, char *serr)
|
||
|
{
|
||
|
int32 retval = OK;
|
||
|
double aosun, aopl;
|
||
|
/* ascensio obliqua of sun */
|
||
|
retval = get_asc_obl(tjd, SE_SUN, "", iflag, dgeo, desc_obl, &aosun, serr);
|
||
|
if (retval != OK)
|
||
|
return retval;
|
||
|
if (is_acronychal) {
|
||
|
if (desc_obl == TRUE)
|
||
|
desc_obl = FALSE;
|
||
|
else
|
||
|
desc_obl = TRUE;
|
||
|
}
|
||
|
/* ascensio obliqua of body */
|
||
|
retval = get_asc_obl(tjd, ipl, star, iflag, dgeo, desc_obl, &aopl, serr);
|
||
|
if (retval != OK)
|
||
|
return retval;
|
||
|
*dsunpl = swe_degnorm(aosun - aopl);
|
||
|
if (is_acronychal)
|
||
|
*dsunpl = swe_degnorm(*dsunpl - 180);
|
||
|
if (*dsunpl > 180) *dsunpl -= 360;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
static int32 get_asc_obl_diff_old(double tjd, int32 ipl, char *star, int32 iflag, double *dgeo, AS_BOOL desc_obl, double *dsunpl, char *serr)
|
||
|
{
|
||
|
int32 retval = OK;
|
||
|
double aosun, aopl;
|
||
|
/* ascensio obliqua of sun */
|
||
|
retval = get_asc_obl(tjd, SE_SUN, "", iflag, dgeo, desc_obl, &aosun, serr);
|
||
|
if (retval != OK)
|
||
|
return retval;
|
||
|
/* ascensio obliqua of body */
|
||
|
retval = get_asc_obl(tjd, ipl, star, iflag, dgeo, desc_obl, &aopl, serr);
|
||
|
if (retval != OK)
|
||
|
return retval;
|
||
|
*dsunpl = swe_degnorm(aosun - aopl);
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
/* times of
|
||
|
* - superior and inferior conjunction (Mercury and Venus)
|
||
|
* - conjunction and opposition (ipl >= Mars)
|
||
|
*/
|
||
|
static double tcon[] =
|
||
|
{
|
||
|
0, 0,
|
||
|
2451550, 2451550, /* Moon */
|
||
|
2451604, 2451670, /* Mercury */
|
||
|
2451980, 2452280, /* Venus */
|
||
|
2451727, 2452074, /* Mars */
|
||
|
2451673, 2451877, /* Jupiter */
|
||
|
2451675, 2451868, /* Saturn */
|
||
|
2451581, 2451768, /* Uranus */
|
||
|
2451568, 2451753, /* Neptune */
|
||
|
};
|
||
|
|
||
|
static int32 find_conjunct_sun(double tjd_start, int32 ipl, int32 helflag, int32 TypeEvent, double *tjd, char *serr)
|
||
|
{
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
int i;
|
||
|
double tjdcon, tjd0, ds, dsynperiod, x[6], xs[6], daspect = 0;
|
||
|
if (ipl >= SE_MARS && TypeEvent >= 3)
|
||
|
daspect = 180;
|
||
|
i = (TypeEvent - 1) / 2 + ipl * 2;
|
||
|
tjd0 = tcon[i];
|
||
|
dsynperiod = get_synodic_period(ipl);
|
||
|
tjdcon = tjd0 + ((floor) ((tjd_start - tjd0) / dsynperiod) + 1) * dsynperiod;
|
||
|
ds = 100;
|
||
|
while (ds > 0.5) {
|
||
|
if (swe_calc(tjdcon, ipl, epheflag|SEFLG_SPEED, x, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (swe_calc(tjdcon, SE_SUN, epheflag|SEFLG_SPEED, xs, serr) == ERR)
|
||
|
return ERR;
|
||
|
ds = swe_degnorm(x[0] - xs[0] - daspect);
|
||
|
if (ds > 180) ds -= 360;
|
||
|
tjdcon -= ds / (x[3] - xs[3]);
|
||
|
}
|
||
|
*tjd = tjdcon;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 get_asc_obl_with_sun(double tjd_start, int32 ipl, char *star, int32 helflag, int32 evtyp, double dperiod, double *dgeo, double *tjdret, char *serr)
|
||
|
{
|
||
|
int i, retval;
|
||
|
int32 is_acronychal = FALSE;
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
double dsunpl = 1, dsunpl_save, dsunpl_test, tjd, daystep;
|
||
|
AS_BOOL desc_obl = FALSE, retro = FALSE;
|
||
|
if (evtyp == SE_EVENING_LAST || evtyp == SE_EVENING_FIRST)
|
||
|
desc_obl = TRUE;
|
||
|
if (evtyp == SE_MORNING_FIRST || evtyp == SE_EVENING_LAST)
|
||
|
retro = TRUE;
|
||
|
if (evtyp == SE_ACRONYCHAL_RISING)
|
||
|
desc_obl = TRUE;
|
||
|
if (evtyp == SE_ACRONYCHAL_RISING || evtyp == SE_ACRONYCHAL_SETTING) {
|
||
|
is_acronychal = TRUE;
|
||
|
if (ipl != SE_MOON)
|
||
|
retro = TRUE;
|
||
|
}
|
||
|
// if (evtyp == 3 || evtyp == 4)
|
||
|
// dangsearch = 180;
|
||
|
/* find date when sun and object have the same ascensio obliqua */
|
||
|
tjd = tjd_start;
|
||
|
dsunpl_save = -999999999;
|
||
|
retval = get_asc_obl_diff(tjd, ipl, star, epheflag, dgeo, desc_obl, is_acronychal, &dsunpl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
daystep = 20;
|
||
|
i = 0;
|
||
|
while (dsunpl_save == -999999999 ||
|
||
|
/*fabs(dsunpl - dsunpl_save) > 180 ||*/
|
||
|
fabs(dsunpl) + fabs(dsunpl_save) > 180 ||
|
||
|
(retro && !(dsunpl_save < 0 && dsunpl >= 0)) ||
|
||
|
(!retro && !(dsunpl_save >= 0 && dsunpl < 0))) {
|
||
|
i++;
|
||
|
if (i > 5000) {
|
||
|
sprintf(serr, "loop in get_asc_obl_with_sun() (1)");
|
||
|
return ERR;
|
||
|
}
|
||
|
dsunpl_save = dsunpl;
|
||
|
tjd += 10.0;
|
||
|
if (dperiod > 0 && tjd - tjd_start > dperiod)
|
||
|
return -2;
|
||
|
retval = get_asc_obl_diff(tjd, ipl, star, epheflag, dgeo, desc_obl, is_acronychal, &dsunpl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
