!--------------------------------------------------------------------------------------------------!
!   CP2K: A general program to perform molecular dynamics simulations                              !
!   Copyright (C) 2000 - 2018  CP2K developers group                                               !
!--------------------------------------------------------------------------------------------------!

! **************************************************************************************************
!> \brief Calculation of Coulomb integrals over Cartesian Gaussian-type functions
!>      (electron repulsion integrals, ERIs).
!> \par Literature
!>      S. Obara and A. Saika, J. Chem. Phys. 84, 3963 (1986)
!> \par History
!>      none
!> \par Parameters
!>       - ax,ay,az    : Angular momentum index numbers of orbital a.
!>       - bx,by,bz    : Angular momentum index numbers of orbital b.
!>       - cx,cy,cz    : Angular momentum index numbers of orbital c.
!>       - coset       : Cartesian orbital set pointer.
!>       - dab         : Distance between the atomic centers a and b.
!>       - dac         : Distance between the atomic centers a and c.
!>       - dbc         : Distance between the atomic centers b and c.
!>       - gccc        : Prefactor of the primitive Gaussian function c.
!>       - l{a,b,c}    : Angular momentum quantum number of shell a, b or c.
!>       - l{a,b,c}_max: Maximum angular momentum quantum number of shell a, b or c.
!>       - l{a,b,c}_min: Minimum angular momentum quantum number of shell a, b or c.
!>       - ncoset      : Number of orbitals in a Cartesian orbital set.
!>       - npgf{a,b}   : Degree of contraction of shell a or b.
!>       - rab         : Distance vector between the atomic centers a and b.
!>       - rab2        : Square of the distance between the atomic centers a and b.
!>       - rac         : Distance vector between the atomic centers a and c.
!>       - rac2        : Square of the distance between the atomic centers a and c.
!>       - rbc         : Distance vector between the atomic centers b and c.
!>       - rbc2        : Square of the distance between the atomic centers b and c.
!>       - rpgf{a,b,c} : Radius of the primitive Gaussian-type function a, b or c.
!>       - zet{a,b,c}  : Exponents of the Gaussian-type functions a, b or c.
!>       - zetp        : Reciprocal of the sum of the exponents of orbital a and b.
!>       - zetw        : Reciprocal of the sum of the exponents of orbital a, b and c.
!> \author Matthias Krack (22.08.2000)
! **************************************************************************************************
MODULE ai_coulomb

   USE gamma,                           ONLY: fgamma => fgamma_0
   USE kinds,                           ONLY: dp
   USE mathconstants,                   ONLY: pi
   USE orbital_pointers,                ONLY: coset,&
                                              ncoset
#include "../base/base_uses.f90"

   IMPLICIT NONE
   CHARACTER(len=*), PARAMETER, PRIVATE :: moduleN = 'ai_coulomb'
   PRIVATE

   ! *** Public subroutines ***

   PUBLIC :: coulomb2, coulomb2_new, coulomb3

CONTAINS

! **************************************************************************************************
!> \brief   Calculation of the primitive two-center Coulomb integrals over
!>          Cartesian Gaussian-type functions.
!> \param la_max ...
!> \param npgfa ...
!> \param zeta ...
!> \param rpgfa ...
!> \param la_min ...
!> \param lc_max ...
!> \param npgfc ...
!> \param zetc ...
!> \param rpgfc ...
!> \param lc_min ...
!> \param rac ...
!> \param rac2 ...
!> \param vac ...
!> \param v ...
!> \param f ...
!> \param maxder ...
!> \param vac_plus ...
!> \date    05.12.2000
!> \author  Matthias Krack
!> \version 1.0
! **************************************************************************************************
   SUBROUTINE coulomb2(la_max, npgfa, zeta, rpgfa, la_min, lc_max, npgfc, zetc, rpgfc, lc_min, &
                       rac, rac2, vac, v, f, maxder, vac_plus)
      INTEGER, INTENT(IN)                                :: la_max, npgfa
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zeta, rpgfa
      INTEGER, INTENT(IN)                                :: la_min, lc_max, npgfc
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zetc, rpgfc
      INTEGER, INTENT(IN)                                :: lc_min
      REAL(KIND=dp), DIMENSION(3), INTENT(IN)            :: rac
      REAL(KIND=dp), INTENT(IN)                          :: rac2
      REAL(KIND=dp), DIMENSION(:, :), INTENT(INOUT)      :: vac
      REAL(KIND=dp), DIMENSION(:, :, :)                  :: v
      REAL(KIND=dp), DIMENSION(0:)                       :: f
      INTEGER, INTENT(IN), OPTIONAL                      :: maxder
      REAL(KIND=dp), DIMENSION(:, :), OPTIONAL           :: vac_plus

      CHARACTER(len=*), PARAMETER :: routineN = 'coulomb2', routineP = moduleN//':'//routineN

