SUBROUTINE CBESH(Z, FNU, KODE, M, N, CY, NZ, IERR)
C***BEGIN PROLOGUE  CBESH
C***DATE WRITTEN   830501   (YYMMDD)
C***REVISION DATE  890801   (YYMMDD)
C***CATEGORY NO.  B5K
C***KEYWORDS  H-BESSEL FUNCTIONS,BESSEL FUNCTIONS OF COMPLEX ARGUMENT,
C             BESSEL FUNCTIONS OF THIRD KIND,HANKEL FUNCTIONS
C***AUTHOR  AMOS, DONALD E., SANDIA NATIONAL LABORATORIES
C***PURPOSE  TO COMPUTE THE H-BESSEL FUNCTIONS OF A COMPLEX ARGUMENT
C***DESCRIPTION
C
C         ON KODE=1, CBESH COMPUTES AN N MEMBER SEQUENCE OF COMPLEX
C         HANKEL (BESSEL) FUNCTIONS CY(J)=H(M,FNU+J-1,Z) FOR KINDS M=1
C         OR 2, REAL, NONNEGATIVE ORDERS FNU+J-1, J=1,...,N, AND COMPLEX
C         Z.NE.CMPLX(0.0E0,0.0E0) IN THE CUT PLANE -PI.LT.ARG(Z).LE.PI.
C         ON KODE=2, CBESH COMPUTES THE SCALED HANKEL FUNCTIONS
C
C         CY(I)=H(M,FNU+J-1,Z)*EXP(-MM*Z*I)       MM=3-2M,      I**2=-1.
C
C         WHICH REMOVES THE EXPONENTIAL BEHAVIOR IN BOTH THE UPPER
C         AND LOWER HALF PLANES. DEFINITIONS AND NOTATION ARE FOUND IN
C         THE NBS HANDBOOK OF MATHEMATICAL FUNCTIONS (REF. 1).
C
C         INPUT
C           Z      - Z=CMPLX(X,Y), Z.NE.CMPLX(0.,0.),-PI.LT.ARG(Z).LE.PI
C           FNU    - ORDER OF INITIAL H FUNCTION, FNU.GE.0.0E0
C           KODE   - A PARAMETER TO INDICATE THE SCALING OPTION
C                    KODE= 1  RETURNS
C                             CY(J)=H(M,FNU+J-1,Z),      J=1,...,N
C                        = 2  RETURNS
C                             CY(J)=H(M,FNU+J-1,Z)*EXP(-I*Z*(3-2M))
C                                  J=1,...,N  ,  I**2=-1
C           M      - KIND OF HANKEL FUNCTION, M=1 OR 2
C           N      - NUMBER OF MEMBERS OF THE SEQUENCE, N.GE.1
C
C         OUTPUT
C           CY     - A COMPLEX VECTOR WHOSE FIRST N COMPONENTS CONTAIN
C                    VALUES FOR THE SEQUENCE
C                    CY(J)=H(M,FNU+J-1,Z)  OR
C                    CY(J)=H(M,FNU+J-1,Z)*EXP(-I*Z*(3-2M))  J=1,...,N
C                    DEPENDING ON KODE, I**2=-1.
C           NZ     - NUMBER OF COMPONENTS SET TO ZERO DUE TO UNDERFLOW,
C                    NZ= 0   , NORMAL RETURN
C                    NZ.GT.0 , FIRST NZ COMPONENTS OF CY SET TO ZERO
C                              DUE TO UNDERFLOW, CY(J)=CMPLX(0.0,0.0)
C                              J=1,...,NZ WHEN Y.GT.0.0 AND M=1 OR
C                              Y.LT.0.0 AND M=2. FOR THE COMPLMENTARY
C                              HALF PLANES, NZ STATES ONLY THE NUMBER
C                              OF UNDERFLOWS.
