SUBROUTINE GDSWIZCB(KGDS,IOPT,NPTS,FILL,XPTS,YPTS,RLON,RLAT,NRET,
     &                    LROT,CROT,SROT)
C$$$  SUBPROGRAM DOCUMENTATION BLOCK
C
C SUBPROGRAM:  GDSWIZCB   GDS WIZARD FOR ROTATED EQUIDISTANT CYLINDRICAL
C   PRGMMR: IREDELL       ORG: W/NMC23       DATE: 96-04-10
C
C ABSTRACT: THIS SUBPROGRAM DECODES THE GRIB GRID DESCRIPTION SECTION
C           (PASSED IN INTEGER FORM AS DECODED BY SUBPROGRAM W3FI63)
C           AND RETURNS ONE OF THE FOLLOWING:
C             (IOPT=+1) EARTH COORDINATES OF SELECTED GRID COORDINATES
C             (IOPT=-1) GRID COORDINATES OF SELECTED EARTH COORDINATES
C           FOR STAGGERED ROTATED EQUIDISTANT CYLINDRICAL PROJECTIONS.
C           (SEE UNDER THE DESCRIPTION OF KGDS TO DETERMINE WHETHER
C           TO COMPUTE A STAGGERED WIND GRID OR A STAGGERED MASS GRID.)
C           IF THE SELECTED COORDINATES ARE MORE THAN ONE GRIDPOINT
C           BEYOND THE THE EDGES OF THE GRID DOMAIN, THEN THE RELEVANT
C           OUTPUT ELEMENTS ARE SET TO FILL VALUES.
C           THE ACTUAL NUMBER OF VALID POINTS COMPUTED IS RETURNED TOO.
C
C PROGRAM HISTORY LOG:
C   96-04-10  IREDELL
C   98-08-19  BALDWIN    MODIFY GDSWIZC9 FOR TYPE 203 ETA GRIDS
C 2003-06-11  IREDELL    INCREASE PRECISION
C
C USAGE:    CALL GDSWIZCB(KGDS,IOPT,NPTS,FILL,XPTS,YPTS,RLON,RLAT,NRET,
C     &                   LROT,CROT,SROT)
C
C   INPUT ARGUMENT LIST:
C     KGDS     - INTEGER (200) GDS PARAMETERS AS DECODED BY W3FI63
C                IMPORTANT NOTE: IF THE 9TH BIT (FROM RIGHT) OF KGDS(11)
C                                (SCANNING MODE FLAG) IS 1, THEN THIS
C                                THE GRID IS COMPUTED FOR A WIND FIELD;
C                                OTHERWISE IT IS FOR A MASS FIELD.  THUS
C                                MOD(KGDS(11)/256,2)=0 FOR MASS GRID.
C     IOPT     - INTEGER OPTION FLAG
C                (+1 TO COMPUTE EARTH COORDS OF SELECTED GRID COORDS)
C                (-1 TO COMPUTE GRID COORDS OF SELECTED EARTH COORDS)
C     NPTS     - INTEGER MAXIMUM NUMBER OF COORDINATES
C     FILL     - REAL FILL VALUE TO SET INVALID OUTPUT DATA
C                (MUST BE IMPOSSIBLE VALUE; SUGGESTED VALUE: -9999.)
C     XPTS     - REAL (NPTS) GRID X POINT COORDINATES IF IOPT>0
C     YPTS     - REAL (NPTS) GRID Y POINT COORDINATES IF IOPT>0
C     RLON     - REAL (NPTS) EARTH LONGITUDES IN DEGREES E IF IOPT<0
C                (ACCEPTABLE RANGE: -360. TO 360.)
C     RLAT     - REAL (NPTS) EARTH LATITUDES IN DEGREES N IF IOPT<0
C                (ACCEPTABLE RANGE: -90. TO 90.)
