/************************************************************
  $Header: /home/dieter/sweph/RCS/swephexp.h,v 1.75 2009/04/08 07:19:08 dieter Exp $
  SWISSEPH: exported definitions and constants 

  This file represents the standard application interface (API)
  to the Swiss Ephemeris.

  A C programmer needs only to include this file, and link his code
  with the SwissEph library.

  The function calls are documented in the Programmer's documentation,
  which is online in HTML format.

  Structure of this file:
    Public API definitions
    Internal developer's definitions
    Public API functions.

  Authors: Dieter Koch and Alois Treindl, Astrodienst Zurich

************************************************************/
/* Copyright (C) 1997 - 2008 Astrodienst AG, Switzerland.  All rights reserved.

  License conditions
  ------------------

  This file is part of Swiss Ephemeris.

  Swiss Ephemeris is distributed with NO WARRANTY OF ANY KIND.  No author
  or distributor accepts any responsibility for the consequences of using it,
  or for whether it serves any particular purpose or works at all, unless he
  or she says so in writing.  

  Swiss Ephemeris is made available by its authors under a dual licensing
  system. The software developer, who uses any part of Swiss Ephemeris
  in his or her software, must choose between one of the two license models,
  which are
  a) GNU public license version 2 or later
  b) Swiss Ephemeris Professional License

  The choice must be made before the software developer distributes software
  containing parts of Swiss Ephemeris to others, and before any public
  service using the developed software is activated.

  If the developer choses the GNU GPL software license, he or she must fulfill
  the conditions of that license, which includes the obligation to place his
  or her whole software project under the GNU GPL or a compatible license.
  See http://www.gnu.org/licenses/old-licenses/gpl-2.0.html

  If the developer choses the Swiss Ephemeris Professional license,
  he must follow the instructions as found in http://www.astro.com/swisseph/ 
  and purchase the Swiss Ephemeris Professional Edition from Astrodienst
  and sign the corresponding license contract.

  The License grants you the right to use, copy, modify and redistribute
  Swiss Ephemeris, but only under certain conditions described in the License.
  Among other things, the License requires that the copyright notices and
  this notice be preserved on all copies.

  Authors of the Swiss Ephemeris: Dieter Koch and Alois Treindl

  The authors of Swiss Ephemeris have no control or influence over any of
  the derived works, i.e. over software or services created by other
  programmers which use Swiss Ephemeris functions.

  The names of the authors or of the copyright holder (Astrodienst) must not
  be used for promoting any software, product or service which uses or contains
  the Swiss Ephemeris. This copyright notice is the ONLY place where the
  names of the authors can legally appear, except in cases where they have
  given special permission in writing.

  The trademarks 'Swiss Ephemeris' and 'Swiss Ephemeris inside' may be used
  for promoting such software, products or services.
*/

#ifdef __cplusplus
extern "C" {
#endif

#ifndef _SWEPHEXP_INCLUDED      /* allow multiple #includes of swephexp.h */
#define _SWEPHEXP_INCLUDED

#include "sweodef.h"

/***********************************************************
 * definitions for use also by non-C programmers
 ***********************************************************/

#define SE_AUNIT_TO_KM        (149597870.700)
#define SE_AUNIT_TO_LIGHTYEAR (1.0/63241.07708427)
#define SE_AUNIT_TO_PARSEC    (1.0/206264.8062471) 

/* values for gregflag in swe_julday() and swe_revjul() */
# define SE_JUL_CAL	0
# define SE_GREG_CAL	1

/*
 * planet numbers for the ipl parameter in swe_calc()
 */
#define SE_ECL_NUT      -1      

#define SE_SUN          0       
#define SE_MOON         1       
#define SE_MERCURY      2       
#define SE_VENUS        3       
#define SE_MARS         4       
#define SE_JUPITER      5       
#define SE_SATURN       6       
#define SE_URANUS       7       
#define SE_NEPTUNE      8       
#define SE_PLUTO        9       
#define SE_MEAN_NODE    10      
#define SE_TRUE_NODE    11
#define SE_MEAN_APOG    12      
#define SE_OSCU_APOG    13    
#define SE_EARTH        14      
#define SE_CHIRON       15      
#define SE_PHOLUS       16      
#define SE_CERES        17      
#define SE_PALLAS       18      
#define SE_JUNO         19      
#define SE_VESTA        20      
#define SE_INTP_APOG    21      
#define SE_INTP_PERG    22    

#define SE_NPLANETS     23      

#define SE_AST_OFFSET   10000
#define SE_VARUNA   (SE_AST_OFFSET + 20000)

#define SE_FICT_OFFSET  	40
#define SE_FICT_OFFSET_1  	39
#define SE_FICT_MAX  	       999 
#define SE_NFICT_ELEM           15

#define SE_COMET_OFFSET 1000

#define SE_NALL_NAT_POINTS      (SE_NPLANETS + SE_NFICT_ELEM)

/* Hamburger or Uranian "planets" */
#define SE_CUPIDO       	40
#define SE_HADES        	41
#define SE_ZEUS         	42
#define SE_KRONOS       	43
#define SE_APOLLON      	44
#define SE_ADMETOS      	45
#define SE_VULKANUS     	46
#define SE_POSEIDON     	47
/* other fictitious bodies */
#define SE_ISIS         	48
#define SE_NIBIRU       	49
#define SE_HARRINGTON           50
#define SE_NEPTUNE_LEVERRIER    51
#define SE_NEPTUNE_ADAMS        52
#define SE_PLUTO_LOWELL         53
#define SE_PLUTO_PICKERING      54
#define SE_VULCAN      		55
#define SE_WHITE_MOON  		56
#define SE_PROSERPINA  		57
#define SE_WALDEMATH  		58

