C----------------------------------------------------------------------- SUBROUTINE POLATEV1(IPOPT,KGDSI,KGDSO,MI,MO,KM,IBI,LI,UI,VI, & NO,RLAT,RLON,CROT,SROT,IBO,LO,UO,VO,IRET) C$$$ SUBPROGRAM DOCUMENTATION BLOCK C C SUBPROGRAM: POLATEV1 INTERPOLATE VECTOR FIELDS (BICUBIC) C PRGMMR: IREDELL ORG: W/NMC23 DATE: 96-04-10 C C ABSTRACT: THIS SUBPROGRAM PERFORMS BICUBIC INTERPOLATION C FROM ANY GRID TO ANY GRID FOR VECTOR FIELDS. C IT REQUIRES THAT NO INPUT FIELDS HAVE BITMAPS (IBI=0). C OPTIONS ALLOW CHOICES BETWEEN STRAIGHT BICUBIC (IPOPT(1)=0) C AND CONSTRAINED BICUBIC (IPOPT(1)=1) WHERE THE VALUE IS C CONFINED WITHIN THE RANGE OF THE SURROUNDING 4 POINTS. C BILINEAR USED WITHIN ONE GRID LENGTH OF BOUNDARIES. C ONLY HORIZONTAL INTERPOLATION IS PERFORMED. C THE GRIDS ARE DEFINED BY THEIR GRID DESCRIPTION SECTIONS C (PASSED IN INTEGER FORM AS DECODED BY SUBPROGRAM W3FI63). C THE CURRENT CODE RECOGNIZES THE FOLLOWING PROJECTIONS: C (KGDS(1)=000) EQUIDISTANT CYLINDRICAL C (KGDS(1)=001) MERCATOR CYLINDRICAL C (KGDS(1)=003) LAMBERT CONFORMAL CONICAL C (KGDS(1)=004) GAUSSIAN CYLINDRICAL (SPECTRAL NATIVE) C (KGDS(1)=005) POLAR STEREOGRAPHIC AZIMUTHAL C (KGDS(1)=202) ROTATED EQUIDISTANT CYLINDRICAL (ETA NATIVE) C WHERE KGDS COULD BE EITHER INPUT KGDSI OR OUTPUT KGDSO. C THE INPUT AND OUTPUT VECTORS ARE ROTATED SO THAT THEY ARE C EITHER RESOLVED RELATIVE TO THE DEFINED GRID C IN THE DIRECTION OF INCREASING X AND Y COORDINATES C OR RESOLVED RELATIVE TO EASTERLY AND NORTHERLY DIRECTIONS, C AS DESIGNATED BY THEIR RESPECTIVE GRID DESCRIPTION SECTIONS. C AS AN ADDED BONUS THE NUMBER OF OUTPUT GRID POINTS C AND THEIR LATITUDES AND LONGITUDES ARE ALSO RETURNED C ALONG WITH THEIR VECTOR ROTATION PARAMETERS. C ON THE OTHER HAND, THE OUTPUT CAN BE A SET OF STATION POINTS C IF KGDSO(1)<0, IN WHICH CASE THE NUMBER OF POINTS C AND THEIR LATITUDES AND LONGITUDES MUST BE INPUT C ALONG WITH THEIR VECTOR ROTATION PARAMETERS. C OUTPUT BITMAPS WILL ONLY BE CREATED WHEN THE OUTPUT GRID C EXTENDS OUTSIDE OF THE DOMAIN OF THE INPUT GRID. C THE OUTPUT FIELD IS SET TO 0 WHERE THE OUTPUT BITMAP IS OFF. C C PROGRAM HISTORY LOG: C 96-04-10 IREDELL C C USAGE: CALL POLATEV1(IPOPT,KGDSI,KGDSO,MI,MO,KM,IBI,LI,UI,VI, C & NO,RLAT,RLON,CROT,SROT,IBO,LO,UO,VO,IRET) C C INPUT