C     LROT     - INTEGER FLAG TO RETURN VECTOR ROTATIONS IF 1
C
C   OUTPUT ARGUMENT LIST:
C     XPTS     - REAL (NPTS) GRID X POINT COORDINATES IF IOPT<0
C     YPTS     - REAL (NPTS) GRID Y POINT COORDINATES IF IOPT<0
C     RLON     - REAL (NPTS) EARTH LONGITUDES IN DEGREES E IF IOPT>0
C     RLAT     - REAL (NPTS) EARTH LATITUDES IN DEGREES N IF IOPT>0
C     NRET     - INTEGER NUMBER OF VALID POINTS COMPUTED
C     CROT     - REAL (NPTS) CLOCKWISE VECTOR ROTATION COSINES IF LROT=1
C     SROT     - REAL (NPTS) CLOCKWISE VECTOR ROTATION SINES IF LROT=1
C                (UGRID=CROT*UEARTH-SROT*VEARTH;
C                 VGRID=SROT*UEARTH+CROT*VEARTH)
C
C ATTRIBUTES:
C   LANGUAGE: FORTRAN 77
C
C$$$
      INTEGER KGDS(200)
      REAL XPTS(NPTS),YPTS(NPTS),RLON(NPTS),RLAT(NPTS)
      REAL CROT(NPTS),SROT(NPTS)
      INTEGER,PARAMETER:: KD=SELECTED_REAL_KIND(15,45)
      REAL(KIND=KD):: RERTH,PI,DPR
      REAL(KIND=KD):: RLAT1,RLON1,RLAT0,RLON0
      REAL(KIND=KD):: SLAT1,CLAT1,SLAT0,CLAT0
      REAL(KIND=KD):: CLON1,SLATR,CLATR,CLONR
      REAL(KIND=KD):: RLATR,RLONR,DLATS,DLONS,XPTFC,YPTFC,SLON
      REAL(KIND=KD):: SLAT,CLAT,CLON,RLATCR,RLONCR,DMIDS,RLATLR,RLONLR
      PARAMETER(RERTH=6.3712E6_KD)
      PARAMETER(PI=3.14159265358979_KD,DPR=180._KD/PI)
C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
      IF(KGDS(1).EQ.203) THEN
        RLAT1=KGDS(4)*1.E-3_KD
        RLON1=KGDS(5)*1.E-3_KD
        RLAT0=KGDS(7)*1.E-3_KD
        RLON0=KGDS(8)*1.E-3_KD
        DLONS=KGDS(9)*1.E-3_KD
        DLATS=KGDS(10)*1.E-3_KD
        DMIDS=SQRT(DLONS*DLONS+DLATS*DLATS)
        IROT=MOD(KGDS(6)/8,2)
        IM=KGDS(2)*2-1
        JM=KGDS(3)
        KSCAN=MOD(KGDS(11)/256,2)
        ISCAN=MOD(KGDS(11)/128,2)
        JSCAN=MOD(KGDS(11)/64,2)
        NSCAN=MOD(KGDS(11)/32,2)
        HI=(-1.)**ISCAN
        HJ=(-1.)**(1-JSCAN)
        SLAT1=SIN(RLAT1/DPR)
        CLAT1=COS(RLAT1/DPR)
        SLAT0=SIN(RLAT0/DPR)
        CLAT0=COS(RLAT0/DPR)
        HS0=SIGN(1._KD,MOD(RLON1-RLON0+180+3600,360._KD)-180)
        CLON1=COS((RLON1-RLON0)/DPR)
        SLATR=CLAT0*SLAT1-SLAT0*CLAT1*CLON1
        CLATR=SQRT(1-SLATR**2)
        CLONR=(CLAT0*CLAT1*CLON1+SLAT0*SLAT1)/CLATR
        RLATLR=DPR*ASIN(max(min(SLATR,1.0_KD),-1.0_KD))
        RLATCR=RLATLR+(JM-1)/2.*DLATS
        RLONLR=HS0*DPR*ACOS(max(min(CLONR,1.0_KD),-1.0_KD))
        RLONCR=RLONLR+(IM-1)/2.*DLONS
c$$$        write(0,*) 'clonr=',clonr,' clatr=',clatr,' clon1=',clon1
c$$$        write(0,*)'hs0=',hs0,' acos(clonr)=',acos(clonr),' dlons=',dlons
