*
* tax_day.F
*
*  This software was developed by the Thermal Modeling and Analysis
*  Project(TMAP) of the National Oceanographic and Atmospheric
*  Administration's (NOAA) Pacific Marine Environmental Lab(PMEL),
*  hereafter referred to as NOAA/PMEL/TMAP.
*
*  Access and use of this software shall impose the following
*  obligations and understandings on the user. The user is granted the
*  right, without any fee or cost, to use, copy, modify, alter, enhance
*  and distribute this software, and any derivative works thereof, and
*  its supporting documentation for any purpose whatsoever, provided
*  that this entire notice appears in all copies of the software,
*  derivative works and supporting documentation.  Further, the user
*  agrees to credit NOAA/PMEL/TMAP in any publications that result from
*  the use of this software or in any product that includes this
*  software. The names TMAP, NOAA and/or PMEL, however, may not be used
*  in any advertising or publicity to endorse or promote any products
*  or commercial entity unless specific written permission is obtained
*  from NOAA/PMEL/TMAP. The user also understands that NOAA/PMEL/TMAP
*  is not obligated to provide the user with any support, consulting,
*  training or assistance of any kind with regard to the use, operation
*  and performance of this software nor to provide the user with any
*  updates, revisions, new versions or "bug fixes".
*
*  THIS SOFTWARE IS PROVIDED BY NOAA/PMEL/TMAP "AS IS" AND ANY EXPRESS
*  OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED
*  WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE
*  ARE DISCLAIMED. IN NO EVENT SHALL NOAA/PMEL/TMAP BE LIABLE FOR ANY SPECIAL,
*  INDIRECT OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER
*  RESULTING FROM LOSS OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF
*  CONTRACT, NEGLIGENCE OR OTHER TORTUOUS ACTION, ARISING OUT OF OR IN
*  CONNECTION WITH THE ACCESS, USE OR PERFORMANCE OF THIS SOFTWARE. 
*
*
* Jing Y. Li 
* May 4th 2006
* 27-Feb-2013 ACM  Fix ticket 2043: remove old code for handling single-
*                  precision values coming in from argument 
* v695  *acm 2/15  Time axis may be an F axis or a T axis.

*
* This function returns day specified by the first argument (variable 
* containing time values) from the second argument (variable from which time 
* encoding will be inferred).
*

*
* In this subroutine we provide information about
* the function.  The user configurable information 
* consists of the following:
*
* descr              Text description of the function
*
* num_args           Required number of arguments
*
* axis_inheritance   Type of axis for the result
*                       ( CUSTOM, IMPLIED_BY_ARGS, NORMAL, ABSTRACT )
*                       CUSTOM          - user defined axis
*                       IMPLIED_BY_ARGS - same axis as the incoming argument
*                       NORMAL          - the result is normal to this axis
*                       ABSTRACT        - an axis which only has index values
*
* piecemeal_ok       For memory optimization:
*                       axes where calculation may be performed piecemeal
*                       ( YES, NO )
* 
*
* For each argument we provide the following information:
*
* name               Text name for an argument
*
* unit               Text units for an argument
*
* desc               Text description of an argument
*
* axis_influence     Are this argument''s axes the same as the result grid?
*                       ( YES, NO )
*
* axis_extend       How much does Ferret need to extend arg limits relative to result 
*


      SUBROUTINE tax_day_init(id)

      IMPLICIT NONE
      INCLUDE 'EF_Util.cmn'

      INTEGER id, arg

* **********************************************************************
*                                            USER CONFIGURABLE PORTION |
*                                                                      |
*                                                                      V

      CALL ef_set_desc(id,
     .        'Returns days of month of time axis coordinate values' )
      CALL ef_set_num_args(id, 2)
      CALL ef_set_axis_inheritance_6d(id,
     .                                IMPLIED_BY_ARGS, IMPLIED_BY_ARGS,
     .                                IMPLIED_BY_ARGS, IMPLIED_BY_ARGS,
     .                                IMPLIED_BY_ARGS, IMPLIED_BY_ARGS)
      CALL ef_set_piecemeal_ok_6d(id, NO, NO, NO, NO, NO, NO)

      arg = 1
      CALL ef_set_arg_name(id, arg, 'A')
      CALL ef_set_arg_unit(id, arg, ' ')
      CALL ef_set_arg_desc(id, arg, 'time steps to convert')
      CALL ef_set_axis_influence_6d(id, arg,
     .                              YES, YES, YES, YES, YES, YES)

      arg = 2
      CALL ef_set_arg_name(id, arg, 'B')
      CALL ef_set_arg_unit(id, arg, ' ')
      CALL ef_set_arg_desc(id, arg, 'variable with reference time axis')
      CALL ef_set_axis_influence_6d(id, arg,
     .                              NO, NO, NO, NO, NO, NO)

*                                                                      ^
*                                                                      |
*                                            USER CONFIGURABLE PORTION |
* **********************************************************************

      RETURN 
      END

*
* In this subroutine we compute the result
*
      SUBROUTINE tax_day_compute(id, arg_1, arg_2, result)

      IMPLICIT NONE
      INCLUDE 'EF_Util.cmn'
      INCLUDE 'EF_mem_subsc.cmn'

      INTEGER id

      REAL arg_1(mem1lox:mem1hix, mem1loy:mem1hiy, mem1loz:mem1hiz, 
     .           mem1lot:mem1hit, mem1loe:mem1hie, mem1lof:mem1hif)
      REAL arg_2(mem2lox:mem2hix, mem2loy:mem2hiy, mem2loz:mem2hiz, 
     .           mem2lot:mem2hit, mem2loe:mem2hie, mem2lof:mem2hif)

      REAL result(memreslox:memreshix, memresloy:memreshiy, 
     .            memresloz:memreshiz, memreslot:memreshit,
     .            memresloe:memreshie, memreslof:memreshif)

* After initialization, the 'res_' arrays contain indexing information 
* for the result axes.  The 'arg_' arrays will contain the indexing 
* information for each variable''s axes. 

