NERS User Guide

Introduction

NERS library interface provides 8 public routines. Routine ners_init is called before any other NERS functions. It specifies NERS control file and the time range of intended EOP use. Time in NERS library is the interval elapsed since 2000.01.01_00:00:00.0 in TAI time scale. Units of time are seconds. Instead of time, events are often get tags of UTC function. In order to convert UTC tag to TAI time, NERS provides function ners_get_utcmtai that returns function UTC minus TAI on the specified timetag UTC. Routine ners_init initializes internal data structure of NERS object that is defined in ners.i or ners.hinclude block. This object is then passed to any other NERS function. NERS provides either the vector Earth orientation parameters on the specified moment of time or the table of the Earth orientation series for the specified range of time and the specified time step. At the end, function ners_quit releases memory acquired by ners_init.

The Earth orientation can be described either as a 3×3 rotation matrix that transforms a Cartesian vector from the rotating terrestrial coordinate system to the inertial non-rotating celestial coordinate system or as parameters on which this matrix depends. For practical needs the rotation matrix and its time derivatives are sufficient to perform astronomical reduction for Earth's rotation. However, NERS also provides the parameters that describes the Earth's rotation on which the rotation matrix depends as well. These parameters are empirical corrections to a deterministic model. Since the Earth's rotation depends on motion of the hydrosphere and atmosphere, it cannot be described with a deterministic model with the accuracy comparable with accuracy of observations and should be continuously monitored using space geodesy observations. For historical reasons several alternative Earth orientation parameters were used. For instance. For instance the rate of change of the angular variable along the axis 3, i.e. the axial motion can be described as Euler angle 3, UT1 rate, or the length of day. NERS provides many alternative Earth orientation parameters. These parameters are not independent.

Use cases

Transform a Carthesian vector of station coordinates in the terrestrial coordinate system to the inertial celestial coordinate system at the specified moment of time. All you need is to call three NERS routines: ners_init, ners_get_eop, ners_quit. First, you run ners_init and specify the time range. If you need to compute the rotation matrix only for one epoch, the range may be just ± 10 seconds. If you are going to compute the transformation matrix for a number of epochs, just specify TAI time of the earliest and the lastest epoch. The artgument time is 64-bit float number of seconds elapsed since 2000.01.01_00:00:00.0 TAI. Second, you run ners_get_eop and specify the time. The type of the EOP is "mat". A product of this mastrix with the Carthesian vector of station coordinates in the terrestrial coordinate system will transform it to the inertial celestial coordinate system. If you need the transfromation matrix for a number of epochs, you call ners_get_eop in a cycle. Finally, you call ners_quit to release dynamic memory allocated by NERS.
See example/ners_fortran_example_01.f and example/ners_c_example_01.c.

Get TAI time for a given UTC timetag. It is rather common to have value of of the non-differntiable function of time UTC(t) for events instead of time TAI. In order to process such data you need to convert UTC timetag to TAI moment of time. All you need is to call three NERS routines: ners_init, ners_get_utcmtai, ners_quit. First, you run ners_init and specify the time range. If you are going to compute convert UTC to TAI for a number of epochs, just specify TAI time of the earliest and the lastest epoch. Second, you run ners_get_utcmtai and specify the UTC timetag elapsed since epoch 2000.01.01_00:00:00.0 UTC. The routine returns function UTC minus TAI. Substracting this function from UTC you tet TAI time: TAI = UTC - UTC_M_TAI. If you need transfrom UTC time tag to TAI for a number of epochs, you call ners_get_utcmtai in a cycle. Finally, you call ners_quit to release dynamic memory allocated by NERS.
See example/ners_fortran_example_02.f and example/ners_c_example_02.c.

Get the last time epoch of the short-term EOP forecast. You need call three NERS routines: ners_init, ners_inq, ners_quit. First, you run ners_init and specify the time range. For this case the range may be just ± 10 seconds of the current moment. Second, you run ners_inq wioth request parameter "range". The routine returns three parameters: start time for EOP assimilaiton, stop time of the short-term EOP forecast, and stop time of the long-term prediction. Time is in seconds elapsed since 2000.01.01_00:00:00.0 TAI. Finally, you call ners_quit to release dynamic memory allocated by NERS.
See example/ners_fortran_example_04.f and example/ners_c_example_04.c.