#define SE_FIXSTAR      -10

#define SE_ASC			0
#define SE_MC			1
#define SE_ARMC			2
#define SE_VERTEX		3
#define SE_EQUASC  		4	/* "equatorial ascendant" */
#define SE_COASC1		5	/* "co-ascendant" (W. Koch) */
#define SE_COASC2		6	/* "co-ascendant" (M. Munkasey) */
#define SE_POLASC		7	/* "polar ascendant" (M. Munkasey) */
#define SE_NASCMC		8

/*
 * flag bits for parameter iflag in function swe_calc()
 * The flag bits are defined in such a way that iflag = 0 delivers what one
 * usually wants:
 *    - the default ephemeris (SWISS EPHEMERIS) is used,
 *    - apparent geocentric positions referring to the true equinox of date
 *      are returned.
 * If not only coordinates, but also speed values are required, use 
 * flag = SEFLG_SPEED.
 *
 * The 'L' behind the number indicates that 32-bit integers (Long) are used.
 */
#define SEFLG_JPLEPH    1       /* use JPL ephemeris */
#define SEFLG_SWIEPH    2       /* use SWISSEPH ephemeris */
#define SEFLG_MOSEPH    4       /* use Moshier ephemeris */

#define SEFLG_HELCTR	8      /* heliocentric position */
#define SEFLG_TRUEPOS	16     /* true/geometric position, not apparent position */
#define SEFLG_J2000	32     /* no precession, i.e. give J2000 equinox */
#define SEFLG_NONUT	64     /* no nutation, i.e. mean equinox of date */
#define SEFLG_SPEED3	128    /* speed from 3 positions (do not use it,
                                * SEFLG_SPEED is faster and more precise.) */
#define SEFLG_SPEED	256    /* high precision speed  */
#define SEFLG_NOGDEFL	512    /* turn off gravitational deflection */
#define SEFLG_NOABERR	1024   /* turn off 'annual' aberration of light */
#define SEFLG_ASTROMETRIC (SEFLG_NOABERR|SEFLG_NOGDEFL) /* astrometric position,
                                * i.e. with light-time, but without aberration and
			        * light deflection */
#define SEFLG_EQUATORIAL (2*1024)    /* equatorial positions are wanted */
#define SEFLG_XYZ	(4*1024)     /* cartesian, not polar, coordinates */
#define SEFLG_RADIANS	(8*1024)     /* coordinates in radians, not degrees */
#define SEFLG_BARYCTR	(16*1024)    /* barycentric position */
#define SEFLG_TOPOCTR	(32*1024)    /* topocentric position */
#define SEFLG_ORBEL_AA SEFLG_TOPOCTR /* used for Astronomical Almanac mode in 
                                      * calculation of Kepler elipses */
#define SEFLG_SIDEREAL	(64*1024)    /* sidereal position */
#define SEFLG_ICRS	(128*1024)   /* ICRS (DE406 reference frame) */
#define SEFLG_DPSIDEPS_1980	(256*1024) /* reproduce JPL Horizons 
                                      * 1962 - today to 0.002 arcsec. */
#define SEFLG_JPLHOR	SEFLG_DPSIDEPS_1980
#define SEFLG_JPLHOR_APPROX	(512*1024)   /* approximate JPL Horizons 1962 - today */

#define SE_SIDBITS		256
/* for projection onto ecliptic of t0 */
#define SE_SIDBIT_ECL_T0        256
/* for projection onto solar system plane */
#define SE_SIDBIT_SSY_PLANE     512
/* with user-defined ayanamsha, t0 is UT */
#define SE_SIDBIT_USER_UT       1024

/* sidereal modes (ayanamsas) */
#define SE_SIDM_FAGAN_BRADLEY    0
#define SE_SIDM_LAHIRI           1
#define SE_SIDM_DELUCE           2
#define SE_SIDM_RAMAN            3
#define SE_SIDM_USHASHASHI       4
#define SE_SIDM_KRISHNAMURTI     5
#define SE_SIDM_DJWHAL_KHUL      6
#define SE_SIDM_YUKTESHWAR       7
#define SE_SIDM_JN_BHASIN        8
#define SE_SIDM_BABYL_KUGLER1    9
#define SE_SIDM_BABYL_KUGLER2   10
#define SE_SIDM_BABYL_KUGLER3   11
#define SE_SIDM_BABYL_HUBER    	12
#define SE_SIDM_BABYL_ETPSC    	13
#define SE_SIDM_ALDEBARAN_15TAU 14
#define SE_SIDM_HIPPARCHOS      15
#define SE_SIDM_SASSANIAN       16
#define SE_SIDM_GALCENT_0SAG    17
#define SE_SIDM_J2000           18
#define SE_SIDM_J1900           19
#define SE_SIDM_B1950           20
#define SE_SIDM_SURYASIDDHANTA  21
#define SE_SIDM_SURYASIDDHANTA_MSUN  22
#define SE_SIDM_ARYABHATA       23
#define SE_SIDM_ARYABHATA_MSUN  24
#define SE_SIDM_SS_REVATI       25
#define SE_SIDM_SS_CITRA        26
#define SE_SIDM_TRUE_CITRA      27
#define SE_SIDM_TRUE_REVATI     28
#define SE_SIDM_TRUE_PUSHYA     29
#define SE_SIDM_GALCENT_RGILBRAND 30
#define SE_SIDM_GALEQU_IAU1958  31
#define SE_SIDM_GALEQU_TRUE     32
#define SE_SIDM_GALEQU_MULA     33
#define SE_SIDM_GALALIGN_MARDYKS 34
#define SE_SIDM_TRUE_MULA       35
#define SE_SIDM_GALCENT_MULA_WILHELM       36
#define SE_SIDM_ARYABHATA_522   37
#define SE_SIDM_BABYL_BRITTON   38
#define SE_SIDM_TRUE_SHEORAN  	39
#define SE_SIDM_GALCENT_COCHRANE   	40
#define SE_SIDM_GALEQU_FIORENZA 41
#define SE_SIDM_VALENS_MOON     42
//#define SE_SIDM_MANJULA         43
#define SE_SIDM_USER            255 /* user-defined ayanamsha, t0 is TT */