      INTEGER                                            :: ax, ay, az, coc, cocx, cocy, cocz, cx, &
                                                            cy, cz, i, ipgf, j, jpgf, la, lc, &
                                                            maxder_local, n, na, nap, nc, nmax
      REAL(KIND=dp)                                      :: dac, f0, f1, f2, f3, f4, f5, f6, fcx, &
                                                            fcy, fcz, rho, t, zetp, zetq, zetw
      REAL(KIND=dp), DIMENSION(3)                        :: raw, rcw

      v = 0.0_dp

      maxder_local = 0
      IF (PRESENT(maxder)) THEN
         maxder_local = maxder
         vac_plus = 0.0_dp
      END IF

      nmax = la_max+lc_max+1

      ! *** Calculate the distance of the centers a and c ***

      dac = SQRT(rac2)

      ! *** Loop over all pairs of primitive Gaussian-type functions ***

      na = 0
      nap = 0

      DO ipgf = 1, npgfa

         nc = 0

         DO jpgf = 1, npgfc

            ! *** Screening ***

            IF (rpgfa(ipgf)+rpgfc(jpgf) < dac) THEN
               DO j = nc+ncoset(lc_min-1)+1, nc+ncoset(lc_max)
                  DO i = na+ncoset(la_min-1)+1, na+ncoset(la_max-maxder_local)
                     vac(i, j) = 0.0_dp
                  END DO
               END DO
               nc = nc+ncoset(lc_max)
               CYCLE
            END IF

            ! *** Calculate some prefactors ***

            zetp = 1.0_dp/zeta(ipgf)
            zetq = 1.0_dp/zetc(jpgf)
            zetw = 1.0_dp/(zeta(ipgf)+zetc(jpgf))

            rho = zeta(ipgf)*zetc(jpgf)*zetw

            f0 = 2.0_dp*SQRT(pi**5*zetw)*zetp*zetq

            ! *** Calculate the incomplete Gamma function ***

            t = rho*rac2

            CALL fgamma(nmax-1, t, f)

            ! *** Calculate the basic two-center Coulomb integrals [s||s]{n} ***

            DO n = 1, nmax
               v(1, 1, n) = f0*f(n-1)
            END DO

            ! *** Vertical recurrence steps: [s||s] -> [s||c] ***

            IF (lc_max > 0) THEN

               f1 = 0.5_dp*zetq
               f2 = -rho*zetq

               rcw(:) = -zeta(ipgf)*zetw*rac(:)

               ! *** [s||p]{n} = (Wi - Ci)*[s||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(1, 2, n) = rcw(1)*v(1, 1, n+1)
                  v(1, 3, n) = rcw(2)*v(1, 1, n+1)
                  v(1, 4, n) = rcw(3)*v(1, 1, n+1)
               END DO

               ! ** [s||c]{n} = (Wi - Ci)*[s||c-1i]{n+1} +     ***
               ! **             f1*Ni(c-1i)*(   [s||c-2i]{n} + ***
               ! **                          f2*[s||c-2i]{n+1} ***

               DO lc = 2, lc_max

                  DO n = 1, nmax-lc

                     ! **** Increase the angular momentum component z of c ***

                     v(1, coset(0, 0, lc), n) = &
                        rcw(3)*v(1, coset(0, 0, lc-1), n+1)+ &
                        f1*REAL(lc-1, dp)*(v(1, coset(0, 0, lc-2), n)+ &
                                           f2*v(1, coset(0, 0, lc-2), n+1))

                     ! *** Increase the angular momentum component y of c ***

                     cz = lc-1
                     v(1, coset(0, 1, cz), n) = rcw(2)*v(1, coset(0, 0, cz), n+1)

                     DO cy = 2, lc
                        cz = lc-cy
                        v(1, coset(0, cy, cz), n) = &
                           rcw(2)*v(1, coset(0, cy-1, cz), n+1)+ &
                           f1*REAL(cy-1, dp)*(v(1, coset(0, cy-2, cz), n)+ &
                                              f2*v(1, coset(0, cy-2, cz), n+1))
                     END DO

                     ! *** Increase the angular momentum component x of c ***

                     DO cy = 0, lc-1
                        cz = lc-1-cy
                        v(1, coset(1, cy, cz), n) = rcw(1)*v(1, coset(0, cy, cz), n+1)
                     END DO

                     DO cx = 2, lc
                        f6 = f1*REAL(cx-1, dp)
                        DO cy = 0, lc-cx
                           cz = lc-cx-cy
                           v(1, coset(cx, cy, cz), n) = &
                              rcw(1)*v(1, coset(cx-1, cy, cz), n+1)+ &
                              f6*(v(1, coset(cx-2, cy, cz), n)+ &
                                  f2*v(1, coset(cx-2, cy, cz), n+1))
                        END DO
                     END DO

                  END DO

               END DO

            END IF

            ! *** Vertical recurrence steps: [s||c] -> [a||c] ***

            IF (la_max > 0) THEN

               f3 = 0.5_dp*zetp
               f4 = -rho*zetp
               f5 = 0.5_dp*zetw

               raw(:) = zetc(jpgf)*zetw*rac(:)

               ! *** [p||s]{n} = (Wi - Ai)*[s||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(2, 1, n) = raw(1)*v(1, 1, n+1)
                  v(3, 1, n) = raw(2)*v(1, 1, n+1)
                  v(4, 1, n) = raw(3)*v(1, 1, n+1)
               END DO