c$$$        write(0,*) 'rlonlr=',rlonlr
C        DLATS=RLATR/(-(JM-1)/2)
C        DLONS=RLONR/(-(IM-1)/2)
        IF(KSCAN.EQ.0) THEN
          IS1=(JM+1)/2
        ELSE
          IS1=JM/2
        ENDIF
        XMIN=0
        XMAX=IM+1
        IF(IM.EQ.NINT(360/ABS(DLONS))) XMAX=IM+2
        YMIN=0
        YMAX=JM+1
        NRET=0
 3033   format('gdswizcb: 203 proj info: rlat1=',F0.3,' rlon1=',F0.3,
     &       ' rlat0=',F0.3,' rlon0=',F0.3,' dlons=',F0.3,
     &       ' dlats=',F0.3,' rloncr=',F0.3,' rlatcr=',F0.3)
        write(0,3033) rlat1,rlon1,rlat0,rlon0,dlons,dlats,rloncr,rlatcr
C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
C  TRANSLATE GRID COORDINATES TO EARTH COORDINATES
        IF(IOPT.EQ.0.OR.IOPT.EQ.1) THEN
C          Calculate grid center point in rotated coordinates:
           XPTFC=(JM-1)/2. + ( (IM-1)/2. - IS1 )
           YPTFC=(JM-1)/2. - ( (IM-1)/2. - IS1 ) + KSCAN

          DO N=1,NPTS
            XPTF=YPTS(N)+(XPTS(N)-IS1)
            YPTF=YPTS(N)-(XPTS(N)-IS1)+KSCAN
            IF(XPTF.GE.XMIN.AND.XPTF.LE.XMAX.AND.
     &         YPTF.GE.YMIN.AND.YPTF.LE.YMAX) THEN
              RLONR=RLONLR+(XPTF-1)*DLONS
              RLATR=RLATLR+(YPTF-1)*DLATS
C              HS=HI*SIGN(1.,XPTF-(IM-1)/2.)
              HS=HI*SIGN(1._KD,XPTF-XPTFC+1)
              IF(ABS(HS)/=1.) HS=1.
              RLONR=(XPTF-XPTFC)*DLONS+RLONCR
              RLATR=(YPTF-YPTFC)*DLATS+RLATCR
              CLONR=COS(RLONR/DPR)
              SLATR=SIN(RLATR/DPR)
              CLATR=COS(RLATR/DPR)
              SLAT=CLAT0*SLATR+SLAT0*CLATR*CLONR
c$$$              write(0,*) 'hs=',hs,' rlonr=',rlonr,' rlatr=',rlatr
              IF(SLAT.LE.-1) THEN
                CLAT=0.
                CLON=COS(RLON0/DPR)
                RLON(N)=0
                RLAT(N)=-90
              ELSEIF(SLAT.GE.1) THEN
                CLAT=0.
                CLON=COS(RLON0/DPR)
                RLON(N)=0
                RLAT(N)=90
              ELSE
                CLAT=SQRT(1-SLAT**2)
                CLON=(CLAT0*CLATR*CLONR-SLAT0*SLATR)/CLAT
                CLON=MIN(MAX(CLON,-1._KD),1._KD)
                RLON(N)=MOD(RLON0+HS*DPR*ACOS(max(min(1.0_KD,CLON),
     &               -1.0_KD))+3600,360._KD)
c$$$                IF( (RLON(N)>=RLON1) .neqv. (HS0>0) ) THEN
c$$$                   IF(RLON(N)<180.) THEN
c$$$                      RLON(N)=RLON(N)-360.
c$$$                   ELSE
c$$$                      RLON(N)=RLON(N)+360.
