mirror of
https://git.planet-casio.com/Lephenixnoir/OpenLibm.git
synced 2024-12-29 13:03:42 +01:00
244 lines
10 KiB
Fortran
244 lines
10 KiB
Fortran
SUBROUTINE ZBESY(ZR, ZI, FNU, KODE, N, CYR, CYI, NZ, CWRKR, CWRKI,
|
|
* IERR)
|
|
C***BEGIN PROLOGUE ZBESY
|
|
C***DATE WRITTEN 830501 (YYMMDD)
|
|
C***REVISION DATE 890801 (YYMMDD)
|
|
C***CATEGORY NO. B5K
|
|
C***KEYWORDS Y-BESSEL FUNCTION,BESSEL FUNCTION OF COMPLEX ARGUMENT,
|
|
C BESSEL FUNCTION OF SECOND KIND
|
|
C***AUTHOR AMOS, DONALD E., SANDIA NATIONAL LABORATORIES
|
|
C***PURPOSE TO COMPUTE THE Y-BESSEL FUNCTION OF A COMPLEX ARGUMENT
|
|
C***DESCRIPTION
|
|
C
|
|
C ***A DOUBLE PRECISION ROUTINE***
|
|
C
|
|
C ON KODE=1, CBESY COMPUTES AN N MEMBER SEQUENCE OF COMPLEX
|
|
C BESSEL FUNCTIONS CY(I)=Y(FNU+I-1,Z) FOR REAL, NONNEGATIVE
|
|
C ORDERS FNU+I-1, I=1,...,N AND COMPLEX Z IN THE CUT PLANE
|
|
C -PI.LT.ARG(Z).LE.PI. ON KODE=2, CBESY RETURNS THE SCALED
|
|
C FUNCTIONS
|
|
C
|
|
C CY(I)=EXP(-ABS(Y))*Y(FNU+I-1,Z) I = 1,...,N , Y=AIMAG(Z)
|
|
C
|
|
C WHICH REMOVE THE EXPONENTIAL GROWTH IN BOTH THE UPPER AND
|
|
C LOWER HALF PLANES FOR Z TO INFINITY. DEFINITIONS AND NOTATION
|
|
C ARE FOUND IN THE NBS HANDBOOK OF MATHEMATICAL FUNCTIONS
|
|
C (REF. 1).
|
|
C
|
|
C INPUT ZR,ZI,FNU ARE DOUBLE PRECISION
|
|
C ZR,ZI - Z=CMPLX(ZR,ZI), Z.NE.CMPLX(0.0D0,0.0D0),
|
|
C -PI.LT.ARG(Z).LE.PI
|
|
C FNU - ORDER OF INITIAL Y FUNCTION, FNU.GE.0.0D0
|
|
C KODE - A PARAMETER TO INDICATE THE SCALING OPTION
|
|
C KODE= 1 RETURNS
|
|
C CY(I)=Y(FNU+I-1,Z), I=1,...,N
|
|
C = 2 RETURNS
|
|
C CY(I)=Y(FNU+I-1,Z)*EXP(-ABS(Y)), I=1,...,N
|
|
C WHERE Y=AIMAG(Z)
|
|
C N - NUMBER OF MEMBERS OF THE SEQUENCE, N.GE.1
|
|
C CWRKR, - DOUBLE PRECISION WORK VECTORS OF DIMENSION AT
|
|
C CWRKI AT LEAST N
|
|
C
|
|
C OUTPUT CYR,CYI ARE DOUBLE PRECISION
|
|
C CYR,CYI- DOUBLE PRECISION VECTORS WHOSE FIRST N COMPONENTS
|
|
C CONTAIN REAL AND IMAGINARY PARTS FOR THE SEQUENCE
|
|
C CY(I)=Y(FNU+I-1,Z) OR
|
|
C CY(I)=Y(FNU+I-1,Z)*EXP(-ABS(Y)) I=1,...,N
|
|
C DEPENDING ON KODE.