               ! *** [a||s]{n} = (Wi - Ai)*[a-1i||s]{n+1} +      ***
               ! ***             f3*Ni(a-1i)*(   [a-2i||s]{n} +  ***
               ! ***                          f4*[a-2i||s]{n+1}) ***

               DO la = 2, la_max

                  DO n = 1, nmax-la

                     ! *** Increase the angular momentum component z of a ***

                     v(coset(0, 0, la), 1, n) = &
                        raw(3)*v(coset(0, 0, la-1), 1, n+1)+ &
                        f3*REAL(la-1, dp)*(v(coset(0, 0, la-2), 1, n)+ &
                                           f4*v(coset(0, 0, la-2), 1, n+1))

                     ! *** Increase the angular momentum component y of a ***

                     az = la-1
                     v(coset(0, 1, az), 1, n) = raw(2)*v(coset(0, 0, az), 1, n+1)

                     DO ay = 2, la
                        az = la-ay
                        v(coset(0, ay, az), 1, n) = &
                           raw(2)*v(coset(0, ay-1, az), 1, n+1)+ &
                           f3*REAL(ay-1, dp)*(v(coset(0, ay-2, az), 1, n)+ &
                                              f4*v(coset(0, ay-2, az), 1, n+1))
                     END DO

                     ! *** Increase the angular momentum component x of a ***

                     DO ay = 0, la-1
                        az = la-1-ay
                        v(coset(1, ay, az), 1, n) = raw(1)*v(coset(0, ay, az), 1, n+1)
                     END DO

                     DO ax = 2, la
                        f6 = f3*REAL(ax-1, dp)
                        DO ay = 0, la-ax
                           az = la-ax-ay
                           v(coset(ax, ay, az), 1, n) = &
                              raw(1)*v(coset(ax-1, ay, az), 1, n+1)+ &
                              f6*(v(coset(ax-2, ay, az), 1, n)+ &
                                  f4*v(coset(ax-2, ay, az), 1, n+1))
                        END DO
                     END DO

                  END DO

               END DO

               DO lc = 1, lc_max

                  DO cx = 0, lc
                     DO cy = 0, lc-cx
                        cz = lc-cx-cy

                        coc = coset(cx, cy, cz)
                        cocx = coset(MAX(0, cx-1), cy, cz)
                        cocy = coset(cx, MAX(0, cy-1), cz)
                        cocz = coset(cx, cy, MAX(0, cz-1))

                        fcx = f5*REAL(cx, dp)
                        fcy = f5*REAL(cy, dp)
                        fcz = f5*REAL(cz, dp)

                        ! *** [p||c]{n} = (Wi - Ai)*[s||c]{n+1} + ***
                        ! ***             f5*Ni(c)*[s||c-1i]{n+1} ***

                        DO n = 1, nmax-1-lc
                           v(2, coc, n) = raw(1)*v(1, coc, n+1)+fcx*v(1, cocx, n+1)
                           v(3, coc, n) = raw(2)*v(1, coc, n+1)+fcy*v(1, cocy, n+1)
                           v(4, coc, n) = raw(3)*v(1, coc, n+1)+fcz*v(1, cocz, n+1)
                        END DO

                        ! *** [a||c]{n} = (Wi - Ai)*[a-1i||c]{n+1} +        ***
                        ! ***             f3*Ni(a-1i)*(   [a-2i||c]{n} +    ***
                        ! ***                          f4*[a-2i||c]{n+1}) + ***
                        ! ***             f5*Ni(c)*[a-1i||c-1i]{n+1}        ***

                        DO la = 2, la_max

                           DO n = 1, nmax-la-lc

                              ! *** Increase the angular momentum component z of a ***

                              v(coset(0, 0, la), coc, n) = &
                                 raw(3)*v(coset(0, 0, la-1), coc, n+1)+ &
                                 f3*REAL(la-1, dp)*(v(coset(0, 0, la-2), coc, n)+ &
                                                    f4*v(coset(0, 0, la-2), coc, n+1))+ &
                                 fcz*v(coset(0, 0, la-1), cocz, n+1)

                              ! *** Increase the angular momentum component y of a ***

                              az = la-1
                              v(coset(0, 1, az), coc, n) = &
                                 raw(2)*v(coset(0, 0, az), coc, n+1)+ &
                                 fcy*v(coset(0, 0, az), cocy, n+1)

                              DO ay = 2, la
                                 az = la-ay
                                 v(coset(0, ay, az), coc, n) = &
                                    raw(2)*v(coset(0, ay-1, az), coc, n+1)+ &
                                    f3*REAL(ay-1, dp)*(v(coset(0, ay-2, az), coc, n)+ &
                                                       f4*v(coset(0, ay-2, az), coc, n+1))+ &
                                    fcy*v(coset(0, ay-1, az), cocy, n+1)
                              END DO