ARGUMENT LIST: C IPOPT - INTEGER (20) INTERPOLATION OPTIONS C IPOPT(1)=0 FOR STRAIGHT BICUBIC; C IPOPT(1)=1 FOR CONSTRAINED BICUBIC WHERE VALUE IS C CONFINED WITHIN THE RANGE OF THE SURROUNDING 4 POINTS. C KGDSI - INTEGER (200) INPUT GDS PARAMETERS AS DECODED BY W3FI63 C KGDSO - INTEGER (200) OUTPUT GDS PARAMETERS C (KGDSO(1)<0 IMPLIES RANDOM STATION POINTS) C MI - INTEGER SKIP NUMBER BETWEEN INPUT GRID FIELDS IF KM>1 C OR DIMENSION OF INPUT GRID FIELDS IF KM=1 C MO - INTEGER SKIP NUMBER BETWEEN OUTPUT GRID FIELDS IF KM>1 C OR DIMENSION OF OUTPUT GRID FIELDS IF KM=1 C KM - INTEGER NUMBER OF FIELDS TO INTERPOLATE C IBI - INTEGER (KM) INPUT BITMAP FLAGS (MUST BE ALL 0) C LI - LOGICAL*1 (MI,KM) INPUT BITMAPS (IF SOME IBI(K)=1) C UI - REAL (MI,KM) INPUT U-COMPONENT FIELDS TO INTERPOLATE C VI - REAL (MI,KM) INPUT V-COMPONENT FIELDS TO INTERPOLATE C NO - INTEGER NUMBER OF OUTPUT POINTS (ONLY IF KGDSO(1)<0) C RLAT - REAL (NO) OUTPUT LATITUDES IN DEGREES (IF KGDSO(1)<0) C RLON - REAL (NO) OUTPUT LONGITUDES IN DEGREES (IF KGDSO(1)<0) C CROT - REAL (NO) VECTOR ROTATION COSINES (IF KGDSO(1)<0) C SROT - REAL (NO) VECTOR ROTATION SINES (IF KGDSO(1)<0) C (UGRID=CROT*UEARTH-SROT*VEARTH; C VGRID=SROT*UEARTH+CROT*VEARTH) C C OUTPUT ARGUMENT LIST: C NO - INTEGER NUMBER OF OUTPUT POINTS (ONLY IF KGDSO(1)>=0) C RLAT - REAL (MO) OUTPUT LATITUDES IN DEGREES (IF KGDSO(1)>=0) C RLON - REAL (MO) OUTPUT LONGITUDES IN DEGREES (IF KGDSO(1)>=0) C CROT - REAL (NO) VECTOR ROTATION COSINES (IF KGDSO(1)>=0) C SROT - REAL (NO) VECTOR ROTATION SINES (IF KGDSO(1)>=0) C (UGRID=CROT*UEARTH-SROT*VEARTH; C VGRID=SROT*UEARTH+CROT*VEARTH) C IBO - INTEGER (KM) OUTPUT BITMAP FLAGS C LO - LOGICAL*1 (MO,KM) OUTPUT BITMAPS (ALWAYS OUTPUT) C UO - REAL (MO,KM) OUTPUT U-COMPONENT FIELDS INTERPOLATED C VO - REAL (MO,KM) OUTPUT V-COMPONENT FIELDS INTERPOLATED C IRET - INTEGER RETURN CODE C 0 SUCCESSFUL INTERPOLATION C 2 UNRECOGNIZED INPUT GRID OR NO GRID OVERLAP C 3 UNRECOGNIZED OUTPUT GRID C 11 INVALID INPUT BITMAPS C C SUBPROGRAMS CALLED: C GDSWIZ GRID DESCRIPTION SECTION WIZARD C (IJKGDS) RETURN FIELD POSITION FOR A GIVEN GRID POINT C (MOVECT) MOVE A VECTOR ALONG A GREAT CIRCLE C POLFIXV MAKE MULTIPLE POLE VECTOR VALUES CONSISTENT C C ATTRIBUTES: C LANGUAGE: FORTRAN 77 C C$$$ CFPP$ EXPAND(IJKGDS,MOVECT) INTEGER IPOPT(20) INTEGER KGDSI(200),KGDSO(200) INTEGER IBI(KM),IBO(KM) LOGICAL*1 LI(MI,KM),LO(MO,KM) REAL UI(MI,KM),VI(MI,KM),UO(MO,KM),VO(MO,KM) REAL RLAT(MO),RLON(MO) REAL CROT(MO),SROT(MO) REAL XPTS(MO),YPTS(MO) REAL XPTI(MI),YPTI(MI),RLOI(MI),RLAI(MI),CROI(MI),SROI(MI) INTEGER N11(MO),N21(MO),N12(MO),N22(MO) REAL W11(MO),W21(MO),W12(MO),W22(MO) REAL C11(MO),C21(MO),C12(MO),C22(MO) REAL S11(MO),S21(MO),S12(MO),S22(MO) PARAMETER(FILL=-9999.) C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C COMPUTE NUMBER OF OUTPUT POINTS AND THEIR LATITUDES AND LONGITUDES. IRET=0 IF(KGDSO(1).GE.0) THEN CALL GDSWIZ(KGDSO, 0,MO,FILL,XPTS,YPTS,RLON,RLAT,NO,1,CROT,SROT) IF(NO.EQ.0) IRET=3 ENDIF CALL GDSWIZ(KGDSI, 0,MI,FILL,XPTI,YPTI,RLOI,RLAI,NV,1,CROI,SROI) C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C LOCATE INPUT POINTS AND COMPUTE THEIR WEIGHTS AND ROTATIONS CALL GDSWIZ(KGDSI,-1,NO,FILL,XPTS,YPTS,RLON,RLAT,NV,0,DUM,DUM) IF(IRET.EQ.0.AND.NV.EQ.0) IRET=2 DO K=1,KM IF(IBI(K).NE.0) IRET=11 ENDDO CMIC$ DO ALL AUTOSCOPE DO K=1,KM DO N=1,NO UO(N,K)=0 VO(N,K)=0 LO(N,K)=.FALSE. ENDDO ENDDO C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C COMPUTE CORNERS IF(IRET.EQ.0) THEN DO N=1,NO XI=XPTS(N) YI=YPTS(N) IF(XI.NE.FILL.AND.YI.NE.FILL) THEN I1=XI-1 I2=I1+3 J1=YI-1 J2=J1+3 XF=XI-I1-1 YF=YI-J1-1 N11(N)=IJKGDS(I1,J1,KGDSI) N21(N)=IJKGDS(I2,J1,KGDSI) N12(N)=IJKGDS(I1,J2,KGDSI) N22(N)=IJKGDS(I2,J2,KGDSI) IF(MIN(N11(N),N21(N),N12(N),N22(N)).GT.0) THEN W11(N)=XF*(1-XF)*(2-XF)*YF*(1-YF)*(2-YF)/36 W21(N)=XF*(1-XF)*(1+XF)*YF*(1-YF)*(2-YF)/36 W12(N)=XF*(1-XF)*(2-XF)*YF*(1-YF)*(1+YF)/36 W22(N)=XF*(1-XF)*(1+XF)*YF*(1-YF)*(1+YF)/36 ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF IF(N11(N).GT.0) THEN CALL MOVECT(RLAI(N11(N)),RLOI(N11(N)),RLAT(N),RLON(N), & CM11,SM11) CALL MOVECT(RLAI(N21(N)),RLOI(N21(N)),RLAT(N),RLON(N), & CM21,SM21) CALL MOVECT(RLAI(N12(N)),RLOI(N12(N)),RLAT(N),RLON(N), & CM12,SM12) CALL MOVECT(RLAI(N22(N)),RLOI(N22(N)),RLAT(N),RLON(N), & CM22,SM22) C11(N)=CM11*CROI(N11(N))+SM11*SROI(N11(N)) S11(N)=SM11*CROI(N11(N))-CM11*SROI(N11(N)) C21(N)=CM21*CROI(N21(N))+SM21*SROI(N21(N)) S21(N)=SM21*CROI(N21(N))-CM21*SROI(N21(N)) C12(N)=CM12*CROI(N12(N))+SM12*SROI(N12(N)) S12(N)=SM12*CROI(N12(N))-CM12*SROI(N12(N)) C22(N)=CM22*CROI(N22(N))+SM22*SROI(N22(N)) S22(N)=SM22*CROI(N22(N))-CM22*SROI(N22(N)) ENDIF ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF ENDDO CMIC$ DO ALL AUTOSCOPE DO K=1,KM DO N=1,NO IF(N11(N).GT.0) THEN U11=C11(N)*UI(N11(N),K)-S11(N)*VI(N11(N),K) V11=S11(N)*UI(N11(N),K)+C11(N)*VI(N11(N),K) U21=C21(N)*UI(N21(N),K)-S21(N)*VI(N21(N),K) V21=S21(N)*UI(N21(N),K)+C21(N)*VI(N21(N),K) U12=C12(N)*UI(N12(N),K)-S12(N)*VI(N12(N),K) V12=S12(N)*UI(N12(N),K)+C12(N)*VI(N12(N),K) U22=C22(N)*UI(N22(N),K)-S22(N)*VI(N22(N),K) V22=S22(N)*UI(N22(N),K)+C22(N)*VI(N22(N),K) UO(N,K)=UO(N,K)+W11(N)*U11+W21(N)*U21 & +W12(N)*U12+W22(N)*U22 VO(N,K)=VO(N,K)+W11(N)*V11+W21(N)*V21 & +W12(N)*V12+W22(N)*V22 ENDIF ENDDO ENDDO C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C COMPUTE TOPS AND BOTTOMS DO N=1,NO XI=XPTS(N) YI=YPTS(N) IF(XI.NE.FILL.AND.YI.NE.FILL) THEN LP=N11(N) IF(LP.GT.0) THEN I1=XI I2=I1+1 J1=YI-1 J2=J1+3 XF=XI-I1 YF=YI-J1-1 N11(N)=IJKGDS(I1,J1,KGDSI) N21(N)=IJKGDS(I2,J1,KGDSI) N12(N)=IJKGDS(I1,J2,KGDSI) N22(N)=IJKGDS(I2,J2,KGDSI) W11(N)=-(1+XF)*(1-XF)*(2-XF)*YF*(1-YF)*(2-YF)/12 W21(N)=-XF*(2-XF)*(1+XF)*YF*(1-YF)*(2-YF)/12 W12(N)=-(1+XF)*(1-XF)*(2-XF)*YF*(1-YF)*(1+YF)/12 W22(N)=-XF*(2-XF)*(1+XF)*YF*(1-YF)*(1+YF)/12 CALL MOVECT(RLAI(N11(N)),RLOI(N11(N)),RLAT(N),RLON(N), & CM11,SM11) CALL MOVECT(RLAI(N21(N)),RLOI(N21(N)),RLAT(N),RLON(N), & CM21,SM21) CALL MOVECT(RLAI(N12(N)),RLOI(N12(N)),RLAT(N),RLON(N), & CM12,SM12) CALL MOVECT(RLAI(N22(N)),RLOI(N22(N)),RLAT(N),RLON(N), & CM22,SM22) C11(N)=CM11*CROI(N11(N))+SM11*SROI(N11(N)) S11(N)=SM11*CROI(N11(N))-CM11*SROI(N11(N)) C21(N)=CM21*CROI(N21(N))+SM21*SROI(N21(N)) S21(N)=SM21*CROI(N21(N))-CM21*SROI(N21(N)) C12(N)=CM12*CROI(N12(N))+SM12*SROI(N12(N)) S12(N)=SM12*CROI(N12(N))-CM12*SROI(N12(N)) C22(N)=CM22*CROI(N22(N))+SM22*SROI(N22(N)) S22(N)=SM22*CROI(N22(N))-CM22*SROI(N22(N)) ENDIF ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF ENDDO CMIC$ DO ALL AUTOSCOPE DO K=1,KM DO N=1,NO IF(N11(N).GT.0) THEN U11=C11(N)*UI(N11(N),K)-S11(N)*VI(N11(N),K) V11=S11(N)*UI(N11(N),K)+C11(N)*VI(N11(N),K) U21=C21(N)*UI(N21(N),K)-S21(N)*VI(N21(N),K) V21=S21(N)*UI(N21(N),K)+C21(N)*VI(N21(N),K) U12=C12(N)*UI(N12(N),K)-S12(N)*VI(N12(N),K) V12=S12(N)*UI(N12(N),K)+C12(N)*VI(N12(N),K) U22=C22(N)*UI(N22(N),K)-S22(N)*VI(N22(N),K) V22=S22(N)*UI(N22(N),K)+C22(N)*VI(N22(N),K) UO(N,K)=UO(N,K)+W11(N)*U11+W21(N)*U21 & +W12(N)*U12+W22(N)*U22 VO(N,K)=VO(N,K)+W11(N)*V11+W21(N)*V21 & +W12(N)*V12+W22(N)*V22 ENDIF ENDDO ENDDO C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C COMPUTE LEFTS AND RIGHTS DO N=1,NO XI=XPTS(N) YI=YPTS(N) IF(XI.NE.FILL.AND.YI.NE.FILL) THEN LP=N11(N) IF(LP.GT.0) THEN I1=XI-1 I2=I1+3 J1=YI J2=J1+1 XF=XI-I1-1 YF=YI-J1 N11(N)=IJKGDS(I1,J1,KGDSI) N21(N)=IJKGDS(I2,J1,KGDSI) N12(N)=IJKGDS(I1,J2,KGDSI) N22(N)=IJKGDS(I2,J2,KGDSI) W11(N)=-XF*(1-XF)*(2-XF)*(1+YF)*(1-YF)*(2-YF)/12 W21(N)=-XF*(1-XF)*(1+XF)*(1+YF)*(1-YF)*(2-YF)/12 W12(N)=-XF*(1-XF)*(2-XF)*YF*(2-YF)*(1+YF)/12 W22(N)=-XF*(1-XF)*(1+XF)*YF*(2-YF)*(1+YF)/12 CALL MOVECT(RLAI(N11(N)),RLOI(N11(N)),RLAT(N),RLON(N), & CM11,SM11) CALL MOVECT(RLAI(N21(N)),RLOI(N21(N)),RLAT(N),RLON(N), & CM21,SM21) CALL MOVECT(RLAI(N12(N)),RLOI(N12(N)),RLAT(N),RLON(N), & CM12,SM12) CALL MOVECT(RLAI(N22(N)),RLOI(N22(N)),RLAT(N),RLON(N), & CM22,SM22) C11(N)=CM11*CROI(N11(N))+SM11*SROI(N11(N)) S11(N)=SM11*CROI(N11(N))-CM11*SROI(N11(N)) C21(N)=CM21*CROI(N21(N))+SM21*SROI(N21(N)) S21(N)=SM21*CROI(N21(N))-CM21*SROI(N21(N)) C12(N)=CM12*CROI(N12(N))+SM12*SROI(N12(N)) S12(N)=SM12*CROI(N12(N))-CM12*SROI(N12(N)) C22(N)=CM22*CROI(N22(N))+SM22*SROI(N22(N)) S22(N)=SM22*CROI(N22(N))-CM22*SROI(N22(N)) ENDIF ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF ENDDO CMIC$ DO ALL AUTOSCOPE DO K=1,KM DO N=1,NO IF(N11(N).GT.0) THEN U11=C11(N)*UI(N11(N),K)-S11(N)*VI(N11(N),K) V11=S11(N)*UI(N11(N),K)+C11(N)*VI(N11(N),K) U21=C21(N)*UI(N21(N),K)-S21(N)*VI(N21(N),K) V21=S21(N)*UI(N21(N),K)+C21(N)*VI(N21(N),K) U12=C12(N)*UI(N12(N),K)-S12(N)*VI(N12(N),K) V12=S12(N)*UI(N12(N),K)+C12(N)*VI(N12(N),K) U22=C22(N)*UI(N22(N),K)-S22(N)*VI(N22(N),K) V22=S22(N)*UI(N22(N),K)+C22(N)*VI(N22(N),K) UO(N,K)=UO(N,K)+W11(N)*U11+W21(N)*U21 & +W12(N)*U12+W22(N)*U22 VO(N,K)=VO(N,K)+W11(N)*V11+W21(N)*V21 & +W12(N)*V12+W22(N)*V22 ENDIF ENDDO ENDDO C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - C COMPUTE CENTERS DO N=1,NO XI=XPTS(N) YI=YPTS(N) IF(XI.NE.FILL.AND.YI.NE.FILL) THEN LP=N11(N) I1=XI I2=I1+1 J1=YI J2=J1+1 XF=XI-I1 YF=YI-J1 N11(N)=IJKGDS(I1,J1,KGDSI) N21(N)=IJKGDS(I2,J1,KGDSI) N12(N)=IJKGDS(I1,J2,KGDSI) N22(N)=IJKGDS(I2,J2,KGDSI) IF(LP.GT.0) THEN