|
|
C NZ - NZ=0 , A NORMAL RETURN
|
|
C NZ.GT.0 , NZ COMPONENTS OF CY SET TO ZERO DUE TO
|
|
C UNDERFLOW (GENERALLY ON KODE=2)
|
|
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 IS
|
|
C TOO LARGE OR CABS(Z) IS 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 FORMULA
|
|
C
|
|
C Y(FNU,Z)=0.5*(H(1,FNU,Z)-H(2,FNU,Z))/I
|
|
C
|
|
C WHERE I**2 = -1 AND THE HANKEL BESSEL FUNCTIONS H(1,FNU,Z)
|
|
C AND H(2,FNU,Z) ARE CALCULATED IN CBESH.
|
|
C
|
|
C FOR NEGATIVE ORDERS,THE FORMULA
|
|
C
|
|
C Y(-FNU,Z) = Y(FNU,Z)*COS(PI*FNU) + J(FNU,Z)*SIN(PI*FNU)
|
|
C
|
|
C CAN BE USED. HOWEVER,FOR LARGE ORDERS CLOSE TO HALF ODD
|
|
C INTEGERS THE FUNCTION CHANGES RADICALLY. WHEN FNU IS A LARGE
|
|
C POSITIVE HALF ODD INTEGER,THE MAGNITUDE OF Y(-FNU,Z)=J(FNU,Z)*
|
|
C SIN(PI*FNU) IS A LARGE NEGATIVE POWER OF TEN. BUT WHEN FNU IS
|
|
C NOT A HALF ODD INTEGER, Y(FNU,Z) DOMINATES IN MAGNITUDE WITH A
|
|
C LARGE POSITIVE POWER OF TEN AND THE MOST THAT THE SECOND TERM
|
|
C CAN BE REDUCED IS BY UNIT ROUNDOFF FROM THE COEFFICIENT. THUS,
|
|
C WIDE CHANGES CAN OCCUR WITHIN UNIT ROUNDOFF OF A LARGE HALF
|
|
C ODD INTEGER. HERE, LARGE MEANS FNU.GT.CABS(Z).
|
|
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=DMAX1(D1MACH(4),1.0D-18) IS
|
|
C DOUBLE PRECISION UNIT ROUNDOFF LIMITED TO 18 DIGITS PRECISION.
|
|
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 ZBESH,I1MACH,D1MACH
|
|
C***END PROLOGUE ZBESY
|
|
C
|
|
C COMPLEX CWRK,CY,C1,C2,EX,HCI,Z,ZU,ZV
|
|
DOUBLE PRECISION CWRKI, CWRKR, CYI, CYR, C1I, C1R, C2I, C2R,
|
|
* ELIM, EXI, EXR, EY, FNU, HCII, STI, STR, TAY, ZI, ZR, DEXP,
|
|
* D1MACH, ASCLE, RTOL, ATOL, AA, BB, TOL
|
|
INTEGER I, IERR, K, KODE, K1, K2, N, NZ, NZ1, NZ2, I1MACH
|
|
DIMENSION CYR(N), CYI(N), CWRKR(N), CWRKI(N)
|
|
C***FIRST EXECUTABLE STATEMENT ZBESY
|
|
IERR = 0
|
|
NZ=0
|
|
IF (ZR.EQ.0.0D0 .AND. ZI.EQ.0.0D0) IERR=1
|
|
IF (FNU.LT.0.0D0) IERR=1
|
|
IF (KODE.LT.1 .OR. KODE.GT.2) IERR=1
|
|
IF (N.LT.1) IERR=1
|
|
IF (IERR.NE.0) RETURN
|
|
HCII = 0.5D0
|
|
CALL ZBESH(ZR, ZI, FNU, KODE, 1, N, CYR, CYI, NZ1, IERR)