#define SE_NSIDM_PREDEF	        43

/* used for swe_nod_aps(): */
#define SE_NODBIT_MEAN		1   /* mean nodes/apsides */
#define SE_NODBIT_OSCU		2   /* osculating nodes/apsides */
#define SE_NODBIT_OSCU_BAR	4   /* same, but motion about solar system barycenter is considered */
#define SE_NODBIT_FOPOINT	256   /* focal point of orbit instead of aphelion */

/* default ephemeris used when no ephemeris flagbit is set */
#define SEFLG_DEFAULTEPH SEFLG_SWIEPH

#define SE_MAX_STNAME		256	/* maximum size of fixstar name;
                                         * the parameter star in swe_fixstar
					 * must allow twice this space for
				         * the returned star name.
					 */

/* defines for eclipse computations */

#define SE_ECL_CENTRAL		1
#define SE_ECL_NONCENTRAL	2
#define SE_ECL_TOTAL		4
#define SE_ECL_ANNULAR		8
#define SE_ECL_PARTIAL		16
#define SE_ECL_ANNULAR_TOTAL	32
#define SE_ECL_PENUMBRAL	64
#define SE_ECL_ALLTYPES_SOLAR   (SE_ECL_CENTRAL|SE_ECL_NONCENTRAL|SE_ECL_TOTAL|SE_ECL_ANNULAR|SE_ECL_PARTIAL|SE_ECL_ANNULAR_TOTAL)
#define SE_ECL_ALLTYPES_LUNAR   (SE_ECL_TOTAL|SE_ECL_PARTIAL|SE_ECL_PENUMBRAL)
#define SE_ECL_VISIBLE			128
#define SE_ECL_MAX_VISIBLE		256
#define SE_ECL_1ST_VISIBLE		512	/* begin of partial eclipse */
#define SE_ECL_PARTBEG_VISIBLE		512	/* begin of partial eclipse */
#define SE_ECL_2ND_VISIBLE		1024	/* begin of total eclipse */
#define SE_ECL_TOTBEG_VISIBLE		1024	/* begin of total eclipse */
#define SE_ECL_3RD_VISIBLE		2048    /* end of total eclipse */
#define SE_ECL_TOTEND_VISIBLE		2048    /* end of total eclipse */
#define SE_ECL_4TH_VISIBLE		4096    /* end of partial eclipse */
#define SE_ECL_PARTEND_VISIBLE		4096    /* end of partial eclipse */
#define SE_ECL_PENUMBBEG_VISIBLE	8192    /* begin of penumbral eclipse */
#define SE_ECL_PENUMBEND_VISIBLE	16384   /* end of penumbral eclipse */
#define SE_ECL_OCC_BEG_DAYLIGHT		8192    /* occultation begins during the day */
#define SE_ECL_OCC_END_DAYLIGHT		16384   /* occultation ends during the day */
#define SE_ECL_ONE_TRY          (32*1024) 
		/* check if the next conjunction of the moon with
		 * a planet is an occultation; don't search further */

/* for swe_rise_transit() */
#define SE_CALC_RISE		1
#define SE_CALC_SET		2
#define SE_CALC_MTRANSIT	4
#define SE_CALC_ITRANSIT	8
#define SE_BIT_DISC_CENTER      256 /* to be or'ed to SE_CALC_RISE/SET,
				     * if rise or set of disc center is 
				     * required */
#define SE_BIT_DISC_BOTTOM      8192 /* to be or'ed to SE_CALC_RISE/SET,
                                      * if rise or set of lower limb of 
				      * disc is requried */
#define SE_BIT_GEOCTR_NO_ECL_LAT 128 /* use geocentric rather than topocentric 
                                        position of object and 
					ignore its ecliptic latitude */
#define SE_BIT_NO_REFRACTION    512 /* to be or'ed to SE_CALC_RISE/SET, 
				     * if refraction is to be ignored */
#define SE_BIT_CIVIL_TWILIGHT    1024 /* to be or'ed to SE_CALC_RISE/SET */
#define SE_BIT_NAUTIC_TWILIGHT   2048 /* to be or'ed to SE_CALC_RISE/SET */
#define SE_BIT_ASTRO_TWILIGHT    4096 /* to be or'ed to SE_CALC_RISE/SET */
#define SE_BIT_FIXED_DISC_SIZE  16384 /* or'ed to SE_CALC_RISE/SET:
                                     * neglect the effect of distance on
				     * disc size */
#define SE_BIT_FORCE_SLOW_METHOD 32768 /* This is only an Astrodienst in-house
                                        * test flag. It forces the usage
					* of the old, slow calculation of
					* risings and settings. */
#define SE_BIT_HINDU_RISING  (SE_BIT_DISC_CENTER|SE_BIT_NO_REFRACTION|SE_BIT_GEOCTR_NO_ECL_LAT)

/* for swe_azalt() and swe_azalt_rev() */
#define SE_ECL2HOR		0
#define SE_EQU2HOR		1
#define SE_HOR2ECL		0
#define SE_HOR2EQU		1

/* for swe_refrac() */
#define SE_TRUE_TO_APP	0
#define SE_APP_TO_TRUE	1

/*
 * only used for experimenting with various JPL ephemeris files
 * which are available at Astrodienst's internal network
 */
#define SE_DE_NUMBER    431
#define SE_FNAME_DE200  "de200.eph"
#define SE_FNAME_DE403  "de403.eph"
#define SE_FNAME_DE404  "de404.eph"
#define SE_FNAME_DE405  "de405.eph"
#define SE_FNAME_DE406  "de406.eph"
#define SE_FNAME_DE431  "de431.eph"
#define SE_FNAME_DFT    SE_FNAME_DE431
#define SE_FNAME_DFT2   SE_FNAME_DE406
#define SE_STARFILE_OLD "fixstars.cat"
#define SE_STARFILE     "sefstars.txt"
#define SE_ASTNAMFILE   "seasnam.txt"
#define SE_FICTFILE     "seorbel.txt"