                              ! *** Increase the angular momentum component x of a ***

                              DO ay = 0, la-1
                                 az = la-1-ay
                                 v(coset(1, ay, az), coc, n) = &
                                    raw(1)*v(coset(0, ay, az), coc, n+1)+ &
                                    fcx*v(coset(0, ay, az), cocx, n+1)
                              END DO

                              DO ax = 2, la
                                 f6 = f3*REAL(ax-1, dp)
                                 DO ay = 0, la-ax
                                    az = la-ax-ay
                                    v(coset(ax, ay, az), coc, n) = &
                                       raw(1)*v(coset(ax-1, ay, az), coc, n+1)+ &
                                       f6*(v(coset(ax-2, ay, az), coc, n)+ &
                                           f4*v(coset(ax-2, ay, az), coc, n+1))+ &
                                       fcx*v(coset(ax-1, ay, az), cocx, n+1)
                                 END DO
                              END DO

                           END DO

                        END DO

                     END DO
                  END DO

               END DO

            END IF

            DO j = ncoset(lc_min-1)+1, ncoset(lc_max)
               DO i = ncoset(la_min-1)+1, ncoset(la_max-maxder_local)
                  vac(na+i, nc+j) = v(i, j, 1)
               END DO
            END DO

            IF (PRESENT(maxder)) THEN
               DO j = ncoset(lc_min-1)+1, ncoset(lc_max)
                  DO i = 1, ncoset(la_max)
                     vac_plus(nap+i, nc+j) = v(i, j, 1)
                  END DO
               END DO
            END IF

            nc = nc+ncoset(lc_max)

         END DO

         na = na+ncoset(la_max-maxder_local)
         nap = nap+ncoset(la_max)

      END DO

   END SUBROUTINE coulomb2
! **************************************************************************************************
!> \brief   Calculation of the primitive two-center Coulomb integrals over
!>          Cartesian Gaussian-type functions. Same as coulomb2 treats derivative
!>          different (now vac_plus is symmetric)
!> \param la_max ...
!> \param npgfa ...
!> \param zeta ...
!> \param la_min ...
!> \param lc_max ...
!> \param npgfc ...
!> \param zetc ...
!> \param lc_min ...
!> \param rac ...
!> \param rac2 ...
!> \param vac ...
!> \param v ...
!> \param f ...
!> \param maxder ...
!> \param vac_plus ...
!> \date    6.02.2008
!> \author  CJM
!> \version 1.0
! **************************************************************************************************

   SUBROUTINE coulomb2_new(la_max, npgfa, zeta, la_min, lc_max, npgfc, zetc, lc_min, &
                           rac, rac2, vac, v, f, maxder, vac_plus)
      INTEGER, INTENT(IN)                                :: la_max, npgfa
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zeta
      INTEGER, INTENT(IN)                                :: la_min, lc_max, npgfc
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zetc
      INTEGER, INTENT(IN)                                :: lc_min
      REAL(KIND=dp), DIMENSION(3), INTENT(IN)            :: rac
      REAL(KIND=dp), INTENT(IN)                          :: rac2
      REAL(KIND=dp), DIMENSION(:, :), INTENT(INOUT)      :: vac
      REAL(KIND=dp), DIMENSION(:, :, :)                  :: v
      REAL(KIND=dp), DIMENSION(0:)                       :: f
      INTEGER, INTENT(IN), OPTIONAL                      :: maxder
      REAL(KIND=dp), DIMENSION(:, :), OPTIONAL           :: vac_plus

      CHARACTER(len=*), PARAMETER :: routineN = 'coulomb2_new', routineP = moduleN//':'//routineN

      INTEGER                                            :: ax, ay, az, coc, cocx, cocy, cocz, cx, &
                                                            cy, cz, i, ipgf, j, jpgf, la, lc, &
                                                            maxder_local, n, na, nap, nc, ncp, nmax
      REAL(KIND=dp)                                      :: dac, f0, f1, f2, f3, f4, f5, f6, fcx, &
                                                            fcy, fcz, rho, t, zetp, zetq, zetw
      REAL(KIND=dp), DIMENSION(3)                        :: raw, rcw

      v = 0.0_dp

      maxder_local = 0
      IF (PRESENT(maxder)) THEN
         maxder_local = maxder
         vac_plus = 0.0_dp
      END IF

      nmax = la_max+lc_max+1

      ! *** Calculate the distance of the centers a and c ***

      dac = SQRT(rac2)

      ! *** Loop over all pairs of primitive Gaussian-type functions ***

      na = 0
      nap = 0

      DO ipgf = 1, npgfa

         nc = 0
         ncp = 0

         DO jpgf = 1, npgfc

            ! *** Calculate some prefactors ***

            zetp = 1.0_dp/zeta(ipgf)
            zetq = 1.0_dp/zetc(jpgf)
            zetw = 1.0_dp/(zeta(ipgf)+zetc(jpgf))

            rho = zeta(ipgf)*zetc(jpgf)*zetw

            f0 = 2.0_dp*SQRT(pi**5*zetw)*zetp*zetq

            ! *** Calculate the incomplete Gamma function ***

            t = rho*rac2

            CALL fgamma(nmax-1, t, f)