C           IERR    -ERROR FLAG
C                    IERR=0, NORMAL RETURN - COMPUTATION COMPLETED
C                    IERR=1, INPUT ERROR   - NO COMPUTATION
C                    IERR=2, OVERFLOW      - NO COMPUTATION, FNU+N-1 TOO
C                            LARGE OR CABS(Z) TOO SMALL OR BOTH
C                    IERR=3, CABS(Z) OR FNU+N-1 LARGE - COMPUTATION DONE
C                            BUT LOSSES OF SIGNIFCANCE BY ARGUMENT
C                            REDUCTION PRODUCE LESS THAN HALF OF MACHINE
C                            ACCURACY
C                    IERR=4, CABS(Z) OR FNU+N-1 TOO LARGE - NO COMPUTA-
C                            TION BECAUSE OF COMPLETE LOSSES OF SIGNIFI-
C                            CANCE BY ARGUMENT REDUCTION
C                    IERR=5, ERROR              - NO COMPUTATION,
C                            ALGORITHM TERMINATION CONDITION NOT MET
C
C***LONG DESCRIPTION
C
C         THE COMPUTATION IS CARRIED OUT BY THE RELATION
C
C         H(M,FNU,Z)=(1/MP)*EXP(-MP*FNU)*K(FNU,Z*EXP(-MP))
C             MP=MM*HPI*I,  MM=3-2*M,  HPI=PI/2,  I**2=-1
C
C         FOR M=1 OR 2 WHERE THE K BESSEL FUNCTION IS COMPUTED FOR THE
C         RIGHT HALF PLANE RE(Z).GE.0.0. THE K FUNCTION IS CONTINUED
C         TO THE LEFT HALF PLANE BY THE RELATION
C
C         K(FNU,Z*EXP(MP)) = EXP(-MP*FNU)*K(FNU,Z)-MP*I(FNU,Z)
C         MP=MR*PI*I, MR=+1 OR -1, RE(Z).GT.0, I**2=-1
C
C         WHERE I(FNU,Z) IS THE I BESSEL FUNCTION.
C
C         EXPONENTIAL DECAY OF H(M,FNU,Z) OCCURS IN THE UPPER HALF Z
C         PLANE FOR M=1 AND THE LOWER HALF Z PLANE FOR M=2.  EXPONENTIAL
C         GROWTH OCCURS IN THE COMPLEMENTARY HALF PLANES.  SCALING
C         BY EXP(-MM*Z*I) REMOVES THE EXPONENTIAL BEHAVIOR IN THE
C         WHOLE Z PLANE FOR Z TO INFINITY.
C
C         FOR NEGATIVE ORDERS,THE FORMULAE
C
C               H(1,-FNU,Z) = H(1,FNU,Z)*CEXP( PI*FNU*I)
C               H(2,-FNU,Z) = H(2,FNU,Z)*CEXP(-PI*FNU*I)
C                         I**2=-1
C
C         CAN BE USED.
C
C         IN MOST COMPLEX VARIABLE COMPUTATION, ONE MUST EVALUATE ELE-
C         MENTARY FUNCTIONS. WHEN THE MAGNITUDE OF Z OR FNU+N-1 IS
C         LARGE, LOSSES OF SIGNIFICANCE BY ARGUMENT REDUCTION OCCUR.
C         CONSEQUENTLY, IF EITHER ONE EXCEEDS U1=SQRT(0.5/UR), THEN
C         LOSSES EXCEEDING HALF PRECISION ARE LIKELY AND AN ERROR FLAG
C         IERR=3 IS TRIGGERED WHERE UR=R1MACH(4)=UNIT ROUNDOFF. ALSO
C         IF EITHER IS LARGER THAN U2=0.5/UR, THEN ALL SIGNIFICANCE IS
C         LOST AND IERR=4. IN ORDER TO USE THE INT FUNCTION, ARGUMENTS
C         MUST BE FURTHER RESTRICTED NOT TO EXCEED THE LARGEST MACHINE
C         INTEGER, U3=I1MACH(9). THUS, THE MAGNITUDE OF Z AND FNU+N-1 IS
C         RESTRICTED BY MIN(U2,U3). ON 32 BIT MACHINES, U1,U2, AND U3
C         ARE APPROXIMATELY 2.0E+3, 4.2E+6, 2.1E+9 IN SINGLE PRECISION
C         ARITHMETIC AND 1.3E+8, 1.8E+16, 2.1E+9 IN DOUBLE PRECISION
C         ARITHMETIC RESPECTIVELY. THIS MAKES U2 AND U3 LIMITING IN
C         THEIR RESPECTIVE ARITHMETICS. THIS MEANS THAT ONE CAN EXPECT
C         TO RETAIN, IN THE WORST CASES ON 32 BIT MACHINES, NO DIGITS
C         IN SINGLE AND ONLY 7 DIGITS IN DOUBLE PRECISION ARITHMETIC.