Description of NERS public functions

ners_init — initializes internal NERS data structure, parses the configuration file and reads the leap second file. It also specifues the interval of time for the Earth orientation parameters that will be computed at the next call to NERS. This interval should not exceed 10 days.

  FORTRAN:  NERS_INIT ( CONFIG_FILE, NERS, TIME_TAI_START, TIME_TAI_STOP, IUER )
  C:       cners_init ( char * config_file, struct ners_struct * ners, 
                        double time_tai_beg, double time_tai_end, int * iuer )


    Input parameters:

    config_file    ( CHARACTER*(*) ) -- name of the NERS configuration file
                                        NERS__CONFIG defined in ners_local.i
                                        specifies the default configuration file
    ners           ( NERS__TYPE    ) -- NERS internal data structure 
    time_tai_start ( REAL*8        ) -- Start time of the time range 
                                        Units: seconds since 2000.01.01_00:00:00.0 TAI
					Value -1.0D0 means the current moment.
    time_tai_stop  ( REAL*8        ) -- Stop  time of the time range. 
                                        Units: seconds since 2000.01.01_00:00:00.0 TAI
					Value -1.0D0 means the current moment.

    Input/Output parameter:

    iuer           ( INTEGER*4     ) -- Error parameter. 
                                        On input:  -1 -- to print the error message if
                                                         an error is detected;
                                                   otherwise, not to print the message:
                                        On output:  0 -- normal completion
                                                   >0 -- error code during NERS 
                                                         initialization

ners_get_eop — returns array of the Earth Orientation Parameters on the specified moment of time. The type of Earth orientation parameter is defined in variable cpar. If it is called the first time, it communicates with the server, downloads the NERS message and prepares the interpolating polynomials for the specified time range, computes intermediate angles and expand them into B-spline basis over the specified time period. Then it computes the requested Earth orientation parameters. When it is called the next time, it reuses the B-spline coefficients computed previously, unless more than 20 minutes elapsed from the computation of the coefficients.

FORTRAN: NERS_GET_EOP ( NERS, TIME_TAI, CPAR, M_PAR, L_PAR, PARS, IUER )
C: cners_get_eop ( struct ners_struct * ners, double time_tai_obs, char * cpar,
int mpar, int * lpar, double eops[], int * iuer )

Input parameters:

ners ( NERS__TYPE ) -- NERS internal data structure
time_tai ( REAL*8 ) -- Time. Units: seconds since 2000.01.01_00:00:00.0 TAI
cpar ( CHARACTER*(*) ) -- Earth orientation parameter name:

mat -- 3x3 matrix of the transformation from the terrestrial
coordinate system to the celestial coordinate system
matr -- First time derivative of the 3x3 matrix of the
transformation from the terrestrial coordinate system
to the celestial coordinate system
matrr -- Second time derivative of the 3x3 matrix of the
transformation from the terrestrial coordinate system
to the celestial coordinate system
matall -- 3x3x3 array of the matrix of the transformation from
the terrestrial coordinate system to the celestial
coordinate system, its first and second time derivative.
[1:3,1:3,1] -- transformation matrix from the terrestrial
coordinate system to the celestial
coordinate system,
[1:3,1:3,2] -- first time derivative of the transformation
matrix above.
[1:3,1:3,3] -- second time derivative of the transformation
matrix above.

utcmtai -- Value of function UTC minus TAI. Units: s.

e1 -- Euler angle around axis one. Units: rad.
e2 -- Euler angle around axis two. Units: rad.
e3 -- Euler angle around axis three. Units: rad.
e1r -- First time derivative of Euler angle around axis one. Units: rad/s.
e2r -- First time derivative of Euler angle around axis two. Units: rad/s.
e3r -- First time derivative of Euler angle around axis three. Units: rad/s.
e1rr -- Second time derivative of Euler angle around axis one. Units: rad/s.
e2rr -- Second time derivative of Euler angle around axis two. Units: rad/s.
e3rr -- Second time derivative of Euler angle around axis three. Units: rad/s.