W11(N)=(1+XF)*(1-XF)*(2-XF)*(1+YF)*(1-YF)*(2-YF)/4 W21(N)=XF*(2-XF)*(1+XF)*(1+YF)*(1-YF)*(2-YF)/4 W12(N)=(1+XF)*(1-XF)*(2-XF)*YF*(2-YF)*(1+YF)/4 W22(N)=XF*(2-XF)*(1+XF)*YF*(2-YF)*(1+YF)/4 ELSEIF(MIN(N11(N),N21(N),N12(N),N22(N)).GT.0) THEN W11(N)=(1-XF)*(1-YF) W21(N)=XF*(1-YF) W12(N)=(1-XF)*YF W22(N)=XF*YF ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF IF(N11(N).GT.0) THEN CALL MOVECT(RLAI(N11(N)),RLOI(N11(N)),RLAT(N),RLON(N), & CM11,SM11) CALL MOVECT(RLAI(N21(N)),RLOI(N21(N)),RLAT(N),RLON(N), & CM21,SM21) CALL MOVECT(RLAI(N12(N)),RLOI(N12(N)),RLAT(N),RLON(N), & CM12,SM12) CALL MOVECT(RLAI(N22(N)),RLOI(N22(N)),RLAT(N),RLON(N), & CM22,SM22) C11(N)=CM11*CROI(N11(N))+SM11*SROI(N11(N)) S11(N)=SM11*CROI(N11(N))-CM11*SROI(N11(N)) C21(N)=CM21*CROI(N21(N))+SM21*SROI(N21(N)) S21(N)=SM21*CROI(N21(N))-CM21*SROI(N21(N)) C12(N)=CM12*CROI(N12(N))+SM12*SROI(N12(N)) S12(N)=SM12*CROI(N12(N))-CM12*SROI(N12(N)) C22(N)=CM22*CROI(N22(N))+SM22*SROI(N22(N)) S22(N)=SM22*CROI(N22(N))-CM22*SROI(N22(N)) ENDIF ELSE N11(N)=0 N21(N)=0 N12(N)=0 N22(N)=0 ENDIF ENDDO CMIC$ DO ALL AUTOSCOPE DO K=1,KM DO N=1,NO IF(N11(N).GT.0) THEN U11=C11(N)*UI(N11(N),K)-S11(N)*VI(N11(N),K) V11=S11(N)*UI(N11(N),K)+C11(N)*VI(N11(N),K) U21=C21(N)*UI(N21(N),K)-S21(N)*VI(N21(N),K) V21=S21(N)*UI(N21(N),K)+C21(N)*VI(N21(N),K) U12=C12(N)*UI(N12(N),K)-S12(N)*VI(N12(N),K) V12=S12(N)*UI(N12(N),K)+C12(N)*VI(N12(N),K) U22=C22(N)*UI(N22(N),K)-S22(N)*VI(N22(N),K) V22=S22(N)*UI(N22(N),K)+C22(N)*VI(N22(N),K) UO(N,K)=UO(N,K)+W11(N)*U11+W21(N)*U21 & +W12(N)*U12+W22(N)*U22 VO(N,K)=VO(N,K)+W11(N)*V11+W21(N)*V21 & +W12(N)*V12+W22(N)*V22 IF(IPOPT(1).GT.0) THEN UMIN=MIN(U11,U21,U12,U22) VMIN=MIN(V11,V21,V12,V22) UMAX=MAX(U11,U21,U12,U22) VMAX=MAX(V11,V21,V12,V22) UO(N,K)=MIN(MAX(UO(N,K),UMIN),UMAX) VO(N,K)=MIN(MAX(VO(N,K),VMIN),VMAX) ENDIF LO(N,K)=.TRUE. ENDIF ENDDO ENDDO ENDIF C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CMIC$ DO ALL AUTOSCOPE DO K=1,KM IBO(K)=IBI(K) DO N=1,NO IF(LO(N,K)) THEN UROT=CROT(N)*UO(N,K)-SROT(N)*VO(N,K) VROT=SROT(N)*UO(N,K)+CROT(N)*VO(N,K) UO(N,K)=UROT VO(N,K)=VROT ELSE IBO(K)=1 UO(N,K)=0. VO(N,K)=0. ENDIF ENDDO ENDDO IF(KGDSO(1).EQ.0) CALL POLFIXV(NO,MO,KM,RLAT,RLON,IBO,LO,UO,VO) C - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END