C         SIMILAR CONSIDERATIONS HOLD FOR OTHER MACHINES.
C
C         THE APPROXIMATE RELATIVE ERROR IN THE MAGNITUDE OF A COMPLEX
C         BESSEL FUNCTION CAN BE EXPRESSED BY P*10**S WHERE P=MAX(UNIT
C         ROUNDOFF,1.0E-18) IS THE NOMINAL PRECISION AND 10**S REPRE-
C         SENTS THE INCREASE IN ERROR DUE TO ARGUMENT REDUCTION IN THE
C         ELEMENTARY FUNCTIONS. HERE, S=MAX(1,ABS(LOG10(CABS(Z))),
C         ABS(LOG10(FNU))) APPROXIMATELY (I.E. S=MAX(1,ABS(EXPONENT OF
C         CABS(Z),ABS(EXPONENT OF FNU)) ). HOWEVER, THE PHASE ANGLE MAY
C         HAVE ONLY ABSOLUTE ACCURACY. THIS IS MOST LIKELY TO OCCUR WHEN
C         ONE COMPONENT (IN ABSOLUTE VALUE) IS LARGER THAN THE OTHER BY
C         SEVERAL ORDERS OF MAGNITUDE. IF ONE COMPONENT IS 10**K LARGER
C         THAN THE OTHER, THEN ONE CAN EXPECT ONLY MAX(ABS(LOG10(P))-K,
C         0) SIGNIFICANT DIGITS; OR, STATED ANOTHER WAY, WHEN K EXCEEDS
C         THE EXPONENT OF P, NO SIGNIFICANT DIGITS REMAIN IN THE SMALLER
C         COMPONENT. HOWEVER, THE PHASE ANGLE RETAINS ABSOLUTE ACCURACY
C         BECAUSE, IN COMPLEX ARITHMETIC WITH PRECISION P, THE SMALLER
C         COMPONENT WILL NOT (AS A RULE) DECREASE BELOW P TIMES THE
C         MAGNITUDE OF THE LARGER COMPONENT. IN THESE EXTREME CASES,
C         THE PRINCIPAL PHASE ANGLE IS ON THE ORDER OF +P, -P, PI/2-P,
C         OR -PI/2+P.
C
C***REFERENCES  HANDBOOK OF MATHEMATICAL FUNCTIONS BY M. ABRAMOWITZ
C                 AND I. A. STEGUN, NBS AMS SERIES 55, U.S. DEPT. OF
C                 COMMERCE, 1955.
C
C               COMPUTATION OF BESSEL FUNCTIONS OF COMPLEX ARGUMENT
C                 BY D. E. AMOS, SAND83-0083, MAY, 1983.
C
C               COMPUTATION OF BESSEL FUNCTIONS OF COMPLEX ARGUMENT
C                 AND LARGE ORDER BY D. E. AMOS, SAND83-0643, MAY, 1983
C
C               A SUBROUTINE PACKAGE FOR BESSEL FUNCTIONS OF A COMPLEX
C                 ARGUMENT AND NONNEGATIVE ORDER BY D. E. AMOS, SAND85-
C                 1018, MAY, 1985
C
C               A PORTABLE PACKAGE FOR BESSEL FUNCTIONS OF A COMPLEX
C                 ARGUMENT AND NONNEGATIVE ORDER BY D. E. AMOS, TRANS.
C                 MATH. SOFTWARE, 1986
C
C***ROUTINES CALLED  CACON,CBKNU,CBUNK,CUOIK,I1MACH,R1MACH
C***END PROLOGUE  CBESH
C
      COMPLEX CY, Z, ZN, ZT, CSGN
      REAL AA, ALIM, ALN, ARG, AZ, CPN, DIG, ELIM, FMM, FN, FNU, FNUL,
     * HPI, RHPI, RL, R1M5, SGN, SPN, TOL, UFL, XN, XX, YN, YY, R1MACH,
     * BB, ASCLE, RTOL, ATOL
      INTEGER I, IERR, INU, INUH, IR, K, KODE, K1, K2, M,
     * MM, MR, N, NN, NUF, NW, NZ, I1MACH
      DIMENSION CY(N)
C
      DATA HPI /1.57079632679489662E0/
C
C***FIRST EXECUTABLE STATEMENT  CBESH
      NZ=0
      XX = REAL(Z)
      YY = AIMAG(Z)
      IERR = 0
      IF (XX.EQ.0.0E0 .AND. YY.EQ.0.0E0) IERR=1
      IF (FNU.LT.0.0E0) IERR=1
      IF (M.LT.1 .OR. M.GT.2) IERR=1
      IF (KODE.LT.1 .OR. KODE.GT.2) IERR=1
      IF (N.LT.1) IERR=1
      IF (IERR.NE.0) RETURN
      NN = N
C-----------------------------------------------------------------------
C     SET PARAMETERS RELATED TO MACHINE CONSTANTS.