}
|
||
|
tjd_start = tjd - daystep;
|
||
|
daystep /= 2.0;
|
||
|
tjd = tjd_start + daystep;
|
||
|
retval = get_asc_obl_diff(tjd, ipl, star, epheflag, dgeo, desc_obl, is_acronychal, &dsunpl_test, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
i = 0;
|
||
|
while (fabs(dsunpl) > 0.00001) {
|
||
|
i++;
|
||
|
if (i > 5000) {
|
||
|
sprintf(serr, "loop in get_asc_obl_with_sun() (2)");
|
||
|
return ERR;
|
||
|
}
|
||
|
if (dsunpl_save * dsunpl_test >= 0) {
|
||
|
dsunpl_save = dsunpl_test;
|
||
|
tjd_start = tjd;
|
||
|
} else {
|
||
|
dsunpl = dsunpl_test;
|
||
|
}
|
||
|
daystep /= 2.0;
|
||
|
tjd = tjd_start + daystep;
|
||
|
retval = get_asc_obl_diff(tjd, ipl, star, epheflag, dgeo, desc_obl, is_acronychal, &dsunpl_test, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
}
|
||
|
*tjdret = tjd;
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
/* works only for fixed stars */
|
||
|
static int32 get_asc_obl_with_sun_old(double tjd_start, int32 ipl, char *star, int32 helflag, int32 TypeEvent, double *dgeo, double *tjdret, char *serr)
|
||
|
{
|
||
|
int retval;
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
double dsunpl = 1, tjd, daystep, dsunpl_save;
|
||
|
double dsynperiod = 367;
|
||
|
double dangsearch = 0;
|
||
|
AS_BOOL desc_obl = FALSE;
|
||
|
if (TypeEvent == 2 || TypeEvent == 3)
|
||
|
desc_obl = TRUE;
|
||
|
if (TypeEvent == 3 || TypeEvent == 4)
|
||
|
dangsearch = 180;
|
||
|
/* find date when sun and object have the same ascensio obliqua */
|
||
|
daystep = dsynperiod;
|
||
|
tjd = tjd_start;
|
||
|
retval = get_asc_obl_diff(tjd, ipl, star, epheflag, dgeo, desc_obl, &dsunpl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
while (dsunpl < 359.99999) {
|
||
|
dsunpl_save = dsunpl;
|
||
|
daystep /= 2.0;
|
||
|
retval = get_asc_obl_diff(tjd + daystep, ipl, star, epheflag, dgeo, desc_obl, &dsunpl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
if (dsunpl > dsunpl_save)
|
||
|
tjd += daystep;
|
||
|
else
|
||
|
dsunpl = dsunpl_save;
|
||
|
}
|
||
|
*tjdret = tjd;
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
#if 0
|
||
|
/* works only for fixed stars */
|
||
|
static int32 get_asc_obl_acronychal(double tjd_start, int32 ipl, char *star, int32 helflag, int32 TypeEvent, double *dgeo, double *tjdret, char *serr)
|
||
|
{
|
||
|
int retval;
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
double dsunpl = 1, tjd, daystep, dsunpl_save;
|
||
|
double dsynperiod = 367;
|
||
|
double aosun, aopl;
|
||
|
AS_BOOL sun_desc = TRUE, obj_desc = FALSE;
|
||
|
daystep = dsynperiod;
|
||
|
tjd = tjd_start;
|
||
|
if (TypeEvent == 4) {
|
||
|
sun_desc = FALSE;
|
||
|
obj_desc = TRUE;
|
||
|
}
|
||
|
/* ascensio (descensio) obliqua of sun */
|
||
|
retval = get_asc_obl(tjd, SE_SUN, "", epheflag, dgeo, sun_desc, &aosun, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
/* ascensio (descensio) obliqua of body */
|
||
|
retval = get_asc_obl(tjd, ipl, star, epheflag, dgeo, obj_desc, &aopl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
dsunpl = swe_degnorm(aosun - aopl + 180);
|
||
|
while (dsunpl < 359.99999) {
|
||
|
dsunpl_save = dsunpl;
|
||
|
daystep /= 2.0;
|
||
|
/* ascensio (descensio) obliqua of sun */
|
||
|
retval = get_asc_obl(tjd+daystep, SE_SUN, "", epheflag, dgeo, sun_desc, &aosun, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
/* ascensio (descensio) obliqua of body */
|
||
|
retval = get_asc_obl(tjd+daystep, ipl, star, epheflag, dgeo, obj_desc, &aopl, serr);
|
||
|
if (retval != OK) /* retval may be ERR or -2 */
|
||
|
return retval;
|
||
|
dsunpl = swe_degnorm(aosun - aopl + 180);
|
||
|
if (dsunpl > dsunpl_save)
|
||
|
tjd += daystep;
|
||
|
else
|
||
|
dsunpl = dsunpl_save;
|
||
|
}
|
||
|
*tjdret = tjd;
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
static int32 get_heliacal_day(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, int32 TypeEvent, double *thel, char *serr)
|
||
|
{
|
||
|
int32 is_rise_or_set = 0, ndays, retval, retval_old;
|
||
|
double direct_day = 0, direct_time = 0, tfac, tend, daystep, tday, vdelta, tret;
|
||
|
double darr[30], vd, dmag;
|
||
|
int32 ipl = DeterObject(ObjectName);
|
||
|
/*
|
||
|
* find the day and minute on which the object becomes visible
|
||
|
*/
|
||
|
switch (TypeEvent) {
|
||
|
/* morning first */
|
||
|
case 1: is_rise_or_set = SE_CALC_RISE;
|
||
|
direct_day = 1; direct_time = -1;
|
||
|
break;
|
||
|
/* evening last */
|
||
|
case 2: is_rise_or_set = SE_CALC_SET;
|
||
|
direct_day = -1; direct_time = 1;
|
||
|
break;
|
||
|
/* evening first */
|
||
