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SuperNOVAS: src/coords.c File Reference

int  ecl2equ (double jd_tt, enum novas_equator_type coord_sys, enum novas_accuracy accuracy, double elon, double elat, double *restrict ra, double *restrict dec)   short  ecl2equ_vec (double jd_tt, enum novas_equator_type coord_sys, enum novas_accuracy accuracy, const double *in, double *out)   short  equ2ecl (double jd_tt, enum novas_equator_type coord_sys, enum novas_accuracy accuracy, double ra, double dec, double *restrict elon, double *restrict elat)   short  equ2ecl_vec (double jd_tt, enum novas_equator_type coord_sys, enum novas_accuracy accuracy, const double *in, double *out)   int  equ2gal (double ra, double dec, double *restrict glon, double *restrict glat)   int  equ2hor (double jd_ut1, double ut1_to_tt, enum novas_accuracy accuracy, double xp, double yp, const on_surface *restrict location, double ra, double dec, enum novas_refraction_model ref_option, double *restrict zd, double *restrict az, double *restrict rar, double *restrict decr)   int  gal2equ (double glon, double glat, double *restrict ra, double *restrict dec)   int  hor_to_itrs (const on_surface *restrict location, double az, double za, double *restrict itrs)   int  itrs_to_hor (const on_surface *restrict location, const double *restrict itrs, double *restrict az, double *restrict za)  
Date
Created on Mar 5, 2025

Various transformations between different coordinate systems

◆ ecl2equ() int ecl2equ ( double  jd_tt, enum novas_equator_type  coord_sys, enum novas_accuracy  accuracy, double  elon, double  elat, double *restrict  ra, double *restrict  dec  )

Convert ecliptic longitude and latitude to right ascension and declination. To convert GCRS ecliptic coordinates (mean ecliptic and equinox of J2000.0), set 'coord_sys' to NOVAS_GCRS_EQUATOR(2); in this case the value of 'jd_tt' can be set to anything, since J2000.0 is assumed. Otherwise, all input coordinates are dynamical at'jd_tt'.

Parameters
jd_tt [day] Terrestrial Time (TT) based Julian date. (Unused if 'coord_sys' is NOVAS_GCRS_EQUATOR[2]) coord_sys The astrometric reference system of the coordinates. If 'coord_sys' is NOVAS_GCRS_EQUATOR(2), the input GCRS coordinates are converted to J2000 ecliptic coordinates. accuracy NOVAS_FULL_ACCURACY (0) or NOVAS_REDUCED_ACCURACY (1) elon [deg] Ecliptic longitude in degrees, referred to specified ecliptic and equinox of date. elat [deg] Ecliptic latitude in degrees, referred to specified ecliptic and equinox of date. [out] ra [h] Right ascension in hours, referred to specified equator and equinox of date. [out] dec [deg] Declination in degrees, referred to specified equator and equinox of date.
Returns
0 if successful, or else 1 if the value of 'coord_sys' is invalid.
See also
ecl2equ_vec()
equ2ecl()
Since
1.0
Author
Attila Kovacs

References ecl2equ_vec().

◆ ecl2equ_vec()

Converts an ecliptic position vector to an equatorial position vector. To convert ecliptic coordinates (mean ecliptic and equinox of J2000.0) to GCRS RA and dec to, set 'coord_sys' to NOVAS_GCRS_EQUATOR(2); in this case the value of 'jd_tt' can be set to anything, since J2000.0 is assumed. Otherwise, all input coordinates are dynamical at 'jd_tt'.

Parameters
jd_tt [day] Terrestrial Time (TT) based Julian date. (Unused if 'coord_sys' is NOVAS_GCRS_EQUATOR[2]) coord_sys The astrometric reference system type of the coordinates accuracy NOVAS_FULL_ACCURACY (0) or NOVAS_REDUCED_ACCURACY (1) in Position vector, referred to specified ecliptic and equinox of date. [out] out Position vector, referred to specified equator and equinox of date. It can be the same vector as the input.
Returns
0 if successful, -1 if either vector argument is NULL or the accuracy is invalid, or else 1 if the value of 'coord_sys' is invalid.
See also
ecl2equ()
equ2ecl_vec()

References e_tilt(), frame_tie(), J2000_TO_ICRS, mean_obliq(), NOVAS_FULL_ACCURACY, NOVAS_GCRS_EQUATOR, NOVAS_MEAN_EQUATOR, NOVAS_REDUCED_ACCURACY, and NOVAS_TRUE_EQUATOR.