      INTEGER res_lo_ss(6),
     .        res_hi_ss(6),
     .        res_incr (6)
      INTEGER arg_lo_ss(6,EF_MAX_ARGS),
     .        arg_hi_ss(6,EF_MAX_ARGS),
     .        arg_incr (6,EF_MAX_ARGS)

      REAL bad_flag(EF_MAX_ARGS), bad_flag_result

* **********************************************************************
*                                            USER CONFIGURABLE PORTION |
*                                                                      |
*                                                                      V

      CHARACTER*20 datebuf
      INTEGER iyear, day_of_mon
      CHARACTER*3 cmon
      INTEGER L2, LL, dir
      CHARACTER*255 err_msg
      REAL*8 ddate
      INTEGER i,j,k,l, m, n
      INTEGER i1, j1, k1, l1, m1, n1

*  variables for checking axis characteristics (modulo axes)
      CHARACTER ax_name(6)*16, ax_units(6)*16
      LOGICAL backward(6), modulo(6), regular(6), tmodulo


      CALL ef_get_res_subscripts_6d(id, res_lo_ss, res_hi_ss, res_incr)
      CALL ef_get_arg_subscripts_6d(id, arg_lo_ss, arg_hi_ss, arg_incr)
      CALL ef_get_bad_flags(id, bad_flag, bad_flag_result)

*  Check to see if time axis of arg 2 is modulo
      CALL ef_get_axis_info_6d(id, ARG2, ax_name, ax_units,
     .                         backward, modulo, regular)
      
* Get the direction of arg 2
      IF (arg_lo_ss(T_AXIS, ARG2) .NE. ef_unspecified_int4) THEN
         dir = T_AXIS
         tmodulo = modulo(T_AXIS)
      ENDIF
      IF (arg_lo_ss(F_AXIS, ARG2) .NE. ef_unspecified_int4) THEN
         dir = F_AXIS
         tmodulo = modulo(F_AXIS)
      ENDIF

      n1 = arg_lo_ss(F_AXIS,ARG1)
      DO 600 n = res_lo_ss(F_AXIS), res_hi_ss(F_AXIS)

      m1 = arg_lo_ss(E_AXIS,ARG1)
      DO 500 m = res_lo_ss(E_AXIS), res_hi_ss(E_AXIS)

      l1 = arg_lo_ss(T_AXIS,ARG1)
      DO 400 l = res_lo_ss(T_AXIS), res_hi_ss(T_AXIS)

      k1 = arg_lo_ss(Z_AXIS,ARG1)
      DO 300 k = res_lo_ss(Z_AXIS), res_hi_ss(Z_AXIS)

      j1 = arg_lo_ss(Y_AXIS,ARG1)
      DO 200 j = res_lo_ss(Y_AXIS), res_hi_ss(Y_AXIS)

      i1 = arg_lo_ss(X_AXIS,ARG1)
      DO 100 i = res_lo_ss(X_AXIS), res_hi_ss(X_AXIS)

         ddate = arg_1(i1,j1,k1,l1,m1,n1)

         IF ( ddate .NE. bad_flag(ARG1) ) THEN

*     Get the date string corresponding to time ddate for the variable ARG2
            CALL EF_GET_AXIS_DATES(id, ARG2, ddate, dir, 1, datebuf)

            IF ( .NOT. tmodulo ) THEN
*               datebuf is in form "DD-MON-YEAR HH:MM:SS". Read day.
               READ (datebuf,120,err=900) day_of_mon, cmon, iyear
  120                   FORMAT (i2, 1x, a3, 1x, i4) 
            ELSE
*               modulo: datebuf is in form "DD-MON HH:MM:SS". Read day.
               READ (datebuf,130,err=900) day_of_mon, cmon
  130          FORMAT (i2, 1x, a3) 
            ENDIF
            result(i,j,k,l,m,n) = day_of_mon 

         ELSE

            result(i,j,k,l,m,n) = bad_flag_result

         ENDIF

         i1 = i1 + arg_incr(X_AXIS,ARG1)
 100  CONTINUE

         j1 = j1 + arg_incr(Y_AXIS,ARG1)
 200  CONTINUE

         k1 = k1 + arg_incr(Z_AXIS,ARG1)
 300  CONTINUE

         l1 = l1 + arg_incr(T_AXIS,ARG1)
 400  CONTINUE

         m1 = m1 + arg_incr(E_AXIS,ARG1)
 500  CONTINUE

         n1 = n1 + arg_incr(F_AXIS,ARG1)
 600  CONTINUE

      RETURN

 900  WRITE (err_msg,*) 
     .  'Error assigning dates/times to timestamp for tax_day ',
     .  datebuf
 999  CALL ef_bail_out (id, err_msg)

*                                                                      ^
*                                                                      |
*                                            USER CONFIGURABLE PORTION |
* **********************************************************************

      RETURN
      END