ut1mtai -- Angle UT1 minus TAI. Units: s.
ut1rat -- First time derivative of angle UT1 minus TAI. Units s/s.
ut1rr -- Second time derivative of angle UT1 minus TAI. Units s/s^2.
lod -- Length of day. Units: s.
lodr -- Rate of change of the length of day. Units: s/day.
xpol -- X pole coordinate. Unit: arcsec.
ypol -- Y pole coordinate. Unit: arcsec.
xpolr -- First time derivative of X pole coordinate. Unit: arcsec/day.
ypolr -- First time derivative of Y pole coordinate. Unit: arcsec/day.
xpolrr -- Second time derivative of X pole coordinate. Unit: arcsec/day**2.
ypolrr -- Second time derivative of Y pole coordinate. Unit: arcsec/day**2.
eop3 -- Array of three EOP parameters:
1: X pole coordinate. Unit: arcsec.
2: Y pole coordinate. Unit: arcsec.
3: UT1 minus TAI. Unit: s.
eop3r -- Array of six EOP parameters:
1: X pole coordinate. Unit: arcsec.
2: Y pole coordinate. Unit: arcsec.
3: UT1 minus TAI. Unit: s.
4: First time derivative of X pole coordinate. Unit: arcsec/day.
5: Second time derivative of Y pole coordinate. Unit: arcsec/day.
6: First time derivative of UT1 minus TAI coordinate. Unit: s/day.

dpsi -- Nutation angle in longitude. Units: rad
deps -- Nutation angle in obliquity. Units: rad
dpsir -- First time derivative of nutation angle in longitude. Units: rad/s.
depsr -- First time derivative of nutation angle in obliquity. Units: rad/s.
nut -- Array of two EOP parameters:
1: Nutation angle in longitude. Units: rad
2: Nutation angle in obliquity. Units: rad
nutr -- Array of four EOP parameters:
1: Nutation angle in longitude. Units: rad
2: Nutation angle in obliquity. Units: rad
3: First time derivative of nutation angle in longitude. Units: rad/s.
4: First time derivative of nutation angle in obliquity. Units: rad/s.
eops -- Array of eight EOP parameters:
1: X pole coordinate. Unit: arcsec.
2: Y pole coordinate. Unit: arcsec.
3: UT1 minus TAI. Unit: s.
4: First time derivative of X pole coordinate. Unit: arcsec/day.
5: Second time derivative of Y pole coordinate. Unit: arcsec/day.
6: First time derivative of UT1 minus TAI coordinate. Unit: s/day.
7: Nutation angle in longitude. Units: arcsec
8: Nutation angle in obliquity. Units: arcsec

h1 -- Contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad.
h2 -- Contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad.
h3 -- Contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad.
h1r -- First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad/s.
h2r -- First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad/s.
h3r -- First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad/s.
h1rr -- Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad/s^2.
h2rr -- Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad/s^2.
h3rr -- Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad/s^2.
heo -- Array of three components of the contribution of empirical harmonic variations in the EOPs:
1: Contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad.
2: Contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad.
3: Contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad.
heor -- Array of three components of the first time derivative of the contribution of empirical harmonic variations in the EOPs:
1: First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad/s.
2: First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad/s.
3: First time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad/s.
heorr -- Array of three components of the first time derivative of the contribution of empirical harmonic variations in the EOPs:
1: Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad/s^2.
2: Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad/s^2.
3: Second time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad/s^2.

m_par ( INTEGER*4 ) -- Maximum number of the elements in the output array.

Output parameters:

l_par ( INTEGER*4 ) -- Actual number of the EOPs
pars ( REAL*8 ) -- Array of EOPs. Dimension: m_par.

Input/Output parameter:

iuer ( INTEGER*4 ) -- Error parameter.
On input: -1 -- to print the error message if
an error is detected;
otherwise, not to print the message:
On output: 0 -- normal completion
>0 -- error code during NERS
initialization

ners_quit — releases memory for internal data structures and un-initialize them.

  FORTRAN:  NERS_QUIT ( CODE, NERS )
  C:       cners_quit ( int * quit_code, struct ners_struct * ners )

    Input parameter:

    code ( INTEGER*4  ) -- Level of re-initialization:
                           NERS__EXP -- release memory with coefficients of EOP expansion for
                                        the interval of time specified in previous call of
                                        routine ners_init.
                           NERS__FCS -- release memory with the NERS forecast message
                           NERS__ALL -- release memory for all internal data structures

    Input/Output parameter:

    ners      ( NERS__TYPE    ) -- NERS internal data structure

ners_inq — inquirers either the time interval of EOP availability or the time of the EOP forecast generation.