c$$$                   ENDIF
c$$$                ENDIF
                RLAT(N)=DPR*ASIN(MAX(MIN(SLAT,1.0_KD),-1.0_KD))
              ENDIF
c$$$ 100          format('N=',I0,' lon=',F0.3,' lat=',F0.3,
c$$$     &             ' from x=',F0.3,' y=',F0.3,' slat=',F0.3)
c$$$              write(0,100) n,rlon(n),rlat(n),xptf,yptf,slat
              NRET=NRET+1
              IF(LROT.EQ.1) THEN
                IF(IROT.EQ.1) THEN
                  IF(CLATR.LE.0) THEN
                    CROT(N)=-SIGN(1._KD,SLATR*SLAT0)
                    SROT(N)=0
                  ELSE
                    SLON=SIN((RLON(N)-RLON0)/DPR)
                    CROT(N)=(CLAT0*CLAT+SLAT0*SLAT*CLON)/CLATR
                    SROT(N)=SLAT0*SLON/CLATR
                  ENDIF
                ELSE
                  CROT(N)=1
                  SROT(N)=0
                ENDIF
              ENDIF
            ELSE
              RLON(N)=FILL
              RLAT(N)=FILL
            ENDIF
          ENDDO
C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
C  TRANSLATE EARTH COORDINATES TO GRID COORDINATES
        ELSEIF(IOPT.EQ.-1) THEN
          DO N=1,NPTS
            IF(ABS(RLON(N)).LE.360.AND.ABS(RLAT(N)).LE.90) THEN
              HS=SIGN(1._KD,MOD(RLON(N)-RLON0+180+3600,360._KD)-180)
              CLON=COS((RLON(N)-RLON0)/DPR)
              SLAT=SIN(RLAT(N)/DPR)
              CLAT=COS(RLAT(N)/DPR)
              SLATR=CLAT0*SLAT-SLAT0*CLAT*CLON
              IF(SLATR.LE.-1) THEN
                CLATR=0.
                RLONR=0
                RLATR=-90
              ELSEIF(SLATR.GE.1) THEN
                CLATR=0.
                RLONR=0
                RLATR=90
              ELSE
                CLATR=SQRT(1-SLATR**2)
                CLONR=(CLAT0*CLAT*CLON+SLAT0*SLAT)/CLATR
                CLONR=MIN(MAX(CLONR,-1._KD),1._KD)
                RLONR=HS*DPR*ACOS(MAX(MIN(CLONR,1.0_KD),-1.0_KD))
                RLATR=DPR*ASIN(MAX(MIN(SLATR,1.0_KD),-1.0_KD))
              ENDIF
c$$$              XPTF=(IM+1)/2+RLONR/DLONS
c$$$              YPTF=(JM+1)/2+RLATR/DLATS
c$$$              XPTF=(IM-1)/2.+(RLONR-RLONCR)/DLONS
c$$$              YPTF=(JM-1)/2.+(RLATR-RLATCR)/DLATS
              XPTF=(RLONR-RLONLR)/DLONS+1
              YPTF=(RLATR-RLATLR)/DLATS+1
c$$$ 200          format('N=',I0,' lon=',F0.3,' lat=',F0.3,
c$$$     &             ' becomes x=',F0.3,' y=',F0.3)
c$$$              write(0,200) n,rlon(n),rlat(n),xptf,yptf
              IF(XPTF.GE.XMIN.AND.XPTF.LE.XMAX.AND.
     &           YPTF.GE.YMIN.AND.YPTF.LE.YMAX) THEN
                XPTS(N)=IS1+(XPTF-(YPTF-KSCAN))/2
                YPTS(N)=(XPTF+(YPTF-KSCAN))/2
                NRET=NRET+1
                IF(LROT.EQ.1) THEN
                  IF(IROT.EQ.1) THEN
                    IF(CLATR.LE.0) THEN
                      CROT(N)=-SIGN(1._KD,SLATR*SLAT0)
                      SROT(N)=0
                    ELSE
                      SLON=SIN((RLON(N)-RLON0)/DPR)
                      CROT(N)=(CLAT0*CLAT+SLAT0*SLAT*CLON)/CLATR
                      SROT(N)=SLAT0*SLON/CLATR
                    ENDIF
                  ELSE
                    CROT(N)=1
                    SROT(N)=0
                  ENDIF
                ENDIF
              ELSE
                XPTS(N)=FILL
                YPTS(N)=FILL
              ENDIF
            ELSE
              XPTS(N)=FILL
              YPTS(N)=FILL
            ENDIF
          ENDDO
        ENDIF
C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
C  PROJECTION UNRECOGNIZED
      ELSE
        IRET=-1
        IF(IOPT.GE.0) THEN
          DO N=1,NPTS
            RLON(N)=FILL
            RLAT(N)=FILL
          ENDDO
        ENDIF
        IF(IOPT.LE.0) THEN
          DO N=1,NPTS
            XPTS(N)=FILL
            YPTS(N)=FILL
          ENDDO
        ENDIF
      ENDIF
C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
      END