/*
 * ephemeris path
 * this defines where ephemeris files are expected if the function
 * swe_set_ephe_path() is not called by the application.
 * Normally, every application should make this call to define its
 * own place for the ephemeris files.
 */

#ifndef SE_EPHE_PATH
#if MSDOS
#  define SE_EPHE_PATH    "\\sweph\\ephe\\"
#else
# ifdef MACOS
#  define SE_EPHE_PATH	":ephe:"
# else
#  define SE_EPHE_PATH    ".:/users/ephe2/:/users/ephe/"
			/* At Astrodienst, we maintain two ephemeris areas for
			   the thousands of asteroid files: 
			   the short files in /users/ephe/ast*,
			   the long file in /users/ephe2/ast*. */
# endif
#endif
#endif  /* SE_EPHE_PATH */

/* defines for function swe_split_deg() (in swephlib.c) */
# define SE_SPLIT_DEG_ROUND_SEC    1
# define SE_SPLIT_DEG_ROUND_MIN    2
# define SE_SPLIT_DEG_ROUND_DEG    4
# define SE_SPLIT_DEG_ZODIACAL     8
# define SE_SPLIT_DEG_NAKSHATRA 1024
# define SE_SPLIT_DEG_KEEP_SIGN   16	/* don't round to next sign, 
					 * e.g. 29.9999999 will be rounded
					 * to 29d59'59" (or 29d59' or 29d) */
# define SE_SPLIT_DEG_KEEP_DEG    32	/* don't round to next degree
					 * e.g. 13.9999999 will be rounded
					 * to 13d59'59" (or 13d59' or 13d) */

/* for heliacal functions */
#define SE_HELIACAL_RISING		1
#define SE_HELIACAL_SETTING		2
#define SE_MORNING_FIRST		SE_HELIACAL_RISING
#define SE_EVENING_LAST			SE_HELIACAL_SETTING
#define SE_EVENING_FIRST		3
#define SE_MORNING_LAST			4
#define SE_ACRONYCHAL_RISING		5  /* still not implemented */
#define SE_ACRONYCHAL_SETTING		6  /* still not implemented */
#define SE_COSMICAL_SETTING		SE_ACRONYCHAL_SETTING

#define SE_HELFLAG_LONG_SEARCH 		128
#define SE_HELFLAG_HIGH_PRECISION 	256
#define SE_HELFLAG_OPTICAL_PARAMS	512
#define SE_HELFLAG_NO_DETAILS		1024
#define SE_HELFLAG_SEARCH_1_PERIOD	(1 << 11)  /*  2048 */
#define SE_HELFLAG_VISLIM_DARK		(1 << 12)  /*  4096 */
#define SE_HELFLAG_VISLIM_NOMOON	(1 << 13)  /*  8192 */
/* the following undocumented defines are for test reasons only */
#define SE_HELFLAG_VISLIM_PHOTOPIC	(1 << 14)  /* 16384 */
#define SE_HELFLAG_VISLIM_SCOTOPIC	(1 << 15)  /* 32768 */
#define SE_HELFLAG_AV	 		(1 << 16)  /* 65536 */
#define SE_HELFLAG_AVKIND_VR 		(1 << 16)  /* 65536 */
#define SE_HELFLAG_AVKIND_PTO 		(1 << 17)
#define SE_HELFLAG_AVKIND_MIN7 		(1 << 18)
#define SE_HELFLAG_AVKIND_MIN9 		(1 << 19)
#define SE_HELFLAG_AVKIND (SE_HELFLAG_AVKIND_VR|SE_HELFLAG_AVKIND_PTO|SE_HELFLAG_AVKIND_MIN7|SE_HELFLAG_AVKIND_MIN9)
#define TJD_INVALID		 	99999999.0
#define SIMULATE_VICTORVB               1

#if 0  // unused and redundant
#define SE_HELIACAL_LONG_SEARCH 	128
#define SE_HELIACAL_HIGH_PRECISION 	256
#define SE_HELIACAL_OPTICAL_PARAMS	512
#define SE_HELIACAL_NO_DETAILS		1024
#define SE_HELIACAL_SEARCH_1_PERIOD	(1 << 11)  /*  2048 */
#define SE_HELIACAL_VISLIM_DARK		(1 << 12)  /*  4096 */
#define SE_HELIACAL_VISLIM_NOMOON	(1 << 13)  /*  8192 */
#define SE_HELIACAL_VISLIM_PHOTOPIC	(1 << 14)  /* 16384 */
#define SE_HELIACAL_AVKIND_VR 		(1 << 15)  /* 32768 */
#define SE_HELIACAL_AVKIND_PTO 		(1 << 16)
#define SE_HELIACAL_AVKIND_MIN7 		(1 << 17)
#define SE_HELIACAL_AVKIND_MIN9 		(1 << 18)
#define SE_HELIACAL_AVKIND (SE_HELFLAG_AVKIND_VR|SE_HELFLAG_AVKIND_PTO|SE_HELFLAG_AVKIND_MIN7|SE_HELFLAG_AVKIND_MIN9)
#endif

#define SE_PHOTOPIC_FLAG		0
#define SE_SCOTOPIC_FLAG		1
#define SE_MIXEDOPIC_FLAG		2