|
case 3: is_rise_or_set = SE_CALC_SET;
|
||
|
direct_day = 1; direct_time = 1;
|
||
|
break;
|
||
|
/* morning last */
|
||
|
case 4: is_rise_or_set = SE_CALC_RISE;
|
||
|
direct_day = -1; direct_time = -1;
|
||
|
break;
|
||
|
}
|
||
|
tfac = 1;
|
||
|
switch (ipl) {
|
||
|
case SE_MOON:
|
||
|
ndays = 6;
|
||
|
daystep = 1;
|
||
|
break;
|
||
|
case SE_MERCURY:
|
||
|
ndays = 60; tjd -= 0 * direct_day;
|
||
|
daystep = 5;
|
||
|
tfac = 5;
|
||
|
break;
|
||
|
case SE_VENUS:
|
||
|
ndays = 300; tjd -= 30 * direct_day;
|
||
|
daystep = 5;
|
||
|
if (TypeEvent >= 3) {
|
||
|
daystep = 15;
|
||
|
tfac = 3;
|
||
|
}
|
||
|
break;
|
||
|
case SE_MARS:
|
||
|
ndays = 400;
|
||
|
daystep = 15;
|
||
|
tfac = 5;
|
||
|
break;
|
||
|
case SE_SATURN:
|
||
|
ndays = 300;
|
||
|
daystep = 20;
|
||
|
tfac = 5;
|
||
|
break;
|
||
|
case -1:
|
||
|
ndays = 300;
|
||
|
if (call_swe_fixstar_mag(ObjectName, &dmag, serr) == ERR)
|
||
|
return ERR;
|
||
|
daystep = 15;
|
||
|
tfac = 10;
|
||
|
if (dmag > 2) {
|
||
|
daystep = 15;
|
||
|
}
|
||
|
if (dmag < 0) {
|
||
|
tfac = 3;
|
||
|
}
|
||
|
break;
|
||
|
default:
|
||
|
ndays = 300;
|
||
|
daystep = 15;
|
||
|
tfac = 3;
|
||
|
break;
|
||
|
}
|
||
|
tend = tjd + ndays * direct_day;
|
||
|
retval_old = -2;
|
||
|
for (tday = tjd;
|
||
|
(direct_day > 0 && tday < tend) || (direct_day < 0 && tday > tend);
|
||
|
tday += daystep * direct_day) {
|
||
|
vdelta = -100;
|
||
|
if ((retval = my_rise_trans(tday, SE_SUN, "", is_rise_or_set, helflag, dgeo, datm, &tret, serr)) == ERR)
|
||
|
return ERR;
|
||
|
/* sun does not rise: try next day */
|
||
|
if (retval == -2) {
|
||
|
retval_old = retval;
|
||
|
continue;
|
||
|
}
|
||
|
retval = swe_vis_limit_mag(tret, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
if (retval == ERR)
|
||
|
return ERR;
|
||
|
#if 1
|
||
|
/* object has appeared above horizon: reduce daystep */
|
||
|
if (retval_old == -2 && retval >= 0 && daystep > 1) {
|
||
|
retval_old = retval;
|
||
|
tday -= daystep * direct_day;
|
||
|
daystep = 1;
|
||
|
/* Note: beyond latitude 55N (?), Mars can have a morning last.
|
||
|
* If the period of visibility is less than 5 days, we may miss the
|
||
|
* event. I don't know if this happens */
|
||
|
if (ipl >= SE_MARS || ipl == -1)
|
||
|
daystep = 5;
|
||
|
continue;
|
||
|
}
|
||
|
retval_old = retval;
|
||
|
#endif
|
||
|
/* object below horizon: try next day */
|
||
|
if (retval == -2)
|
||
|
continue;
|
||
|
vdelta = darr[0] - darr[7];
|
||
|
/* find minute of object's becoming visible */
|
||
|
while (retval != -2 && (vd = darr[0] - darr[7]) < 0) {
|
||
|
if (vd < -1.0)
|
||
|
tret += 5.0 / 1440.0 * direct_time * tfac;
|
||
|
else if (vd < -0.5)
|
||
|
tret += 2.0 / 1440.0 * direct_time * tfac;
|
||
|
else if (vd < -0.1)
|
||
|
tret += 1.0 / 1440.0 * direct_time * tfac;
|
||
|
else
|
||
|
tret += 1.0 / 1440.0 * direct_time;
|
||
|
retval = swe_vis_limit_mag(tret, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
if (retval == ERR)
|
||
|
return ERR;
|
||
|
}
|
||
|
vdelta = darr[0] - darr[7];
|
||
|
/* object is visible, save time of appearance */
|
||
|
if (vdelta > 0) {
|
||
|
if ((ipl >= SE_MARS || ipl == -1) && daystep > 1) {
|
||
|
tday -= daystep * direct_day;
|
||
|
daystep = 1;
|
||
|
} else {
|
||
|
*thel = tret;
|
||
|
return OK;
|
||
|
}
|
||
|
}
|
||
|
}
|
||
|
sprintf(serr, "heliacal event does not happen");
|
||
|
return -2;
|
||
|
}
|
||
|
|
||
|
#if 0
|
||
|
static int32 get_acronychal_day_new(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, int32 TypeEvent, double *thel, char *serr) {
|
||
|
double tjdc = tjd, tret, x[6], xaz[6], AltO = -10;
|
||
|
int32 retval, is_rise_or_set, iter_day;
|
||
|
int32 ipl = DeterObject(ObjectName);
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
int32 iflag = epheflag | SEFLG_EQUATORIAL | SEFLG_TOPOCTR;
|
||
|
if ((retval = my_rise_trans(tret, 0, ObjectName, SE_CALC_RISE, helflag, dgeo, datm, &tret, serr)) == ERR) return ERR;
|
||
|
trise = tret;
|
||
|
tret += 0.01
|
||
|
if ((retval = my_rise_trans(tret, 0, ObjectName, SE_CALC_SET, helflag, dgeo, datm, &tret, serr)) == ERR) return ERR;
|
||
|
trise = tset;
|
||
|
|
||
|
*thel = tret;
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
#if 0
|
||
|
static int32 get_acronychal_day_old(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, int32 TypeEvent, double *thel, char *serr) {
|
||
|
double tjdc = tjd, tret, x[6], xaz[6], AltO = -10;
|
||
|
int32 retval, is_rise_or_set, iter_day;
|
||
|
int32 ipl = DeterObject(ObjectName);
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