    FORTRAN:  NERS_INQ  ( NERS, REQ, M_PAR, L_PAR, PARS, IUER )
    C:       cners_quit ( int * quit_code, struct ners_struct * ners )

    Input parameter:

    ners   ( NERS__TYPE    ) -- NERS internal data structure 
    req    ( CHARACTER*(*) ) -- request type. Supported requests:

                  range        -- request of the EOP range. Returns three values:
                                  1: start time of EOP availability. Units: seconds since
                                     2000.01.01_00:00:00.0 TAI.
                                  2: stop  time of the EOP or the EOP forecast availability. 
                                     Units: seconds since 2000.01.01_00:00:00.0 TAI.
                                  3: stop  time of the long-term EOP prediction
                  fcs_gen_time -- request of the EOP forecast message generation time.
                                  Return one value:
                                  1: time of the EOP forecast generation. Units: seconds since
                                     2000.01.01_00:00:00.0 TAI.

    m_par  ( INTEGER*4     ) -- Maximum number of the elements in the output array.

    Output parameters:

    l_par     ( INTEGER*4     ) -- Actual number of the EOPs
    pars      ( REAL*8        ) -- Array of EOPs. Dimension: m_par.

    Input/Output parameter:

    iuer           ( INTEGER*4     ) -- Error parameter. 
                                        On input:  -1 -- to print the error message if
                                                         an error is detected;
                                                   otherwise, not to print the message:
                                        On output:  0 -- normal completion
                                                   >0 -- error code during NERS

ners_get_series — returns a 2D array of the Earth Orientation Parameters time series for the specified time range with the specified time step. The type of Earth orientation parameter(s) is defined in variable cpar.

    FORTRAN:  NERS_GET_SERIES ( NERS, TIME_TAI_START, TIME_TAI_STOP, TIME_STEP, CPAR, 
                                DIM1, DIM2, NS, TIM, SER, IUER )
    C:       cners_get_series  ( struct ners_struct * ners, double time_tai_beg, double time_tai_end, 
                         double tim_step, char * cpar, int m_par, int m_ser, int * ns, 
                         double tim[], double ser[], int * iuer )

    Input parameters:

    ners           ( NERS__TYPE    ) -- NERS internal data structure 
    time_tai_start ( REAL*8        ) -- Start time of EOP series. Units: seconds since 2000.01.01_00:00:00.0 TAI
    time_tai_stop  ( REAL*8        ) -- Stop  time of EOP series. Units: seconds since 2000.01.01_00:00:00.0 TAI
    time_step      ( REAL*8        ) -- Time step of the EOP series. Units: seconds since 2000.01.01_00:00:00.0 TAI
    cpar           ( CHARACTER*(*) ) -- Earth orientation parameter name.

                euler   --  Euler angles of the Earth rotation
                            1: Euler  angle around axis one.   Units: rad.
                            2: Euler  angle around axis two.   Units: rad.
                            3: Euler  angle around axis three. Units: rad.

                euler_r --  First time derivative of Euler angles of the Earth rotation 
                            1: First  time derivative of Euler angle around axis one.   Units: rad/s.
                            2: First  time derivative of Euler angle around axis two.   Units: rad/s.
                            3: First  time derivative of Euler angle around axis three. Units: rad/s.

                polu    --  Array of three EOP parameters:
                            1: X pole coordinate. Unit: arcsec.
                            2: Y pole coordinate. Unit: arcsec.
                            3: UT1 minus TAI.     Unit: s.
                polur   --  Array of six EOP parameters:
                            1: X pole coordinate. Unit: arcsec.
                            2: Y pole coordinate. Unit: arcsec.
                            3: UT1 minus TAI.     Unit: s.
                            4: First  time derivative of X pole coordinate. Unit: arcsec/day.
                            5: Second time derivative of Y pole coordinate. Unit: arcsec/day.
                            6: First  time derivative of UT1 minus TAI coordinate. Unit: s/day.

                eops    --  Array of eight EOP parameters:
                            1: X pole coordinate. Unit: arcsec.
                            2: Y pole coordinate. Unit: arcsec.
                            3: UT1 minus TAI.     Unit: s.
                            4: First  time derivative of X pole coordinate. Unit: arcsec/day.
                            5: Second time derivative of Y pole coordinate. Unit: arcsec/day.
                            6: First  time derivative of UT1 minus TAI coordinate. Unit: s/day.
                            7: Nutation angle in longitude. Units: arcsec
                            8: Nutation angle in obliquity. Units: arcsec

                heo     --  Array of three components of the contribution of empirical harmonic variations in the EOPs:
                            1: Contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad.
                            2: Contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad.
                            3: Contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad.
                heor    --  Array of three components of the first time derivative of the contribution of empirical harmonic variations in the EOPs:
                            1: First  time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 1. Units: rad/s.
                            2: First  time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 2. Units: rad/s.
                            3: First  time derivative of the contribution of empirical harmonic variations in the EOPs with respect to axis 3. Units: rad/s.