/* for swe_set_tid_acc() and ephemeris-dependent delta t:
 * intrinsic tidal acceleration in the mean motion of the moon,
 * not given in the parameters list of the ephemeris files but computed
 * by Chapront/Chapront-Touze/Francou A&A 387 (2002), p. 705.
 */
#define SE_TIDAL_DE200          (-23.8946)
#define SE_TIDAL_DE403          (-25.580)  /* was (-25.8) until V. 1.76.2 */
#define SE_TIDAL_DE404          (-25.580)  /* was (-25.8) until V. 1.76.2 */
#define SE_TIDAL_DE405          (-25.826)  /* was (-25.7376) until V. 1.76.2 */
#define SE_TIDAL_DE406          (-25.826)  /* was (-25.7376) until V. 1.76.2 */
#define SE_TIDAL_DE421          (-25.85)   /* JPL Interoffice Memorandum 14-mar-2008 on DE421 Lunar Orbit */
#define SE_TIDAL_DE422          (-25.85)   /* JPL Interoffice Memorandum 14-mar-2008 on DE421 (sic!) Lunar Orbit */
#define SE_TIDAL_DE430          (-25.82)   /* JPL Interoffice Memorandum 9-jul-2013 on DE430 Lunar Orbit */
#define SE_TIDAL_DE431          (-25.80)   /* IPN Progress Report 42-196, February 15, 2014, p. 15; was (-25.82) in V. 2.00.00 */
#define SE_TIDAL_26             (-26.0)
#define SE_TIDAL_STEPHENSON_2016             (-25.85)
#define SE_TIDAL_DEFAULT        SE_TIDAL_DE431
#define SE_TIDAL_AUTOMATIC             999999
#define SE_TIDAL_MOSEPH                SE_TIDAL_DE404
#define SE_TIDAL_SWIEPH                SE_TIDAL_DEFAULT
#define SE_TIDAL_JPLEPH                SE_TIDAL_DEFAULT

/* for function swe_set_delta_t_userdef() */
#define SE_DELTAT_AUTOMATIC             (-1E-10)

#define SE_MODEL_DELTAT         0
#define SE_MODEL_PREC_LONGTERM  1
#define SE_MODEL_PREC_SHORTTERM 2
#define SE_MODEL_NUT            3
#define SE_MODEL_BIAS           4
#define SE_MODEL_JPLHOR_MODE    5
#define SE_MODEL_JPLHORA_MODE   6
#define SE_MODEL_SIDT           7
#define NSE_MODELS              8

/* precession models */
#define SEMOD_NPREC		10
#define SEMOD_PREC_IAU_1976      1
#define SEMOD_PREC_LASKAR_1986   2
#define SEMOD_PREC_WILL_EPS_LASK 3
#define SEMOD_PREC_WILLIAMS_1994 4
#define SEMOD_PREC_SIMON_1994    5
#define SEMOD_PREC_IAU_2000      6
#define SEMOD_PREC_BRETAGNON_2003      7
#define SEMOD_PREC_IAU_2006      8
#define SEMOD_PREC_VONDRAK_2011  9
#define SEMOD_PREC_OWEN_1990     10
#define SEMOD_PREC_DEFAULT       SEMOD_PREC_VONDRAK_2011
/* SE versions before 1.70 used IAU 1976 precession for 
 * a limited time range of 2 centuries in combination with 
 * the long-term precession Simon 1994.
 */
#define SEMOD_PREC_DEFAULT_SHORT SEMOD_PREC_VONDRAK_2011

/* nutation models */
#define SEMOD_NNUT		4
#define SEMOD_NUT_IAU_1980          1
#define SEMOD_NUT_IAU_CORR_1987     2 /* Herring's (1987) corrections to IAU 1980 
				    * nutation series. AA (1996) neglects them.*/
#define SEMOD_NUT_IAU_2000A         3 /* very time consuming ! */
#define SEMOD_NUT_IAU_2000B         4 /* fast, but precision of milli-arcsec */
#define SEMOD_NUT_DEFAULT           SEMOD_NUT_IAU_2000B  /* fast, but precision of milli-arcsec */

/* methods for sidereal time */
#define SEMOD_NSIDT		4
#define SEMOD_SIDT_IAU_1976         1
#define SEMOD_SIDT_IAU_2006         2
#define SEMOD_SIDT_IERS_CONV_2010   3
#define SEMOD_SIDT_LONGTERM         4
#define SEMOD_SIDT_DEFAULT          SEMOD_SIDT_LONGTERM
//#define SEMOD_SIDT_DEFAULT          SEMOD_SIDT_IERS_CONV_2010

/* frame bias methods */
#define SEMOD_NBIAS		3
#define SEMOD_BIAS_NONE             1  /* ignore frame bias */
#define SEMOD_BIAS_IAU2000          2  /* use frame bias matrix IAU 2000 */
#define SEMOD_BIAS_IAU2006          3  /* use frame bias matrix IAU 2006 */
#define SEMOD_BIAS_DEFAULT          SEMOD_BIAS_IAU2006

/* methods of JPL Horizons (iflag & SEFLG_JPLHOR), 
 * using daily dpsi, deps;  see explanations below */
#define SEMOD_NJPLHOR		2
#define SEMOD_JPLHOR_LONG_AGREEMENT  1  /* daily dpsi and deps from file are 
                                     * limited to 1962 - today. JPL uses the
				     * first and last value for all  dates 
				     * beyond this time range. */
#define SEMOD_JPLHOR_DEFAULT        SEMOD_JPLHOR_LONG_AGREEMENT
/* Note, currently this is the only option for SEMOD_JPLHOR..*/
/* SEMOD_JPLHOR_LONG_AGREEMENT, if combined with SEFLG_JPLHOR provides good 
 * agreement with JPL Horizons for 9998 BC (-9997) until 9999 CE. 
 * - After 20-jan-1962 until today, Horizons uses correct dpsi and deps. 
 * - For dates before that, it uses dpsi and deps of 20-jan-1962, which 
 *   provides a continuous ephemeris, but does not make sense otherwise.
 * - Before 1.1.1799 and after 1.1.2202, the precession model Owen 1990
 *   is used, as in Horizons. 
 * An agreement with Horizons to a couple of milli arc seconds is achieved 
 * for the whole time range of Horizons. (BC 9998-Mar-20 to AD 9999-Dec-31 TT.)
 */