int32 iflag = epheflag | SEFLG_EQUATORIAL | SEFLG_TOPOCTR;
|
||
|
if (TypeEvent == 3) {
|
||
|
is_rise_or_set = SE_CALC_SET;
|
||
|
tret = tjdc - 3;
|
||
|
if (ipl >= SE_MARS)
|
||
|
tret = tjdc - 3;
|
||
|
iter_day = 1;
|
||
|
} else {
|
||
|
is_rise_or_set = SE_CALC_RISE;
|
||
|
tret = tjdc + 3;
|
||
|
if (ipl >= SE_MARS)
|
||
|
tret = tjdc + 3;
|
||
|
iter_day = -1;
|
||
|
}
|
||
|
while (AltO < 0) {
|
||
|
tret += 0.3 * iter_day;
|
||
|
if (iter_day == -1)
|
||
|
tret -= 1;
|
||
|
retval = my_rise_trans(tret, SE_SUN, "", is_rise_or_set, helflag, dgeo, datm, &tret, serr);
|
||
|
if (retval != OK)
|
||
|
return retval;
|
||
|
/* determine object's position */
|
||
|
if (ipl == -1)
|
||
|
retval = call_swe_fixstar(ObjectName, tret+swe_deltat(tret), iflag, x, serr);
|
||
|
else
|
||
|
retval = swe_calc(tret+swe_deltat(tret), ipl, iflag, x, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
swe_azalt(tret, SE_EQU2HOR, dgeo, datm[0], datm[1], x, xaz);
|
||
|
AltO = xaz[2];
|
||
|
}
|
||
|
*thel = tret;
|
||
|
return OK;
|
||
|
}
|
||
|
#endif
|
||
|
|
||
|
static int32 time_optimum_visibility(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, double *tret, char *serr)
|
||
|
{
|
||
|
int32 retval, retval_sv, i;
|
||
|
double d, vl, darr[10], phot_scot_opic, phot_scot_opic_sv;
|
||
|
*tret = tjd;
|
||
|
retval = swe_vis_limit_mag(tjd, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
retval_sv = retval;
|
||
|
vl = darr[0] - darr[7];
|
||
|
phot_scot_opic_sv = retval & SE_SCOTOPIC_FLAG;
|
||
|
for (i = 0, d = 100.0 / 86400.0; i < 3; i++, d /= 10.0) {
|
||
|
while((retval = swe_vis_limit_mag(tjd - d, dgeo, datm, dobs, ObjectName, helflag, darr, serr)) >= 0
|
||
|
&& darr[0] > darr[7]
|
||
|
&& darr[0] - darr[7] > vl) {
|
||
|
tjd -= d; vl = darr[0] - darr[7];
|
||
|
retval_sv = retval;
|
||
|
phot_scot_opic_sv = retval & SE_SCOTOPIC_FLAG;
|
||
|
/* printf("1: %f\n", darr[8]);*/
|
||
|
}
|
||
|
if (retval == ERR) return ERR;
|
||
|
while((retval = swe_vis_limit_mag(tjd + d, dgeo, datm, dobs, ObjectName, helflag, darr, serr)) >= 0
|
||
|
&& darr[0] > darr[7]
|
||
|
&& darr[0] - darr[7] > vl) {
|
||
|
tjd += d; vl = darr[0] - darr[7];
|
||
|
retval_sv = retval;
|
||
|
phot_scot_opic_sv = retval & SE_SCOTOPIC_FLAG;
|
||
|
/* printf("2: %f\n", darr[8]);*/
|
||
|
}
|
||
|
if (retval == ERR) return ERR;
|
||
|
}
|
||
|
/* printf("3: %f <-> %f\n", darr[8], phot_scot_opic_sv);*/
|
||
|
*tret = tjd;
|
||
|
if (retval >= 0) {
|
||
|
/* search for optimum came to an end because change scotopic/photopic: */
|
||
|
phot_scot_opic = (retval & SE_SCOTOPIC_FLAG);
|
||
|
if (phot_scot_opic_sv != phot_scot_opic) {
|
||
|
/* calling function writes warning into serr */
|
||
|
return -2;
|
||
|
}
|
||
|
/* valid result found but it is close to the scotopic/photopic limit */
|
||
|
if (retval_sv & SE_MIXEDOPIC_FLAG) {
|
||
|
return -2;
|
||
|
}
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 time_limit_invisible(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, int32 direct, double *tret, char *serr)
|
||
|
{
|
||
|
int32 retval, retval_sv, i, ncnt = 3;
|
||
|
double d = 0, darr[10], phot_scot_opic, phot_scot_opic_sv;
|
||
|
double d0 = 100.0 / 86400.0;
|
||
|
*tret = tjd;
|
||
|
if (strcmp(ObjectName, "moon") == 0) {
|
||
|
d0 *= 10;
|
||
|
ncnt = 4;
|
||
|
}
|
||
|
retval = swe_vis_limit_mag(tjd + d * direct, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
retval_sv = retval;
|
||
|
phot_scot_opic_sv = retval & SE_SCOTOPIC_FLAG;
|
||
|
for (i = 0, d = d0; i < ncnt; i++, d /= 10.0) {
|
||
|
while((retval = swe_vis_limit_mag(tjd + d * direct, dgeo, datm, dobs, ObjectName, helflag, darr, serr)) >= 0
|
||
|
&& darr[0] > darr[7]) {
|
||
|
tjd += d * direct;
|
||
|
retval_sv = retval;
|
||
|
phot_scot_opic_sv = retval & SE_SCOTOPIC_FLAG;
|
||
|
/* printf("%d: %f\n", direct, darr[8]); */
|
||
|
}
|
||
|
}
|
||
|
/* printf("4: %f, %f/%f %f <-> %f\n", darr[8], darr[0], darr[7], tjd, phot_scot_opic_sv); */
|
||
|
*tret = tjd;
|
||
|
/* if object disappears at setting, retval is -2, but we want it OK, and
|
||
|
* also suppress the warning "object is below local horizon" */
|
||
|
*serr = '\0';
|
||
|
if (retval >= 0) {
|
||
|
/* search for limit came to an end because change scotopic/photopic: */
|
||
|
phot_scot_opic = (retval & SE_SCOTOPIC_FLAG);
|
||
|
if (phot_scot_opic_sv != phot_scot_opic) {
|
||
|
/* calling function writes warning into serr */
|
||
|
return -2;
|
||
|
}
|
||
|
/* valid result found but it is close to the scotopic/photopic limit */
|
||
|
if (retval_sv & SE_MIXEDOPIC_FLAG) {
|
||
|
return -2;
|
||
|
}