◆ equ2ecl() short equ2ecl ( double  jd_tt, enum novas_equator_type  coord_sys, enum novas_accuracy  accuracy, double  ra, double  dec, double *restrict  elon, double *restrict  elat  )

Convert right ascension and declination to ecliptic longitude and latitude. To convert GCRS RA and dec to ecliptic coordinates (mean ecliptic and equinox of J2000.0), set 'coord_sys' to NOVAS_GCRS_EQUATOR(2); in this case the value of 'jd_tt' can be set to anything, since J2000.0 is assumed. Otherwise, all input coordinates are dynamical at 'jd_tt'.

Parameters
jd_tt [day] Terrestrial Time (TT) based Julian date. (Unused if 'coord_sys' is NOVAS_GCRS_EQUATOR[2]) coord_sys The astrometric reference system of the coordinates. If 'coord_sys' is NOVAS_GCRS_EQUATOR(2), the input GCRS coordinates are converted to J2000 ecliptic coordinates. accuracy NOVAS_FULL_ACCURACY (0) or NOVAS_REDUCED_ACCURACY (1) ra [h] Right ascension in hours, referred to specified equator and equinox of date. dec [deg] Declination in degrees, referred to specified equator and equinox of date. [out] elon [deg] Ecliptic longitude in degrees, referred to specified ecliptic and equinox of date. [out] elat [deg] Ecliptic latitude in degrees, referred to specified ecliptic and equinox of date.
Returns
0 if successful, or else 1 if the value of 'coord_sys' is invalid.
See also
equ2ecl_vec()
ecl2equ()

References equ2ecl_vec().

◆ equ2ecl_vec()

Converts an equatorial position vector to an ecliptic position vector. To convert ICRS RA and dec to ecliptic coordinates (mean ecliptic and equinox of J2000.0), set 'coord_sys' to NOVAS_GCRS_EQUATOR(2); in this case the value of 'jd_tt' can be set to anything, since J2000.0 is assumed. Otherwise, all input coordinates are dynamical at 'jd_tt'.

Parameters
jd_tt [day] Terrestrial Time (TT) based Julian date. (Unused if 'coord_sys' is NOVAS_GCRS_EQUATOR[2]) coord_sys The astrometric reference system type of the coordinates. accuracy NOVAS_FULL_ACCURACY (0) or NOVAS_REDUCED_ACCURACY (1) in Position vector, referred to specified equator and equinox of date. [out] out Position vector, referred to specified ecliptic and equinox of date. It can be the same vector as the input. If 'coord_sys' is NOVAS_GCRS_EQUATOR(2), the input GCRS coordinates are converted to J2000 ecliptic coordinates.
Returns
0 if successful, -1 if either vector argument is NULL or the accuracy is invalid, or else 1 if the value of 'coord_sys' is invalid.
See also
equ2ecl()
ecl2equ_vec()

References e_tilt(), frame_tie(), ICRS_TO_J2000, mean_obliq(), NOVAS_FULL_ACCURACY, NOVAS_GCRS_EQUATOR, NOVAS_MEAN_EQUATOR, NOVAS_REDUCED_ACCURACY, and NOVAS_TRUE_EQUATOR.

◆ equ2gal() int equ2gal ( double  ra, double  dec, double *restrict  glon, double *restrict  glat  )

Converts ICRS right ascension and declination to galactic longitude and latitude.

REFERENCES:

  1. Hipparcos and Tycho Catalogues, Vol. 1, Section 1.5.3.
Parameters
ra [h] ICRS right ascension in hours. dec [deg] ICRS declination in degrees. [out] glon [deg] Galactic longitude in degrees. [out] glat [deg] Galactic latitude in degrees.
Returns
0 if successful, or -1 if either of the output pointer arguments are NULL.
See also
gal2equ()
◆ equ2hor() int equ2hor ( double  jd_ut1, double  ut1_to_tt, enum novas_accuracy  accuracy, double  xp, double  yp, const on_surface *restrict  location, double  ra, double  dec, enum novas_refraction_model  ref_option, double *restrict  zd, double *restrict  az, double *restrict  rar, double *restrict  decr  )

Transforms topocentric (TOD) right ascension and declination to zenith distance and azimuth. This method should not be used to convert CIRS apparent coordinates (IAU 2000 standard) – for those you should use cirs_to_itrs() followed by itrs_to_hor() instead.