|
|
IF (IERR.NE.0.AND.IERR.NE.3) GO TO 170
|
|
CALL ZBESH(ZR, ZI, FNU, KODE, 2, N, CWRKR, CWRKI, NZ2, IERR)
|
|
IF (IERR.NE.0.AND.IERR.NE.3) GO TO 170
|
|
NZ = MIN0(NZ1,NZ2)
|
|
IF (KODE.EQ.2) GO TO 60
|
|
DO 50 I=1,N
|
|
STR = CWRKR(I) - CYR(I)
|
|
STI = CWRKI(I) - CYI(I)
|
|
CYR(I) = -STI*HCII
|
|
CYI(I) = STR*HCII
|
|
50 CONTINUE
|
|
RETURN
|
|
60 CONTINUE
|
|
TOL = DMAX1(D1MACH(4),1.0D-18)
|
|
K1 = I1MACH(15)
|
|
K2 = I1MACH(16)
|
|
K = MIN0(IABS(K1),IABS(K2))
|
|
R1M5 = D1MACH(5)
|
|
C-----------------------------------------------------------------------
|
|
C ELIM IS THE APPROXIMATE EXPONENTIAL UNDER- AND OVERFLOW LIMIT
|
|
C-----------------------------------------------------------------------
|
|
ELIM = 2.303D0*(DBLE(FLOAT(K))*R1M5-3.0D0)
|
|
EXR = DCOS(ZR)
|
|
EXI = DSIN(ZR)
|
|
EY = 0.0D0
|
|
TAY = DABS(ZI+ZI)
|
|
IF (TAY.LT.ELIM) EY = DEXP(-TAY)
|
|
IF (ZI.LT.0.0D0) GO TO 90
|
|
C1R = EXR*EY
|
|
C1I = EXI*EY
|
|
C2R = EXR
|
|
C2I = -EXI
|
|
70 CONTINUE
|
|
NZ = 0
|
|
RTOL = 1.0D0/TOL
|
|
ASCLE = D1MACH(1)*RTOL*1.0D+3
|
|
DO 80 I=1,N
|
|
C STR = C1R*CYR(I) - C1I*CYI(I)
|
|
C STI = C1R*CYI(I) + C1I*CYR(I)
|
|
C STR = -STR + C2R*CWRKR(I) - C2I*CWRKI(I)
|
|
C STI = -STI + C2R*CWRKI(I) + C2I*CWRKR(I)
|
|
C CYR(I) = -STI*HCII
|
|
C CYI(I) = STR*HCII
|
|
AA = CWRKR(I)
|
|
BB = CWRKI(I)
|
|
ATOL = 1.0D0
|
|
IF (DMAX1(DABS(AA),DABS(BB)).GT.ASCLE) GO TO 75
|
|
AA = AA*RTOL
|
|
BB = BB*RTOL
|
|
ATOL = TOL
|
|
75 CONTINUE
|
|
STR = (AA*C2R - BB*C2I)*ATOL
|
|
STI = (AA*C2I + BB*C2R)*ATOL
|
|
AA = CYR(I)
|
|
BB = CYI(I)
|
|
ATOL = 1.0D0
|
|
IF (DMAX1(DABS(AA),DABS(BB)).GT.ASCLE) GO TO 85
|
|
AA = AA*RTOL
|
|
BB = BB*RTOL
|
|
ATOL = TOL
|
|
85 CONTINUE
|
|
STR = STR - (AA*C1R - BB*C1I)*ATOL
|
|
STI = STI - (AA*C1I + BB*C1R)*ATOL
|
|
CYR(I) = -STI*HCII
|
|
CYI(I) = STR*HCII
|
|
IF (STR.EQ.0.0D0 .AND. STI.EQ.0.0D0 .AND. EY.EQ.0.0D0) NZ = NZ
|
|
* + 1
|
|
80 CONTINUE
|
|
RETURN
|
|
90 CONTINUE
|
|
C1R = EXR
|
|
C1I = EXI
|
|
C2R = EXR*EY
|
|
C2I = -EXI*EY
|
|
GO TO 70
|
|
170 CONTINUE
|
|
NZ = 0
|
|
RETURN
|
|
END
|