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 get_acronychal_day(double tjd, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 helflag, int32 TypeEvent, double *thel, char *serr) {
|
||
|
double tret, tret_dark, darr[30], dtret;
|
||
|
/* x[6], xaz[6], alto, azio, alto_dark, azio_dark;*/
|
||
|
int32 retval, is_rise_or_set, direct;
|
||
|
int32 ipl = DeterObject(ObjectName);
|
||
|
helflag |= SE_HELFLAG_VISLIM_PHOTOPIC;
|
||
|
/*int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);*/
|
||
|
/* int32 iflag = epheflag | SEFLG_EQUATORIAL | SEFLG_TOPOCTR;*/
|
||
|
if (TypeEvent == 3 || TypeEvent == 5) {
|
||
|
is_rise_or_set = SE_CALC_RISE;
|
||
|
/* tret = tjdc - 3;
|
||
|
if (ipl >= SE_MARS)
|
||
|
tret = tjdc - 3;*/
|
||
|
direct = -1;
|
||
|
} else {
|
||
|
is_rise_or_set = SE_CALC_SET;
|
||
|
/*tret = tjdc + 3;
|
||
|
if (ipl >= SE_MARS)
|
||
|
tret = tjdc + 3;*/
|
||
|
direct = 1;
|
||
|
}
|
||
|
dtret = 999;
|
||
|
#if 0
|
||
|
while (fabs(dtret) > 0.5) {
|
||
|
#else
|
||
|
while (fabs(dtret) > 0.5 / 1440.0) {
|
||
|
#endif
|
||
|
tjd += 0.7 * direct;
|
||
|
if (direct < 0) tjd -= 1;
|
||
|
retval = my_rise_trans(tjd, ipl, ObjectName, is_rise_or_set, helflag, dgeo, datm, &tjd, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
retval = swe_vis_limit_mag(tjd, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
while(darr[0] < darr[7]) {
|
||
|
tjd += 10.0 / 1440.0 * -direct;
|
||
|
retval = swe_vis_limit_mag(tjd, dgeo, datm, dobs, ObjectName, helflag, darr, serr);
|
||
|
}
|
||
|
retval = time_limit_invisible(tjd, dgeo, datm, dobs, ObjectName, helflag | SE_HELFLAG_VISLIM_DARK, direct, &tret_dark, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
retval = time_limit_invisible(tjd, dgeo, datm, dobs, ObjectName, helflag | SE_HELFLAG_VISLIM_NOMOON, direct, &tret, serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
#if 0
|
||
|
if (azalt_cart(tret_dark, dgeo, datm, ObjectName, helflag, darr, serr) == ERR)
|
||
|
return ERR;
|
||
|
if (azalt_cart(tret, dgeo, datm, ObjectName, helflag, darr+6, serr) == ERR)
|
||
|
return ERR;
|
||
|
dtret = acos(swi_dot_prod_unit(darr+3, darr+9)) / DEGTORAD;
|
||
|
#else
|
||
|
dtret = fabs(tret - tret_dark);
|
||
|
#endif
|
||
|
}
|
||
|
if (azalt_cart(tret, dgeo, datm, "sun", helflag, darr, serr) == ERR)
|
||
|
return ERR;
|
||
|
*thel = tret;
|
||
|
if (darr[1] < -12) {
|
||
|
sprintf(serr, "acronychal rising/setting not available, %f", darr[1]);
|
||
|
return OK;
|
||
|
} else {
|
||
|
sprintf(serr, "solar altitude, %f", darr[1]);
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 get_heliacal_details(double tday, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 TypeEvent, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
int32 i, retval, direct;
|
||
|
AS_BOOL optimum_undefined, limit_1_undefined, limit_2_undefined;
|
||
|
/* find next optimum visibility */
|
||
|
optimum_undefined = FALSE;
|
||
|
retval = time_optimum_visibility(tday, dgeo, datm, dobs, ObjectName, helflag, &(dret[1]), serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
if (retval == -2) {
|
||
|
retval = OK;
|
||
|
optimum_undefined = TRUE; /* change photopic <-> scotopic vision */
|
||
|
}
|
||
|
/* find moment of becoming visible */
|
||
|
direct = 1;
|
||
|
if (TypeEvent == 1 || TypeEvent == 4)
|
||
|
direct = -1;
|
||
|
limit_1_undefined = FALSE;
|
||
|
retval = time_limit_invisible(tday, dgeo, datm, dobs, ObjectName, helflag, direct, &(dret[0]), serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
if (retval == -2) {
|
||
|
retval = OK;
|
||
|
limit_1_undefined = TRUE; /* change photopic <-> scotopic vision */
|
||
|
}
|
||
|
/* find moment of end of visibility */
|
||
|
direct *= -1;
|
||
|
limit_2_undefined = FALSE;
|
||
|
retval = time_limit_invisible(dret[1], dgeo, datm, dobs, ObjectName, helflag, direct, &(dret[2]), serr);
|
||
|
if (retval == ERR) return ERR;
|
||
|
if (retval == -2) {
|
||
|
retval = OK;
|
||
|
limit_2_undefined = TRUE; /* change photopic <-> scotopic vision */
|
||
|
}
|
||
|
/* correct sequence of times:
|
||
|
* with event types 2 and 3 swap dret[0] and dret[2] */
|
||
|
if (TypeEvent == 2 || TypeEvent == 3) {
|
||
|
tday = dret[2];
|
||
|
dret[2] = dret[0];
|
||
|
dret[0] = tday;
|
||
|
i = (int) limit_1_undefined;
|
||
|
limit_1_undefined = limit_2_undefined;
|
||
|
limit_2_undefined = (AS_BOOL) i;
|
||
|
}
|
||
|
/*if (retval == OK && dret[0] == dret[1]) */
|
||
|
if (optimum_undefined || limit_1_undefined || limit_2_undefined) {
|
||
|
sprintf(serr, "return values [");
|
||
|
if (limit_1_undefined)
|
||
|
strcat(serr, "0,");
|
||
|
if (optimum_undefined)
|
||
|
strcat(serr, "1,");