/* methods of approximation of JPL Horizons (iflag & SEFLG_JPLHORA), 
 * without dpsi, deps; see explanations below */
#define SEMOD_NJPLHORA		3
#define SEMOD_JPLHORA_1     1
#define SEMOD_JPLHORA_2     2
#define SEMOD_JPLHORA_3     3
#define SEMOD_JPLHORA_DEFAULT     SEMOD_JPLHORA_3
/* With SEMOD_JPLHORA_1, planetary positions are always calculated 
 * using a recent precession/nutation model. Frame bias matrix is applied 
 * with some correction to RA and another correction added to epsilon.
 * This provides a very good approximation of JPL Horizons positions. 
 *
 * With SEMOD_JPLHORA_2, frame bias as recommended by IERS Conventions 2003 
 * and 2010 is *not* applied. Instead, dpsi_bias and deps_bias are added to 
 * nutation. This procedure is found in some older astronomical software.
 * Equatorial apparent positions will be close to JPL Horizons 
 * (within a few mas) between 1962 and current years. Ecl. longitude 
 * will be good, latitude bad. 
 *
 * With SEMOD_JPLHORA_3 works like SEMOD_JPLHORA_3 after 1962, but like
 * SEFLG_JPLHOR before that. This allows EXTREMELY good agreement with JPL 
 * Horizons over its whole time range.
 */

#define SEMOD_NDELTAT		5
#define SEMOD_DELTAT_STEPHENSON_MORRISON_1984   1
#define SEMOD_DELTAT_STEPHENSON_1997   2
#define SEMOD_DELTAT_STEPHENSON_MORRISON_2004   3
#define SEMOD_DELTAT_ESPENAK_MEEUS_2006   4
#define SEMOD_DELTAT_STEPHENSON_ETC_2016   5
//#define SEMOD_DELTAT_DEFAULT   SEMOD_DELTAT_ESPENAK_MEEUS_2006
#define SEMOD_DELTAT_DEFAULT   SEMOD_DELTAT_STEPHENSON_ETC_2016

/**************************************************************
 * here follow some ugly definitions which are only required
 * if SwissEphemeris is compiled on Windows, either to use a DLL
 * or to create a DLL.
 * Unix users can savely ignore his section
 * and skip to the export function decarations below.
 ************************************************************/
#if defined(MAKE_DLL) || defined(USE_DLL) || defined(_WINDOWS)
#  include <windows.h>
extern HANDLE dllhandle;        // set by swedllst::DllMain, 
				// defined in sweph.c
				// used by GetModuleFilename in sweph.c
#endif

#ifdef USE_DLL
#  include "swedll.h"
#endif

#if defined(DOS32) || !MSDOS || defined(WIN32)
			/* use compiler switch to define DOS32 */
#  define MALLOC malloc  
#  define CALLOC calloc  
#  define FREE free  
#else
#  ifdef __BORLANDC__
#    include <alloc.h>
#    define MALLOC farmalloc  
#    define CALLOC farcalloc  
#    define FREE farfree  
#  else
#    define MALLOC _fmalloc
#    define CALLOC _fcalloc
#    define FREE _ffree
#  endif
#endif

/* DLL defines
  Define UNDECO_DLL for un-decorated dll
  verify compiler option __cdecl for un-decorated and __stdcall for decorated */
/*#define UNDECO_DLL*/
#ifdef MAKE_DLL
  #if defined (PASCAL) || defined(__stdcall)
   #if defined UNDECO_DLL
    #define CALL_CONV __cdecl
   #else
    #define CALL_CONV __stdcall
   #endif 
  #else
    #define CALL_CONV 
  #endif
  /* To export symbols in the new DLL model of Win32, Microsoft 
     recommends the following approach */ 
  #define EXP32  __declspec( dllexport )
#else 
  #define CALL_CONV 
  #define EXP32 
#endif  


#ifndef _SWEDLL_H

/***********************************************************
 * exported functions
 ***********************************************************/

#define ext_def(x)	extern EXP32 x CALL_CONV 
			/* ext_def(x) evaluates to x on Unix */

ext_def(int32) swe_heliacal_ut(double tjdstart_ut, double *geopos, double *datm, double *dobs, char *ObjectName, int32 TypeEvent, int32 iflag, double *dret, char *serr);
ext_def(int32) swe_heliacal_pheno_ut(double tjd_ut, double *geopos, double *datm, double *dobs, char *ObjectName, int32 TypeEvent, int32 helflag, double *darr, char *serr);
ext_def(int32) swe_vis_limit_mag(double tjdut, double *geopos, double *datm, double *dobs, char *ObjectName, int32 helflag, double *dret, char *serr);

/* the following are secret, for Victor Reijs' */
ext_def(int32) 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);
ext_def(int32) 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);

/* the following is secret, for Dieter, allows to test old models of
 * precession, nutation, etc. Search for SE_MODEL_... in this file */
ext_def(void) swe_set_astro_models(char *samod, int32 iflag);
ext_def(void) swe_get_astro_models(char *samod, char *sdet, int32 iflag);

/**************************** 
 * exports from sweph.c 
 ****************************/

ext_def(char *) swe_version(char *);
ext_def(char *) swe_get_library_path(char *);

/* planets, moon, nodes etc. */
ext_def( int32 ) swe_calc(
        double tjd, int ipl, int32 iflag, 
        double *xx,
        char *serr);

ext_def(int32) swe_calc_ut(double tjd_ut, int32 ipl, int32 iflag, 
	double *xx, char *serr);