It uses a method that properly accounts for polar motion, which is significant at the sub-arcsecond level. This function can also adjust coordinates for atmospheric refraction.

Deprecated:
The name of this function does not reveal what type of equatorial coordinates it requires. To make it less ambiguous, you should use tod_to_itrs() followed by itrs_to_hor() instead, possibly following it with refract_astro() if you also want to apply optical refraction.

NOTES:

REFERENCES:

  1. Kaplan, G. (2008). USNO/AA Technical Note of 28 Apr 2008, "Refraction as a Vector."
Parameters
jd_ut1 [day] UT1 based Julian date ut1_to_tt [s] TT - UT1 Time difference in seconds accuracy NOVAS_FULL_ACCURACY (0) or NOVAS_REDUCED_ACCURACY (1) xp [arcsec] Conventionally-defined x coordinate of celestial intermediate pole with respect to ITRS reference pole, in arcseconds. yp [arcsec] Conventionally-defined y coordinate of celestial intermediate pole with respect to ITRS reference pole, in arcseconds. location The observer location ra [h] Topocentric right ascension of object of interest, in hours, referred to true equator and equinox of date. dec [deg] Topocentric declination of object of interest, in degrees, referred to true equator and equinox of date. ref_option NOVAS_STANDARD_ATMOSPHERE (1), or NOVAS_WEATHER_AT_LOCATION (2) if to use the weather [out] zd [deg] Topocentric zenith distance in degrees (unrefracted). [out] az [deg] Topocentric azimuth (measured east from north) in degrees. [out] rar [h] Topocentric right ascension of object of interest, in hours, referred to true equator and equinox of date, affected by refraction if 'ref_option' is non-zero. (It may be NULL if not required) [out] decr [deg] Topocentric declination of object of interest, in degrees, referred to true equator and equinox of date. (It may be NULL if not required)
Returns
0 if successful, or -1 if one of the 'zd' or 'az' output pointers are NULL.
See also
itrs_to_hor()
tod_to_itrs()
NOVAS_TOD

References EROT_GST, NOVAS_DYNAMICAL_CLASS, refract_astro(), and ter2cel().

◆ gal2equ() int gal2equ ( double  glon, double  glat, double *restrict  ra, double *restrict  dec  )

Converts galactic longitude and latitude to ICRS right ascension and declination.

REFERENCES:

  1. Hipparcos and Tycho Catalogues, Vol. 1, Section 1.5.3.
Parameters
glon [deg] Galactic longitude in degrees. glat [deg] Galactic latitude in degrees. [out] ra [h] ICRS right ascension in hours. [out] dec [deg] ICRS declination in degrees.
Returns
0 if successful, or -1 if either of the output pointer arguments are NULL.
See also
equ2gal()
Since
1.0
Author
Attila Kovacs
◆ hor_to_itrs() int hor_to_itrs ( const on_surface *restrict  location, double  az, double  za, double *restrict  itrs  )

Converts astrometric (unrefracted) azimuth and zenith angles at the specified observer location to a unit position vector in the Earth-fixed ITRS frame.

Parameters
location Observer location on Earth az [deg] astrometric azimuth angle at observer location [0:360]. It may be NULL if not required. za [deg] astrometric zenith angle at observer location [0:180]. It may be NULL if not required. [out] itrs Unit 3-vector direction in Earth-fixed ITRS frame
Returns
0 if successful, or else -1 if the location or the input vector is NULL.
See also
itrs_to_hor()
itrs_to_cirs()
itrs_to_tod()
refract()
Since
1.0
Author
Attila Kovacs
◆ itrs_to_hor() int itrs_to_hor ( const on_surface *restrict  location, const double *restrict  itrs, double *restrict  az, double *restrict  za  )

Converts a position vector in the Earth-fixed ITRS frame to astrometric (unrefracted) azimuth and zenith angles at the specified observer location.

Parameters
location Observer location on Earth itrs 3-vector position in Earth-fixed ITRS frame [out] az [deg] astrometric azimuth angle at observer location [0:360]. It may be NULL if not required. [out] za [deg] astrometric zenith angle at observer location [0:180]. It may be NULL if not required.
Returns
0 if successful, or else -1 if the location or the input vector is NULL.
See also
hor_to_itrs()
cirs_to_itrs()
tod_to_itrs()
refract_astro()
Since
1.0
Author
Attila Kovacs

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