|
||
|
if (limit_2_undefined)
|
||
|
strcat(serr, "2,");
|
||
|
strcat(serr, "] are uncertain due to change between photopic and scotopic vision");
|
||
|
}
|
||
|
return OK;
|
||
|
}
|
||
|
|
||
|
static int32 heliacal_ut_vis_lim(double tjd_start, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 TypeEventIn, int32 helflag, double *dret, char *serr_ret)
|
||
|
{
|
||
|
int i;
|
||
|
double d, darr[10], direct = 1, tjd, tday;
|
||
|
int32 epheflag, retval = OK, helflag2;
|
||
|
int32 iflag, ipl;
|
||
|
int32 TypeEvent = TypeEventIn;
|
||
|
char serr[AS_MAXCH];
|
||
|
for (i = 0; i < 10; i++)
|
||
|
dret[i] = 0;
|
||
|
*dret = tjd_start;
|
||
|
*serr = '\0';
|
||
|
ipl = DeterObject(ObjectName);
|
||
|
epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
iflag = SEFLG_TOPOCTR | SEFLG_EQUATORIAL | epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT | SEFLG_TRUEPOS;
|
||
|
if (ipl == SE_MERCURY)
|
||
|
tjd = tjd_start - 30;
|
||
|
else
|
||
|
tjd = tjd_start - 50; /* -50 makes sure, that no event is missed,
|
||
|
* but may return an event before start date */
|
||
|
helflag2 = helflag;
|
||
|
/*helflag2 &= ~SE_HELFLAG_HIGH_PRECISION;*/
|
||
|
/*
|
||
|
* heliacal event
|
||
|
*/
|
||
|
if (ipl == SE_MERCURY || ipl == SE_VENUS || TypeEvent <= 2) {
|
||
|
if (ipl == -1) {
|
||
|
/* find date when star rises with sun (cosmic rising) */
|
||
|
retval = get_asc_obl_with_sun(tjd, ipl, ObjectName, helflag, TypeEvent, 0, dgeo, &tjd, serr);
|
||
|
if (retval != OK)
|
||
|
goto swe_heliacal_err; /* retval may be -2 or ERR */
|
||
|
} else {
|
||
|
/* find date of conjunction of object with sun */
|
||
|
if ((retval = find_conjunct_sun(tjd, ipl, helflag, TypeEvent, &tjd, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
/* find the day and minute on which the object becomes visible */
|
||
|
retval = get_heliacal_day(tjd, dgeo, datm, dobs, ObjectName, helflag2, TypeEvent, &tday, serr);
|
||
|
if (retval != OK)
|
||
|
goto swe_heliacal_err;
|
||
|
/*
|
||
|
* acronychal event
|
||
|
*/
|
||
|
} else {
|
||
|
if (1 || ipl == -1) {
|
||
|
/*retval = get_asc_obl_acronychal(tjd, ipl, ObjectName, helflag2, TypeEvent, dgeo, &tjd, serr);*/
|
||
|
retval = get_asc_obl_with_sun(tjd, ipl, ObjectName, helflag, TypeEvent, 0, dgeo, &tjd, serr);
|
||
|
if (retval != OK)
|
||
|
goto swe_heliacal_err;
|
||
|
} else {
|
||
|
/* find date of conjunction of object with sun */
|
||
|
if ((retval = find_conjunct_sun(tjd, ipl, helflag, TypeEvent, &tjd, serr)) == ERR)
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
tday = tjd;
|
||
|
retval = get_acronychal_day(tjd, dgeo, datm, dobs, ObjectName, helflag2, TypeEvent, &tday, serr);
|
||
|
if (retval != OK)
|
||
|
goto swe_heliacal_err;
|
||
|
}
|
||
|
dret[0] = tday;
|
||
|
if (!(helflag & SE_HELFLAG_NO_DETAILS)) {
|
||
|
/* more precise event times for
|
||
|
* - morning first, evening last
|
||
|
* - venus and mercury's evening first and morning last
|
||
|
*/
|
||
|
if (ipl == SE_MERCURY || ipl == SE_VENUS || TypeEvent <= 2) {
|
||
|
retval = get_heliacal_details(tday, dgeo, datm, dobs, ObjectName, TypeEvent, helflag2, dret, serr);
|
||
|
if (retval == ERR) goto swe_heliacal_err;
|
||
|
} else if (0) {
|
||
|
if (TypeEvent == 4 || TypeEvent == 6) direct = -1;
|
||
|
for (i = 0, d = 100.0 / 86400.0; i < 3; i++, d /= 10.0) {
|
||
|
while((retval = swe_vis_limit_mag(*dret + d * direct, dgeo, datm, dobs, ObjectName, helflag, darr, serr)) == -2 || (retval >= 0 && darr[0] < darr[7])) {
|
||
|
*dret += d * direct;
|
||
|
}
|
||
|
}
|
||
|
/* the last time step must be added */
|
||
|
if (retval == OK)
|
||
|
*dret += 1.0 / 86400.0 * direct;
|
||
|
}
|
||
|
} /* if (1) */
|
||
|
swe_heliacal_err:
|
||
|
if (serr_ret != NULL && *serr != '\0')
|
||
|
strcpy(serr_ret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
/*###################################################################*/
|
||
|
static int32 moon_event_vis_lim(double tjdstart, double *dgeo, double *datm, double *dobs, int32 TypeEvent, int32 helflag, double *dret, char *serr_ret)
|
||
|
{
|
||
|
double tjd, trise;
|
||
|
char serr[AS_MAXCH];
|
||
|
char ObjectName[30];
|
||
|
int32 iflag, ipl, retval, helflag2, direct;
|
||
|
int32 epheflag = helflag & (SEFLG_JPLEPH|SEFLG_SWIEPH|SEFLG_MOSEPH);
|
||
|
dret[0] = tjdstart; /* will be returned in error case */
|
||
|
if (TypeEvent == 1 || TypeEvent == 2) {
|
||
|
if (serr != NULL)
|
||
|
strcpy(serr, "error: the moon has no morning first or evening last");
|
||
|
return ERR;
|
||
|
}
|
||
|
strcpy(ObjectName, "moon");
|
||
|
ipl = SE_MOON;
|
||
|
iflag = SEFLG_TOPOCTR | SEFLG_EQUATORIAL | epheflag;