/* fixed stars */
ext_def( int32 ) swe_fixstar(
        char *star, double tjd, int32 iflag, 
        double *xx,
        char *serr);

ext_def(int32) swe_fixstar_ut(char *star, double tjd_ut, int32 iflag, 
	double *xx, char *serr);

ext_def(int32) swe_fixstar_mag(char *star, double *mag, char *serr);

ext_def( int32 ) swe_fixstar2(
        char *star, double tjd, int32 iflag, 
        double *xx,
        char *serr);

ext_def(int32) swe_fixstar2_ut(char *star, double tjd_ut, int32 iflag, 
	double *xx, char *serr);

ext_def(int32) swe_fixstar2_mag(char *star, double *mag, char *serr);

/* close Swiss Ephemeris */
ext_def( void ) swe_close(void);

/* set directory path of ephemeris files */
ext_def( void ) swe_set_ephe_path(char *path);

/* set file name of JPL file */
ext_def( void ) swe_set_jpl_file(char *fname);

/* get planet name */
ext_def( char *) swe_get_planet_name(int ipl, char *spname);

/* set geographic position of observer */
ext_def (void) swe_set_topo(double geolon, double geolat, double geoalt);

/* set sidereal mode */
ext_def(void) swe_set_sid_mode(int32 sid_mode, double t0, double ayan_t0);

/* get ayanamsa */
ext_def(int32) swe_get_ayanamsa_ex(double tjd_et, int32 iflag, double *daya, char *serr);
ext_def(int32) swe_get_ayanamsa_ex_ut(double tjd_ut, int32 iflag, double *daya, char *serr);
ext_def(double) swe_get_ayanamsa(double tjd_et);
ext_def(double) swe_get_ayanamsa_ut(double tjd_ut);


ext_def(const char *) swe_get_ayanamsa_name(int32 isidmode);

/*ext_def(void) swe_set_timeout(int32 tsec);*/

/**************************** 
 * exports from swedate.c 
 ****************************/

ext_def( int ) swe_date_conversion(
        int y , int m , int d ,         /* year, month, day */
        double utime,   /* universal time in hours (decimal) */
        char c,         /* calendar g[regorian]|j[ulian] */
        double *tjd);

ext_def( double ) swe_julday(
        int year, int month, int day, double hour, 
        int gregflag);

ext_def( void ) swe_revjul (
        double jd, 
        int gregflag,
        int *jyear, int *jmon, int *jday, double *jut);

ext_def(int32) swe_utc_to_jd(
        int32 iyear, int32 imonth, int32 iday, 
	int32 ihour, int32 imin, double dsec, 
	int32 gregflag, double *dret, char *serr);

ext_def(void) swe_jdet_to_utc(
        double tjd_et, int32 gregflag, 
	int32 *iyear, int32 *imonth, int32 *iday, 
	int32 *ihour, int32 *imin, double *dsec);

ext_def(void) swe_jdut1_to_utc(
        double tjd_ut, int32 gregflag, 
	int32 *iyear, int32 *imonth, int32 *iday, 
	int32 *ihour, int32 *imin, double *dsec);

ext_def(void) swe_utc_time_zone(
        int32 iyear, int32 imonth, int32 iday,
	int32 ihour, int32 imin, double dsec,
	double d_timezone,
	int32 *iyear_out, int32 *imonth_out, int32 *iday_out,
	int32 *ihour_out, int32 *imin_out, double *dsec_out);

/**************************** 
 * exports from swehouse.c 
 ****************************/

ext_def( int ) swe_houses(
        double tjd_ut, double geolat, double geolon, int hsys, 
	double *cusps, double *ascmc);

ext_def( int ) swe_houses_ex(
        double tjd_ut, int32 iflag, double geolat, double geolon, int hsys, 
	double *cusps, double *ascmc);

ext_def( int ) swe_houses_armc(
        double armc, double geolat, double eps, int hsys, 
	double *cusps, double *ascmc);

ext_def(double) swe_house_pos(
	double armc, double geolat, double eps, int hsys, double *xpin, char *serr);

ext_def(char *) swe_house_name(int hsys);



/**************************** 
 * exports from swecl.c 
 ****************************/

ext_def(int32) swe_gauquelin_sector(double t_ut, int32 ipl, char *starname, int32 iflag, int32 imeth, double *geopos, double atpress, double attemp, double *dgsect, char *serr);

/* computes geographic location and attributes of solar 
 * eclipse at a given tjd */
ext_def (int32) swe_sol_eclipse_where(double tjd, int32 ifl, double *geopos, double *attr, char *serr);

ext_def (int32) swe_lun_occult_where(double tjd, int32 ipl, char *starname, int32 ifl, double *geopos, double *attr, char *serr);

/* computes attributes of a solar eclipse for given tjd, geolon, geolat */
ext_def (int32) swe_sol_eclipse_how(double tjd, int32 ifl, double *geopos, double *attr, char *serr);

/* finds time of next local eclipse */
ext_def (int32) swe_sol_eclipse_when_loc(double tjd_start, int32 ifl, double *geopos, double *tret, double *attr, int32 backward, char *serr);

ext_def (int32) swe_lun_occult_when_loc(double tjd_start, int32 ipl, char *starname, int32 ifl,
     double *geopos, double *tret, double *attr, int32 backward, char *serr);

/* finds time of next eclipse globally */
ext_def (int32) swe_sol_eclipse_when_glob(double tjd_start, int32 ifl, int32 ifltype,
     double *tret, int32 backward, char *serr);

/* finds time of next occultation globally */
ext_def (int32) swe_lun_occult_when_glob(double tjd_start, int32 ipl, char *starname, int32 ifl, int32 ifltype,
     double *tret, int32 backward, char *serr);

/* computes attributes of a lunar eclipse for given tjd */
ext_def (int32) swe_lun_eclipse_how(
          double tjd_ut, 
          int32 ifl,
          double *geopos, 
          double *attr, 
          char *serr);

ext_def (int32) swe_lun_eclipse_when(double tjd_start, int32 ifl, int32 ifltype,
     double *tret, int32 backward, char *serr);

ext_def (int32) swe_lun_eclipse_when_loc(double tjd_start, int32 ifl, 
     double *geopos, double *tret, double *attr, int32 backward, char *serr);