            ! *** Calculate the basic two-center Coulomb integrals [s||s]{n} ***

            DO n = 1, nmax
               v(1, 1, n) = f0*f(n-1)
            END DO

            ! *** Vertical recurrence steps: [s||s] -> [s||c] ***

            IF (lc_max > 0) THEN

               f1 = 0.5_dp*zetq
               f2 = -rho*zetq

               rcw(:) = -zeta(ipgf)*zetw*rac(:)

               ! *** [s||p]{n} = (Wi - Ci)*[s||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(1, 2, n) = rcw(1)*v(1, 1, n+1)
                  v(1, 3, n) = rcw(2)*v(1, 1, n+1)
                  v(1, 4, n) = rcw(3)*v(1, 1, n+1)
               END DO

               ! ** [s||c]{n} = (Wi - Ci)*[s||c-1i]{n+1} +     ***
               ! **             f1*Ni(c-1i)*(   [s||c-2i]{n} + ***
               ! **                          f2*[s||c-2i]{n+1} ***

               DO lc = 2, lc_max

                  DO n = 1, nmax-lc

                     ! **** Increase the angular momentum component z of c ***

                     v(1, coset(0, 0, lc), n) = &
                        rcw(3)*v(1, coset(0, 0, lc-1), n+1)+ &
                        f1*REAL(lc-1, dp)*(v(1, coset(0, 0, lc-2), n)+ &
                                           f2*v(1, coset(0, 0, lc-2), n+1))

                     ! *** Increase the angular momentum component y of c ***

                     cz = lc-1
                     v(1, coset(0, 1, cz), n) = rcw(2)*v(1, coset(0, 0, cz), n+1)

                     DO cy = 2, lc
                        cz = lc-cy
                        v(1, coset(0, cy, cz), n) = &
                           rcw(2)*v(1, coset(0, cy-1, cz), n+1)+ &
                           f1*REAL(cy-1, dp)*(v(1, coset(0, cy-2, cz), n)+ &
                                              f2*v(1, coset(0, cy-2, cz), n+1))
                     END DO

                     ! *** Increase the angular momentum component x of c ***

                     DO cy = 0, lc-1
                        cz = lc-1-cy
                        v(1, coset(1, cy, cz), n) = rcw(1)*v(1, coset(0, cy, cz), n+1)
                     END DO

                     DO cx = 2, lc
                        f6 = f1*REAL(cx-1, dp)
                        DO cy = 0, lc-cx
                           cz = lc-cx-cy
                           v(1, coset(cx, cy, cz), n) = &
                              rcw(1)*v(1, coset(cx-1, cy, cz), n+1)+ &
                              f6*(v(1, coset(cx-2, cy, cz), n)+ &
                                  f2*v(1, coset(cx-2, cy, cz), n+1))
                        END DO
                     END DO

                  END DO

               END DO

            END IF

            ! *** Vertical recurrence steps: [s||c] -> [a||c] ***

            IF (la_max > 0) THEN

               f3 = 0.5_dp*zetp
               f4 = -rho*zetp
               f5 = 0.5_dp*zetw

               raw(:) = zetc(jpgf)*zetw*rac(:)

               ! *** [p||s]{n} = (Wi - Ai)*[s||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(2, 1, n) = raw(1)*v(1, 1, n+1)
                  v(3, 1, n) = raw(2)*v(1, 1, n+1)
                  v(4, 1, n) = raw(3)*v(1, 1, n+1)
               END DO

               ! *** [a||s]{n} = (Wi - Ai)*[a-1i||s]{n+1} +      ***
               ! ***             f3*Ni(a-1i)*(   [a-2i||s]{n} +  ***
               ! ***                          f4*[a-2i||s]{n+1}) ***

               DO la = 2, la_max

                  DO n = 1, nmax-la

                     ! *** Increase the angular momentum component z of a ***

                     v(coset(0, 0, la), 1, n) = &
                        raw(3)*v(coset(0, 0, la-1), 1, n+1)+ &
                        f3*REAL(la-1, dp)*(v(coset(0, 0, la-2), 1, n)+ &
                                           f4*v(coset(0, 0, la-2), 1, n+1))

                     ! *** Increase the angular momentum component y of a ***

                     az = la-1
                     v(coset(0, 1, az), 1, n) = raw(2)*v(coset(0, 0, az), 1, n+1)

                     DO ay = 2, la
                        az = la-ay
                        v(coset(0, ay, az), 1, n) = &
                           raw(2)*v(coset(0, ay-1, az), 1, n+1)+ &
                           f3*REAL(ay-1, dp)*(v(coset(0, ay-2, az), 1, n)+ &
                                              f4*v(coset(0, ay-2, az), 1, n+1))
                     END DO

                     ! *** Increase the angular momentum component x of a ***

                     DO ay = 0, la-1
                        az = la-1-ay
                        v(coset(1, ay, az), 1, n) = raw(1)*v(coset(0, ay, az), 1, n+1)
                     END DO