|
||
|
if (!(helflag & SE_HELFLAG_HIGH_PRECISION))
|
||
|
iflag |= SEFLG_NONUT|SEFLG_TRUEPOS;
|
||
|
helflag2 = helflag;
|
||
|
helflag2 &= ~SE_HELFLAG_HIGH_PRECISION;
|
||
|
/* check Synodic/phase Period */
|
||
|
tjd = tjdstart - 30; /* -50 makes sure, that no event is missed,
|
||
|
* but may return an event before start date */
|
||
|
if ((retval = find_conjunct_sun(tjd, ipl, helflag, TypeEvent, &tjd, serr)) == ERR)
|
||
|
return ERR;
|
||
|
/* find the day and minute on which the object becomes visible */
|
||
|
retval = get_heliacal_day(tjd, dgeo, datm, dobs, ObjectName, helflag2, TypeEvent, &tjd, serr);
|
||
|
if (retval != OK)
|
||
|
goto moon_event_err;
|
||
|
dret[0] = tjd;
|
||
|
/* find next optimum visibility */
|
||
|
retval = time_optimum_visibility(tjd, dgeo, datm, dobs, ObjectName, helflag, &tjd, serr);
|
||
|
if (retval == ERR) goto moon_event_err;
|
||
|
dret[1] = tjd;
|
||
|
/* find moment of becoming visible */
|
||
|
/* Note: The on the day of fist light the moon may become visible
|
||
|
* already during day. It also may appear during day, disappear again
|
||
|
* and then reappear after sunset */
|
||
|
direct = 1;
|
||
|
if (TypeEvent == 4)
|
||
|
direct = -1;
|
||
|
retval = time_limit_invisible(tjd, dgeo, datm, dobs, ObjectName, helflag, direct, &tjd, serr);
|
||
|
if (retval == ERR) goto moon_event_err;
|
||
|
dret[2] = tjd;
|
||
|
/* find moment of end of visibility */
|
||
|
direct *= -1;
|
||
|
retval = time_limit_invisible(dret[1], dgeo, datm, dobs, ObjectName, helflag, direct, &tjd, serr);
|
||
|
dret[0] = tjd;
|
||
|
if (retval == ERR) goto moon_event_err;
|
||
|
/* if the moon is visible before sunset, we return sunset as start time */
|
||
|
if (TypeEvent == 3) {
|
||
|
if ((retval = my_rise_trans(tjd, SE_SUN, "", SE_CALC_SET, helflag, dgeo, datm, &trise, serr)) == ERR)
|
||
|
return ERR;
|
||
|
if (trise < dret[1]) {
|
||
|
dret[0] = trise;
|
||
|
/* do not warn, it happens too often */
|
||
|
/*strcpy(serr, "start time given is sunset, but moon is observable before that");*/
|
||
|
}
|
||
|
/* if the moon is visible after sunrise, we return sunrise as end time */
|
||
|
} else {
|
||
|
if ((retval = my_rise_trans(dret[1], SE_SUN, "", SE_CALC_RISE, helflag, dgeo, datm, &trise, serr)) == ERR)
|
||
|
return ERR;
|
||
|
if (dret[0] > trise) {
|
||
|
dret[0] = trise;
|
||
|
/* do not warn, it happens too often */
|
||
|
/*strcpy(serr, "end time given is sunrise, but moon is observable after that");*/
|
||
|
}
|
||
|
}
|
||
|
/* correct order of the three times: */
|
||
|
if (TypeEvent == 4) {
|
||
|
tjd = dret[0];
|
||
|
dret[0] = dret[2];
|
||
|
dret[2] = tjd;
|
||
|
}
|
||
|
moon_event_err:
|
||
|
if (serr_ret != NULL && *serr != '\0')
|
||
|
strcpy(serr_ret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
|
||
|
static int32 MoonEventJDut(double JDNDaysUTStart, double *dgeo, double *datm, double *dobs, int32 TypeEvent, int32 helflag, double *dret, char *serr)
|
||
|
{
|
||
|
int32 avkind = helflag & SE_HELFLAG_AVKIND;
|
||
|
if (avkind)
|
||
|
return moon_event_arc_vis(JDNDaysUTStart, dgeo, datm, dobs, TypeEvent, helflag, dret, serr);
|
||
|
else
|
||
|
return moon_event_vis_lim(JDNDaysUTStart, dgeo, datm, dobs, TypeEvent, helflag, dret, serr);
|
||
|
}
|
||
|
|
||
|
static int32 heliacal_ut(double JDNDaysUTStart, double *dgeo, double *datm, double *dobs, char *ObjectName, int32 TypeEventIn, int32 helflag, double *dret, char *serr_ret)
|
||
|
{
|
||
|
int32 avkind = helflag & SE_HELFLAG_AVKIND;
|
||
|
if (avkind)
|
||
|
return heliacal_ut_arc_vis(JDNDaysUTStart, dgeo, datm, dobs, ObjectName, TypeEventIn, helflag, dret, serr_ret);
|
||
|
else
|
||
|
return heliacal_ut_vis_lim(JDNDaysUTStart, dgeo, datm, dobs, ObjectName, TypeEventIn, helflag, dret, serr_ret);
|
||
|
}
|
||
|
|
||
|
/*' Magn [-]
|
||
|
' tjd_ut start date (JD) for event search
|
||
|
' dgeo[3] geogr. longitude, latitude, eye height (m above sea level)
|
||
|
' datm[4] atm. pressure, temperature, RH, and VR
|
||
|
' - pressure atmospheric pressure (mbar, =hPa) default 1013.25hPa
|
||
|
' - temperature deg C, default 15 deg C (if at
|
||
|
' If both attemp and atpress are 0, a temperature and
|
||
|
' atmospheric pressure are estimated from the above-mentioned
|
||
|
' default values and the height above sea level.
|
||
|
' - RH relative humidity in %
|
||
|
' - VR VR>=1: the Meteorological range: default 40 km
|
||
|
' 1>VR>0: the ktot (so the total atmospheric coefficient):
|
||
|
' a good default would be 0.25
|
||
|
' VR=-1: the ktot is calculated from the other atmospheric
|
||
|
' constants.