/* planetary phenomena */
ext_def (int32) swe_pheno(double tjd, int32 ipl, int32 iflag, double *attr, char *serr);
 
ext_def(int32) swe_pheno_ut(double tjd_ut, int32 ipl, int32 iflag, double *attr, char *serr);

ext_def (double) swe_refrac(double inalt, double atpress, double attemp, int32 calc_flag);

ext_def (double) swe_refrac_extended(double inalt, double geoalt, double atpress, double attemp, double lapse_rate, int32 calc_flag, double *dret);

ext_def (void) swe_set_lapse_rate(double lapse_rate);

ext_def (void) swe_azalt(
      double tjd_ut,
      int32 calc_flag,
      double *geopos,
      double atpress,
      double attemp,
      double *xin, 
      double *xaz); 

ext_def (void) swe_azalt_rev(
      double tjd_ut,
      int32 calc_flag,
      double *geopos,
      double *xin, 
      double *xout); 

ext_def (int32) swe_rise_trans_true_hor(
               double tjd_ut, int32 ipl, char *starname, 
	       int32 epheflag, int32 rsmi,
               double *geopos, 
	       double atpress, double attemp,
	       double horhgt,
               double *tret,
               char *serr);

ext_def (int32) swe_rise_trans(
               double tjd_ut, int32 ipl, char *starname, 
	       int32 epheflag, int32 rsmi,
               double *geopos, 
	       double atpress, double attemp,
               double *tret,
               char *serr);

ext_def (int32) swe_nod_aps(double tjd_et, int32 ipl, int32 iflag, 
                      int32  method,
                      double *xnasc, double *xndsc, 
                      double *xperi, double *xaphe, 
                      char *serr);

ext_def (int32) swe_nod_aps_ut(double tjd_ut, int32 ipl, int32 iflag, 
                      int32  method,
                      double *xnasc, double *xndsc, 
                      double *xperi, double *xaphe, 
                      char *serr);
ext_def (int32) swe_get_orbital_elements(
  double tjd_et, int32 ipl, int32 iflag, double *dret, char *serr);

ext_def (int32) swe_orbit_max_min_true_distance(double tjd_et, int32 ipl, int32 iflag, double *dmax, double *dmin, double *dtrue, char *serr);

/**************************** 
 * exports from swephlib.c 
 ****************************/

/* delta t */
ext_def( double ) swe_deltat(double tjd);
ext_def(double) swe_deltat_ex(double tjd, int32 iflag, char *serr);

/* equation of time */
ext_def(int32) swe_time_equ(double tjd, double *te, char *serr);
ext_def(int32) swe_lmt_to_lat(double tjd_lmt, double geolon, double *tjd_lat, char *serr);
ext_def(int32) swe_lat_to_lmt(double tjd_lat, double geolon, double *tjd_lmt, char *serr);

/* sidereal time */
ext_def( double ) swe_sidtime0(double tjd_ut, double eps, double nut);
ext_def( double ) swe_sidtime(double tjd_ut);
ext_def( void ) swe_set_interpolate_nut(AS_BOOL do_interpolate);

/* coordinate transformation polar -> polar */
ext_def( void ) swe_cotrans(double *xpo, double *xpn, double eps);
ext_def( void ) swe_cotrans_sp(double *xpo, double *xpn, double eps);

/* tidal acceleration to be used in swe_deltat() */
ext_def( double ) swe_get_tid_acc(void);
ext_def( void ) swe_set_tid_acc(double t_acc);

/* set a user defined delta t to be returned by functions
 * swe_deltat() and swe_deltat_ex() */
ext_def (void) swe_set_delta_t_userdef(double dt);

ext_def( double ) swe_degnorm(double x);
ext_def( double ) swe_radnorm(double x);
ext_def( double ) swe_rad_midp(double x1, double x0);
ext_def( double ) swe_deg_midp(double x1, double x0);

ext_def( void ) swe_split_deg(double ddeg, int32 roundflag, int32 *ideg, int32 *imin, int32 *isec, double *dsecfr, int32 *isgn);

/******************************************************* 
 * other functions from swephlib.c;
 * they are not needed for Swiss Ephemeris,
 * but may be useful to former Placalc users.
 ********************************************************/

/* normalize argument into interval [0..DEG360] */
ext_def( centisec ) swe_csnorm(centisec p);

/* distance in centisecs p1 - p2 normalized to [0..360[ */
ext_def( centisec ) swe_difcsn (centisec p1, centisec p2);

ext_def( double ) swe_difdegn (double p1, double p2);

/* distance in centisecs p1 - p2 normalized to [-180..180[ */
ext_def( centisec ) swe_difcs2n(centisec p1, centisec p2);

ext_def( double ) swe_difdeg2n(double p1, double p2);
ext_def( double ) swe_difrad2n(double p1, double p2);

/* round second, but at 29.5959 always down */
ext_def( centisec ) swe_csroundsec(centisec x);

/* double to int32 with rounding, no overflow check */
ext_def( int32 ) swe_d2l(double x);

/* monday = 0, ... sunday = 6 */
ext_def( int ) swe_day_of_week(double jd);

ext_def( char *) swe_cs2timestr(CSEC t, int sep, AS_BOOL suppressZero, char *a);

ext_def( char *) swe_cs2lonlatstr(CSEC t, char pchar, char mchar, char *s);

ext_def( char *) swe_cs2degstr(CSEC t, char *a);

#endif  /* #ifndef _SWEDLL_H */

#endif  /* #ifndef _SWEPHEXP_INCLUDED */

#ifdef __cplusplus
} /* extern C */
#endif