    dim1           ( INTEGER*4     ) -- First  dimension of the EOP series array. The dimension runs over time.
    dim2           ( INTEGER*4     ) -- Second dimension of the EOP series array. The dimension runs over parameters.

    Output parameters:

    ns             ( INTEGER*4     ) -- the number of returned EOP values
    tim            ( REAL*8        ) -- Array of EOP time epochs. Dimension: ns. Units: seconds since 2000.01.01_00:00:00.0 TAI
    ser            ( REAL*8        ) -- Two dimensional Array of EOPs. Dimensions: dim1,dim2. The number of 
                                        filled elements along the first  dimension is ns. The number of
                                        filled elements along the second dimension depends on value of 
                                        parameter cpar.

    Input/Output parameter:

    iuer           ( INTEGER*4     ) -- Error parameter. 
                                        On input:  -1 -- to print the error message if
                                                         an error is detected;
                                                   otherwise, not to print the message:
                                        On output:  0 -- normal completion
                                                   >0 -- error code during NERS

ners_get_utcmtai — returns value of UTC minus TAI on the specified UTC time tag.

    FORTRAN:  NERS_GET_UTCMTAI ( NERS, UTC, UTC_M_TAI, IUER ) 
    C:       cners_get_utcmtai ( struct ners_struct * ners, double * utc_obs, 
                                 double * utc, int * iuer )

    Input parameters:

    ners      ( NERS__TYPE    ) -- NERS internal data structure 
    utc       ( REAL*8        ) -- UTC time tag. Units: seconds elapsed since 2000.01.01_00:00:00.0 UTC.

    Output:

    utc_m_tai ( REAL*8  ) -- UTC minus TAI function. Units: seconds.

    Input/Output parameter:

    iuer      ( INTEGER*4     ) -- Error parameter. 
                                   On input:  -1 -- to print the error message if
                                                    an error is detected;
                                               otherwise, not to print the message:
                                   On output:  0 -- normal completion
                                              >0 -- error code during NERS

ners_azelha_comp — Computes azimuth, elevation, hour angle, and their time derivatives at moment of time TIM_TAI for station with coordinates in the terrestrial coordinate system COO_TRS that observes a source with coordinates in the barycentric celestial coordinate system , right ascension and declination RA, DEC.

    FORTRAN:  NERS_AZELHA_COMP ( NERS, TIM_TAI, COO_TRS, RA, DEC,
                                 REFR_MODE, AZ, EL, HA,
                                 AZ_RATE, EL_RATE, HA_RATE, IUER ) 

    C:       cners_azelha_comp ( struct ners_struct * ners, double time_tai_beg, double coo_trs[],
                                 double ra, double dec, char * refr, double * az, double * el, 
                                 double * ha, double * az_rate, double * el_rate, double * ha_rate, 
                                 int * iuer ) ;


    Input parameters:

    TIM_TAI   ( REAL*8    ) -- Time for which the Earth orientation
                               parameter(s) is to be computed elapsed
                               since 2000.01.01_00:00:00.0 TAI. Unit:
                               sec. If TIM_TAI .LE. -1.0D14, then the
                               azimuth and elevation at the current
                               moment of time will be computed.
    COO_TRS   ( REAL*8    ) -- Vector of station coordinates in the
                               rotating crust-fixed coordinate system.
                               Units: m.
    RA        ( REAL*8    ) -- Source right ascension in the inertial
                               barycenter coordinate system. Units: rad.
    DEC       ( REAL*8    ) -- Source declination in the inertial
                               barycenter coordinate system. Units: rad.
    REFR_MODE ( CHARACTER ) -- Refraction mode. Supported values:
                               none  -- refractivity is not accounted.
                               optic -- formula Bennett for optic range
                                        is used ( Bennett, G.G. (1982).
                                        "The Calculation of Astronomical
                                        Refraction in Marine Navigation".
                                        Journal of Navigation, 35(2),
                                        255-259.
                               radio -- 3.13D-4/tg(el) expression
                                        suitable for radio waves is used.
                               both formulae have a floor of 3 deg, i.e.
                               refraction at elevations below 3 deg is
                               considered to be equal to refraction at
                               3 deg.