                     DO ax = 2, la
                        f6 = f3*REAL(ax-1, dp)
                        DO ay = 0, la-ax
                           az = la-ax-ay
                           v(coset(ax, ay, az), 1, n) = &
                              raw(1)*v(coset(ax-1, ay, az), 1, n+1)+ &
                              f6*(v(coset(ax-2, ay, az), 1, n)+ &
                                  f4*v(coset(ax-2, ay, az), 1, n+1))
                        END DO
                     END DO

                  END DO

               END DO

               DO lc = 1, lc_max

                  DO cx = 0, lc
                     DO cy = 0, lc-cx
                        cz = lc-cx-cy

                        coc = coset(cx, cy, cz)
                        cocx = coset(MAX(0, cx-1), cy, cz)
                        cocy = coset(cx, MAX(0, cy-1), cz)
                        cocz = coset(cx, cy, MAX(0, cz-1))

                        fcx = f5*REAL(cx, dp)
                        fcy = f5*REAL(cy, dp)
                        fcz = f5*REAL(cz, dp)

                        ! *** [p||c]{n} = (Wi - Ai)*[s||c]{n+1} + ***
                        ! ***             f5*Ni(c)*[s||c-1i]{n+1} ***

                        DO n = 1, nmax-1-lc
                           v(2, coc, n) = raw(1)*v(1, coc, n+1)+fcx*v(1, cocx, n+1)
                           v(3, coc, n) = raw(2)*v(1, coc, n+1)+fcy*v(1, cocy, n+1)
                           v(4, coc, n) = raw(3)*v(1, coc, n+1)+fcz*v(1, cocz, n+1)
                        END DO

                        ! *** [a||c]{n} = (Wi - Ai)*[a-1i||c]{n+1} +        ***
                        ! ***             f3*Ni(a-1i)*(   [a-2i||c]{n} +    ***
                        ! ***                          f4*[a-2i||c]{n+1}) + ***
                        ! ***             f5*Ni(c)*[a-1i||c-1i]{n+1}        ***

                        DO la = 2, la_max

                           DO n = 1, nmax-la-lc

                              ! *** Increase the angular momentum component z of a ***

                              v(coset(0, 0, la), coc, n) = &
                                 raw(3)*v(coset(0, 0, la-1), coc, n+1)+ &
                                 f3*REAL(la-1, dp)*(v(coset(0, 0, la-2), coc, n)+ &
                                                    f4*v(coset(0, 0, la-2), coc, n+1))+ &
                                 fcz*v(coset(0, 0, la-1), cocz, n+1)

                              ! *** Increase the angular momentum component y of a ***

                              az = la-1
                              v(coset(0, 1, az), coc, n) = &
                                 raw(2)*v(coset(0, 0, az), coc, n+1)+ &
                                 fcy*v(coset(0, 0, az), cocy, n+1)

                              DO ay = 2, la
                                 az = la-ay
                                 v(coset(0, ay, az), coc, n) = &
                                    raw(2)*v(coset(0, ay-1, az), coc, n+1)+ &
                                    f3*REAL(ay-1, dp)*(v(coset(0, ay-2, az), coc, n)+ &
                                                       f4*v(coset(0, ay-2, az), coc, n+1))+ &
                                    fcy*v(coset(0, ay-1, az), cocy, n+1)
                              END DO

                              ! *** Increase the angular momentum component x of a ***

                              DO ay = 0, la-1
                                 az = la-1-ay
                                 v(coset(1, ay, az), coc, n) = &
                                    raw(1)*v(coset(0, ay, az), coc, n+1)+ &
                                    fcx*v(coset(0, ay, az), cocx, n+1)
                              END DO

                              DO ax = 2, la
                                 f6 = f3*REAL(ax-1, dp)
                                 DO ay = 0, la-ax
                                    az = la-ax-ay
                                    v(coset(ax, ay, az), coc, n) = &
                                       raw(1)*v(coset(ax-1, ay, az), coc, n+1)+ &
                                       f6*(v(coset(ax-2, ay, az), coc, n)+ &
                                           f4*v(coset(ax-2, ay, az), coc, n+1))+ &
                                       fcx*v(coset(ax-1, ay, az), cocx, n+1)
                                 END DO
                              END DO

                           END DO

                        END DO

                     END DO
                  END DO

               END DO

            END IF

            DO j = ncoset(lc_min-1)+1, ncoset(lc_max-maxder_local)
               DO i = ncoset(la_min-1)+1, ncoset(la_max-maxder_local)
                  vac(na+i, nc+j) = v(i, j, 1)
               END DO
            END DO

            IF (PRESENT(maxder)) THEN
               DO j = 1, ncoset(lc_max)
                  DO i = 1, ncoset(la_max)
                     vac_plus(nap+i, ncp+j) = v(i, j, 1)
                  END DO
               END DO
            END IF

            nc = nc+ncoset(lc_max-maxder_local)
            ncp = ncp+ncoset(lc_max)

         END DO

         na = na+ncoset(la_max-maxder_local)
         nap = nap+ncoset(la_max)