|
||
|
' age [Year] default 36, experienced sky observer in ancient times
|
||
|
' optimum age is 23
|
||
|
' SN Snellen factor of the visual aquity of the observer
|
||
|
' default 1
|
||
|
' see: http://www.i-see.org/eyecharts.html#make-your-own
|
||
|
' TypeEvent 1 morning first
|
||
|
' 2 evening last
|
||
|
' 3 evening first
|
||
|
' 4 morning last
|
||
|
' dret output: time (tjd_ut) of heliacal event
|
||
|
' see http://www.iol.ie/~geniet/eng/atmoastroextinction.htm
|
||
|
*/
|
||
|
int32 FAR PASCAL_CONV swe_heliacal_ut(double JDNDaysUTStart, double *dgeo, double *datm, double *dobs, char *ObjectNameIn, int32 TypeEvent, int32 helflag, double *dret, char *serr_ret)
|
||
|
{
|
||
|
int32 retval, Planet, itry;
|
||
|
char ObjectName[AS_MAXCH], serr[AS_MAXCH], s[AS_MAXCH];
|
||
|
double tjd0 = JDNDaysUTStart, tjd, dsynperiod, tjdmax, tadd;
|
||
|
int32 MaxCountSynodicPeriod = MAX_COUNT_SYNPER;
|
||
|
char *sevent[7] = {"", "morning first", "evening last", "evening first", "morning last", "acronychal rising", "acronychal setting"};
|
||
|
if (helflag & SE_HELFLAG_LONG_SEARCH)
|
||
|
MaxCountSynodicPeriod = MAX_COUNT_SYNPER_MAX;
|
||
|
/* if (helflag & SE_HELFLAG_SEARCH_1_PERIOD)
|
||
|
MaxCountSynodicPeriod = 1; */
|
||
|
*serr = '\0';
|
||
|
if (serr_ret != NULL)
|
||
|
*serr_ret = '\0';
|
||
|
/* note, the fixed stars functions rewrite the star name. The input string
|
||
|
may be too short, so we have to make sure we have enough space */
|
||
|
strcpy_VBsafe(ObjectName, ObjectNameIn);
|
||
|
default_heliacal_parameters(datm, dgeo, dobs, helflag);
|
||
|
swe_set_topo(dgeo[0], dgeo[1], dgeo[2]);
|
||
|
Planet = DeterObject(ObjectName);
|
||
|
/*
|
||
|
* Moon events
|
||
|
*/
|
||
|
if (Planet == SE_MOON) {
|
||
|
if (TypeEvent == 1 || TypeEvent == 2) {
|
||
|
if (serr_ret != NULL)
|
||
|
sprintf(serr_ret, "%s (event type %d) does not exist for the moon\n", sevent[TypeEvent], TypeEvent);
|
||
|
return ERR;
|
||
|
}
|
||
|
tjd = tjd0;
|
||
|
retval = MoonEventJDut(tjd, dgeo, datm, dobs, TypeEvent, helflag, dret, serr);
|
||
|
while (retval != -2 && *dret < tjd0) {
|
||
|
tjd += 15;
|
||
|
*serr = '\0';
|
||
|
retval = MoonEventJDut(tjd, dgeo, datm, dobs, TypeEvent, helflag, dret, serr);
|
||
|
}
|
||
|
if (serr_ret != NULL && *serr != '\0')
|
||
|
strcpy(serr_ret, serr);
|
||
|
return retval;
|
||
|
}
|
||
|
/*
|
||
|
* planets and fixed stars
|
||
|
*/
|
||
|
if (!(helflag & SE_HELFLAG_AVKIND)) {
|
||
|
if (Planet == -1 || Planet >= SE_MARS) {
|
||
|
if (TypeEvent == 3 || TypeEvent == 4) {
|
||
|
if (serr_ret != NULL) {
|
||
|
if (Planet == -1)
|
||
|
strcpy(s, ObjectName);
|
||
|
else
|
||
|
swe_get_planet_name(Planet, s);
|
||
|
sprintf(serr_ret, "%s (event type %d) does not exist for %s\n", sevent[TypeEvent], TypeEvent, s);
|
||
|
}
|
||
|
return ERR;
|
||
|
}
|
||
|
}
|
||
|
}
|
||
|
/* arcus visionis method: set the TypeEvent for acronychal events */
|
||
|
if (helflag & SE_HELFLAG_AVKIND) {
|
||
|
if (Planet == -1 || Planet >= SE_MARS) {
|
||
|
if (TypeEvent == SE_ACRONYCHAL_RISING)
|
||
|
TypeEvent = 3;
|
||
|
if (TypeEvent == SE_ACRONYCHAL_SETTING)
|
||
|
TypeEvent = 4;
|
||
|
}
|
||
|
/* acronychal rising and setting (cosmic setting) are ill-defined.
|
||
|
* We do not calculate them with the "visibility limit method" */
|
||
|
} else if (1) {
|
||
|
if (TypeEvent == SE_ACRONYCHAL_RISING || TypeEvent == SE_ACRONYCHAL_SETTING) {
|
||
|
if (serr_ret != NULL) {
|
||
|
if (Planet == -1)
|
||
|
strcpy(s, ObjectName);
|
||
|
else
|
||
|
swe_get_planet_name(Planet, s);
|
||
|
sprintf(serr_ret, "%s (event type %d) is not provided for %s\n", sevent[TypeEvent], TypeEvent, s);
|
||
|
}
|
||
|
return ERR;
|
||
|
}
|
||
|
}
|
||
|
dsynperiod = get_synodic_period(Planet);
|
||
|
tjdmax = tjd0 + dsynperiod * MaxCountSynodicPeriod;
|
||
|
tadd = dsynperiod * 0.6;
|
||
|
if (Planet == SE_MERCURY)
|
||
|
tadd = 30;
|
||
|
/*
|
||
|
* this is the outer loop over n synodic periods
|
||
|
*/
|
||
|
tjd = tjd0;
|
||
|
retval = -2; /* indicates that another synodic period has to be done */
|
||
|
for (itry = 0;
|
||
|
tjd < tjdmax && retval == -2;
|
||
|
itry++, tjd += tadd) {
|
||
|
*serr = '\0';
|
||
|
retval = heliacal_ut(tjd, dgeo, datm, dobs, ObjectName, TypeEvent, helflag, dret, serr);
|
||
|
/* if resulting event date < start date for search (tjd0): retry starting
|
||
|
* from half a period later. The event must be found now, unless there
|
||
|
* is none, as is often the case with Mercury */
|
||
|
while (retval != -2 && *dret < tjd0) {
|
||
|
tjd += tadd;
|
||
|
*serr = '\0';
|
||
|
retval = heliacal_ut(tjd, dgeo, datm, dobs, ObjectName, TypeEvent, helflag, dret, serr);
|
||
|
}
|
||
|
}
|
||
|
/*
|
||
|
* no event was found within MaxCountSynodicPeriod, return error
|
||
|
*/
|
||
|
if ((helflag & SE_HELFLAG_SEARCH_1_PERIOD) && (retval == -2 || dret[0] > tjd0 + dsynperiod * 1.5)) {
|
||
|
strcpy(serr, "no heliacal date found within this synodic period");
|
||
|
retval = -2;
|
||
|
} else if (retval == -2) {
|
||
|
sprintf(serr, "no heliacal date found within %d synodic periods", MaxCountSynodicPeriod);
|
||
|
retval = ERR;
|
||
|
}
|
||
|
if (serr_ret != NULL && *serr != '\0')
|
||
|
strcpy(serr_ret, serr);
|
||
|
return retval;
|
||
|
}
|