    Output parameters:

    AZ        ( REAL*8    ) -- Azimuth in rad.
    EL        ( REAL*8    ) -- Elevation in rad.
    HA        ( REAL*8    ) -- Hour angle in rad.
    AZ_RATE   ( REAL*8    ) -- Time derivative of azimuth   in rad/s.
    EL_RATE   ( REAL*8    ) -- Time derivative of elevation in rad/s.
    HA_RATE   ( REAL*8    ) -- Time derivative of hour angle in rad/s.

    Input/Output parameter:

    NERS     ( NERS__TYPE ) -- The data structure that keeps internal
                               parameters related to the Network Earth
                               Rotation Service.

    IUER      ( INTEGER*4     ) -- Error parameter. 
                                   On input:  -1 -- to print the error message if
                                                    an error is detected;
                                               otherwise, not to print the message:
                                   On output:  0 -- normal completion
                                              >0 -- error code during NERS

ners_radec_comp — Computes right ascension, declination and their time derivatives in the barycentric coordinate system at moment of time TIM_TAI for station with coordinates in the terrestrial coordinate system COO_TRS that observes a source with given azimuth and elevation.

    FORTRAN:  NERS_RADEC_COMP ( NERS, TIM_TAI, COO_TRS, AZ, EL, REFR_MODE,
                                RA, DEC, RA_RATE, DEC_RATE, IUER )

    C:        cners_radec_comp  ( struct ners_struct * ners, double tim_tai, 
                                  double coo_trs[], double az, double el,
                                  char * refr_mode, double * ra, double * dec, 
                                  double * ra_rate, double * dec_rate, int * iuer )

    Input parameters:

    TIM_TAI   ( REAL*8    ) -- Time for which the Earth orientation
                               parameter(s) is to be computed elapsed
                               since 2000.01.01_00:00:00.0 TAI. Unit:
                               sec. If TIM_TAI .LE. -1.0D14, then the
                               right ascension and declination at the
                               current moment of time will be computed.
    COO_TRS   ( REAL*8    ) -- Vector of station coordinates in the
                               rotating crust-fixed coordinate system.
                               Units: m.
    AZ        ( REAL*8    ) -- Azimuth in rad.
    EL        ( REAL*8    ) -- Elevation in rad.
    REFR_MODE ( CHARACTER ) -- Refraction mode. Supported values:
                               none  -- refractivity is not accounted.
                               optic -- formula Bennett for optic range
                                        is used ( Bennett, G.G. (1982).
                                        "The Calculation of Astronomical
                                        Refraction in Marine Navigation".
                                        Journal of Navigation, 35(2),
                                        255-259.
                               radio -- 3.13D-4/tg(el) expression
                                        suitable for radio waves is used.
                               both formulae have a floor of 3 deg, i.e.
                               refraction at elevations below 3 deg is
                               considered to be equal to refraction at
                               3 deg.
   
    Output parameters:
   
    RA        ( REAL*8    ) -- Source right ascension in the inertial
                               barycentric coordinate system. Units: rad.
    DEC       ( REAL*8    ) -- Source declination in the inertial
                               barycentric coordinate system. Units: rad.
    RA_RATE   ( REAL*8    ) -- Rate of change of right ascension in the
                               inertial barycentric coordinate system.
                               Units: rad/s.
    DEC_RATE  ( REAL*8    ) -- Rate of change of declination in the
                               inertial barycentric coordinate system.
                               Units: rad/s.
   
    Input/Output parameter:
   
       NERS ( NERS__TYPE ) -- The data structure that keeps internal
                              parameters related to the Network Earth
                              Rotation Service.
       IUER ( INTEGER*4, OPT ) -- Universal error handler.
                              Input: switch IUER=0 -- no error messages
                                     will be generated even in the case
                                     of error. IUER=-1 -- in the case of
                                     error the message will be put on
                                     stdout.
                              Output: 0 in the case of successful
                                      completion and non-zero in the
                                      case of error.

This web page was prepared by Leonid Petrov ()
Last update: 2025.07.22_18:45:23