      END DO

   END SUBROUTINE coulomb2_new

! **************************************************************************************************
!> \brief   Calculation of the primitive three-center Coulomb integrals over
!>          Cartesian Gaussian-type functions (electron repulsion integrals,
!>          ERIs).
!> \param la_max ...
!> \param npgfa ...
!> \param zeta ...
!> \param rpgfa ...
!> \param la_min ...
!> \param lb_max ...
!> \param npgfb ...
!> \param zetb ...
!> \param rpgfb ...
!> \param lb_min ...
!> \param lc_max ...
!> \param zetc ...
!> \param rpgfc ...
!> \param lc_min ...
!> \param gccc ...
!> \param rab ...
!> \param rab2 ...
!> \param rac ...
!> \param rac2 ...
!> \param rbc2 ...
!> \param vabc ...
!> \param int_abc ...
!> \param v ...
!> \param f ...
!> \param maxder ...
!> \param vabc_plus ...
!> \date    06.11.2000
!> \author  Matthias Krack
!> \version 1.0
! **************************************************************************************************
   SUBROUTINE coulomb3(la_max, npgfa, zeta, rpgfa, la_min, lb_max, npgfb, zetb, rpgfb, lb_min, &
                       lc_max, zetc, rpgfc, lc_min, gccc, rab, rab2, rac, rac2, rbc2, vabc, int_abc, &
                       v, f, maxder, vabc_plus)
      INTEGER, INTENT(IN)                                :: la_max, npgfa
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zeta, rpgfa
      INTEGER, INTENT(IN)                                :: la_min, lb_max, npgfb
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: zetb, rpgfb
      INTEGER, INTENT(IN)                                :: lb_min, lc_max
      REAL(KIND=dp), INTENT(IN)                          :: zetc, rpgfc
      INTEGER, INTENT(IN)                                :: lc_min
      REAL(KIND=dp), DIMENSION(:), INTENT(IN)            :: gccc
      REAL(KIND=dp), DIMENSION(3), INTENT(IN)            :: rab
      REAL(KIND=dp), INTENT(IN)                          :: rab2
      REAL(KIND=dp), DIMENSION(3), INTENT(IN)            :: rac
      REAL(KIND=dp), INTENT(IN)                          :: rac2, rbc2
      REAL(KIND=dp), DIMENSION(:, :), INTENT(INOUT)      :: vabc
      REAL(KIND=dp), DIMENSION(:, :, :), INTENT(OUT)     :: int_abc
      REAL(KIND=dp), DIMENSION(:, :, :, :)               :: v
      REAL(KIND=dp), DIMENSION(0:)                       :: f
      INTEGER, INTENT(IN), OPTIONAL                      :: maxder
      REAL(KIND=dp), DIMENSION(:, :), OPTIONAL           :: vabc_plus

      CHARACTER(len=*), PARAMETER :: routineN = 'coulomb3', routineP = moduleN//':'//routineN

      INTEGER                                            :: ax, ay, az, bx, by, bz, coc, cocx, cocy, &
                                                            cocz, cx, cy, cz, i, ipgf, j, jpgf, k, &
                                                            kk, la, la_start, lb, lc, &
                                                            maxder_local, n, na, nap, nb, nmax
      REAL(KIND=dp)                                      :: dab, dac, dbc, f0, f1, f2, f3, f4, f5, &
                                                            f6, f7, fcx, fcy, fcz, fx, fy, fz, t, &
                                                            zetp, zetq, zetw
      REAL(KIND=dp), DIMENSION(3)                        :: rap, rbp, rcp, rcw, rpw

      v = 0.0_dp

      maxder_local = 0
      IF (PRESENT(maxder)) THEN
         maxder_local = maxder
      END IF

      nmax = la_max+lb_max+lc_max+1

      ! *** Calculate the distances of the centers a, b and c ***

      dab = SQRT(rab2)
      dac = SQRT(rac2)
      dbc = SQRT(rbc2)

      ! *** Initialize integrals array
      int_abc = 0.0_dp

      ! *** Loop over all pairs of primitive Gaussian-type functions ***

      na = 0
      nap = 0

      DO ipgf = 1, npgfa

         ! *** Screening ***
         IF (rpgfa(ipgf)+rpgfc < dac) THEN
            na = na+ncoset(la_max-maxder_local)
            nap = nap+ncoset(la_max)
            CYCLE
         END IF

         nb = 0

         DO jpgf = 1, npgfb

            ! *** Screening ***
            IF ( &
               (rpgfb(jpgf)+rpgfc < dbc) .OR. &
               (rpgfa(ipgf)+rpgfb(jpgf) < dab)) THEN
               nb = nb+ncoset(lb_max)
               CYCLE
            END IF

            ! *** Calculate some prefactors ***

            zetp = 1.0_dp/(zeta(ipgf)+zetb(jpgf))
            zetq = 1.0_dp/zetc
            zetw = 1.0_dp/(zeta(ipgf)+zetb(jpgf)+zetc)

            f0 = 2.0_dp*SQRT(pi**5*zetw)*zetp*zetq
            f1 = zetb(jpgf)*zetp
            f2 = 0.5_dp*zetp
            f4 = -zetc*zetw

            f0 = f0*EXP(-zeta(ipgf)*f1*rab2)

            rap(:) = f1*rab(:)
            rcp(:) = rap(:)-rac(:)
            rpw(:) = f4*rcp(:)