C     TOL IS THE APPROXIMATE UNIT ROUNDOFF LIMITED TO 1.0E-18.
C     ELIM IS THE APPROXIMATE EXPONENTIAL OVER- AND UNDERFLOW LIMIT.
C     EXP(-ELIM).LT.EXP(-ALIM)=EXP(-ELIM)/TOL    AND
C     EXP(ELIM).GT.EXP(ALIM)=EXP(ELIM)*TOL       ARE INTERVALS NEAR
C     UNDERFLOW AND OVERFLOW LIMITS WHERE SCALED ARITHMETIC IS DONE.
C     RL IS THE LOWER BOUNDARY OF THE ASYMPTOTIC EXPANSION FOR LARGE Z.
C     DIG = NUMBER OF BASE 10 DIGITS IN TOL = 10**(-DIG).
C     FNUL IS THE LOWER BOUNDARY OF THE ASYMPTOTIC SERIES FOR LARGE FNU
C-----------------------------------------------------------------------
      TOL = AMAX1(R1MACH(4),1.0E-18)
      K1 = I1MACH(12)
      K2 = I1MACH(13)
      R1M5 = R1MACH(5)
      K = MIN0(IABS(K1),IABS(K2))
      ELIM = 2.303E0*(FLOAT(K)*R1M5-3.0E0)
      K1 = I1MACH(11) - 1
      AA = R1M5*FLOAT(K1)
      DIG = AMIN1(AA,18.0E0)
      AA = AA*2.303E0
      ALIM = ELIM + AMAX1(-AA,-41.45E0)
      FNUL = 10.0E0 + 6.0E0*(DIG-3.0E0)
      RL = 1.2E0*DIG + 3.0E0
      FN = FNU + FLOAT(NN-1)
      MM = 3 - M - M
      FMM = FLOAT(MM)
      ZN = Z*CMPLX(0.0E0,-FMM)
      XN = REAL(ZN)
      YN = AIMAG(ZN)
      AZ = CABS(Z)
C-----------------------------------------------------------------------
C     TEST FOR RANGE
C-----------------------------------------------------------------------
      AA = 0.5E0/TOL
      BB=FLOAT(I1MACH(9))*0.5E0
      AA=AMIN1(AA,BB)
      IF(AZ.GT.AA) GO TO 240
      IF(FN.GT.AA) GO TO 240
      AA=SQRT(AA)
      IF(AZ.GT.AA) IERR=3
      IF(FN.GT.AA) IERR=3
C-----------------------------------------------------------------------
C     OVERFLOW TEST ON THE LAST MEMBER OF THE SEQUENCE
C-----------------------------------------------------------------------
   35 CONTINUE
      UFL = R1MACH(1)*1.0E+3
      IF (AZ.LT.UFL) GO TO 220
      IF (FNU.GT.FNUL) GO TO 90
      IF (FN.LE.1.0E0) GO TO 70
      IF (FN.GT.2.0E0) GO TO 60
      IF (AZ.GT.TOL) GO TO 70
      ARG = 0.5E0*AZ
      ALN = -FN*ALOG(ARG)
      IF (ALN.GT.ELIM) GO TO 220
      GO TO 70
   60 CONTINUE
      CALL CUOIK(ZN, FNU, KODE, 2, NN, CY, NUF, TOL, ELIM, ALIM)
      IF (NUF.LT.0) GO TO 220
      NZ = NZ + NUF
      NN = NN - NUF
C-----------------------------------------------------------------------
C     HERE NN=N OR NN=0 SINCE NUF=0,NN, OR -1 ON RETURN FROM CUOIK
C     IF NUF=NN, THEN CY(I)=CZERO FOR ALL I
C-----------------------------------------------------------------------
      IF (NN.EQ.0) GO TO 130
   70 CONTINUE
      IF ((XN.LT.0.0E0) .OR. (XN.EQ.0.0E0 .AND. YN.LT.0.0E0 .AND.
     * M.EQ.2)) GO TO 80
C-----------------------------------------------------------------------
C     RIGHT HALF PLANE COMPUTATION, XN.GE.0. .AND. (XN.NE.0. .OR.
C     YN.GE.0. .OR. M=1)
C-----------------------------------------------------------------------
      CALL CBKNU(ZN, FNU, KODE, NN, CY, NZ, TOL, ELIM, ALIM)
      GO TO 110
C-----------------------------------------------------------------------
C     LEFT HALF PLANE COMPUTATION
C-----------------------------------------------------------------------
   80 CONTINUE
      MR = -MM
      CALL CACON(ZN, FNU, KODE, MR, NN, CY, NW, RL, FNUL, TOL, ELIM,
     * ALIM)
      IF (NW.LT.0) GO TO 230
      NZ=NW
      GO TO 110
   90 CONTINUE
C-----------------------------------------------------------------------
C     UNIFORM ASYMPTOTIC EXPANSIONS FOR FNU.GT.FNUL
C-----------------------------------------------------------------------
      MR = 0
      IF ((XN.GE.0.0E0) .AND. (XN.NE.0.0E0 .OR. YN.GE.0.0E0 .OR.
     * M.NE.2)) GO TO 100
      MR = -MM
      IF (XN.EQ.0.0E0 .AND. YN.LT.0.0E0) ZN = -ZN
  100 CONTINUE
      CALL CBUNK(ZN, FNU, KODE, MR, NN, CY, NW, TOL, ELIM, ALIM)
      IF (NW.LT.0) GO TO 230
      NZ = NZ + NW
  110 CONTINUE
C-----------------------------------------------------------------------
C     H(M,FNU,Z) = -FMM*(I/HPI)*(ZT**FNU)*K(FNU,-Z*ZT)
C
C     ZT=EXP(-FMM*HPI*I) = CMPLX(0.0,-FMM), FMM=3-2*M, M=1,2
C-----------------------------------------------------------------------
      SGN = SIGN(HPI,-FMM)
C-----------------------------------------------------------------------
C     CALCULATE EXP(FNU*HPI*I) TO MINIMIZE LOSSES OF SIGNIFICANCE
C     WHEN FNU IS LARGE
C-----------------------------------------------------------------------
      INU = INT(FNU)
      INUH = INU/2
      IR = INU - 2*INUH
      ARG = (FNU-FLOAT(INU-IR))*SGN
      RHPI = 1.0E0/SGN
      CPN = RHPI*COS(ARG)
      SPN = RHPI*SIN(ARG)
C     ZN = CMPLX(-SPN,CPN)
      CSGN = CMPLX(-SPN,CPN)
C     IF (MOD(INUH,2).EQ.1) ZN = -ZN
      IF (MOD(INUH,2).EQ.1) CSGN = -CSGN
      ZT = CMPLX(0.0E0,-FMM)
      RTOL = 1.0E0/TOL
      ASCLE = UFL*RTOL
      DO 120 I=1,NN
C       CY(I) = CY(I)*ZN
C       ZN = ZN*ZT
        ZN=CY(I)
        AA=REAL(ZN)
        BB=AIMAG(ZN)
        ATOL=1.0E0
        IF (AMAX1(ABS(AA),ABS(BB)).GT.ASCLE) GO TO 125
          ZN = ZN*CMPLX(RTOL,0.0E0)
          ATOL = TOL
  125   CONTINUE
        ZN = ZN*CSGN
        CY(I) = ZN*CMPLX(ATOL,0.0E0)
        CSGN = CSGN*ZT
  120 CONTINUE
      RETURN
  130 CONTINUE
      IF (XN.LT.0.0E0) GO TO 220
      RETURN
  220 CONTINUE
      IERR=2
      NZ=0
      RETURN
  230 CONTINUE
      IF(NW.EQ.(-1)) GO TO 220
      NZ=0
      IERR=5
      RETURN
  240 CONTINUE
      IERR=4
      GO TO 35
      END