            ! *** Calculate the incomplete Gamma function ***

            t = -f4*(rcp(1)*rcp(1)+rcp(2)*rcp(2)+rcp(3)*rcp(3))/zetp

            CALL fgamma(nmax-1, t, f)

            ! *** Calculate the basic three-center Coulomb integrals [ss||s]{n} ***

            DO n = 1, nmax
               v(1, 1, 1, n) = f0*f(n-1)
            END DO

            ! *** Recurrence steps: [ss||s] -> [as||s] ***

            IF (la_max > 0) THEN

               ! *** Vertical recurrence steps: [ss||s] -> [as||s] ***

               ! *** [ps||s]{n} = (Pi - Ai)*[ss||s]{n} +              ***
               ! ***              (Wi - Pi)*[ss||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(2, 1, 1, n) = rap(1)*v(1, 1, 1, n)+rpw(1)*v(1, 1, 1, n+1)
                  v(3, 1, 1, n) = rap(2)*v(1, 1, 1, n)+rpw(2)*v(1, 1, 1, n+1)
                  v(4, 1, 1, n) = rap(3)*v(1, 1, 1, n)+rpw(3)*v(1, 1, 1, n+1)
               END DO

               ! *** [as||s]{n} = (Pi - Ai)*[(a-1i)s||s]{n} +        ***
               ! ***              (Wi - Pi)*[(a-1i)s||s]{n+1} +      ***
               ! ***              f2*Ni(a-1i)*(   [(a-2i)s||s]{n} +  ***
               ! ***                           f4*[(a-2i)s||s]{n+1}) ***

               DO la = 2, la_max

                  DO n = 1, nmax-la

                     ! *** Increase the angular momentum component z of a ***

                     v(coset(0, 0, la), 1, 1, n) = &
                        rap(3)*v(coset(0, 0, la-1), 1, 1, n)+ &
                        rpw(3)*v(coset(0, 0, la-1), 1, 1, n+1)+ &
                        f2*REAL(la-1, dp)*(v(coset(0, 0, la-2), 1, 1, n)+ &
                                           f4*v(coset(0, 0, la-2), 1, 1, n+1))

                     ! *** Increase the angular momentum component y of a ***

                     az = la-1
                     v(coset(0, 1, az), 1, 1, n) = &
                        rap(2)*v(coset(0, 0, az), 1, 1, n)+ &
                        rpw(2)*v(coset(0, 0, az), 1, 1, n+1)

                     DO ay = 2, la
                        az = la-ay
                        v(coset(0, ay, az), 1, 1, n) = &
                           rap(2)*v(coset(0, ay-1, az), 1, 1, n)+ &
                           rpw(2)*v(coset(0, ay-1, az), 1, 1, n+1)+ &
                           f2*REAL(ay-1, dp)*(v(coset(0, ay-2, az), 1, 1, n)+ &
                                              f4*v(coset(0, ay-2, az), 1, 1, n+1))
                     END DO

                     ! *** Increase the angular momentum component x of a ***

                     DO ay = 0, la-1
                        az = la-1-ay
                        v(coset(1, ay, az), 1, 1, n) = &
                           rap(1)*v(coset(0, ay, az), 1, 1, n)+ &
                           rpw(1)*v(coset(0, ay, az), 1, 1, n+1)
                     END DO

                     DO ax = 2, la
                        f3 = f2*REAL(ax-1, dp)
                        DO ay = 0, la-ax
                           az = la-ax-ay
                           v(coset(ax, ay, az), 1, 1, n) = &
                              rap(1)*v(coset(ax-1, ay, az), 1, 1, n)+ &
                              rpw(1)*v(coset(ax-1, ay, az), 1, 1, n+1)+ &
                              f3*(v(coset(ax-2, ay, az), 1, 1, n)+ &
                                  f4*v(coset(ax-2, ay, az), 1, 1, n+1))
                        END DO
                     END DO

                  END DO

               END DO

               ! *** Recurrence steps: [as||s] -> [ab||s] ***

               IF (lb_max > 0) THEN

                  ! *** Horizontal recurrence steps ***

                  rbp(:) = rap(:)-rab(:)

                  ! *** [ap||s]{n} = [(a+1i)s||s]{n} - (Bi - Ai)*[as||s]{n} ***

                  la_start = MAX(0, la_min-1)

                  DO la = la_start, la_max-1
                     DO n = 1, nmax-la-1
                        DO ax = 0, la
                           DO ay = 0, la-ax
                              az = la-ax-ay
                              v(coset(ax, ay, az), 2, 1, n) = &
                                 v(coset(ax+1, ay, az), 1, 1, n)- &
                                 rab(1)*v(coset(ax, ay, az), 1, 1, n)
                              v(coset(ax, ay, az), 3, 1, n) = &
                                 v(coset(ax, ay+1, az), 1, 1, n)- &
                                 rab(2)*v(coset(ax, ay, az), 1, 1, n)
                              v(coset(ax, ay, az), 4, 1, n) = &
                                 v(coset(ax, ay, az+1), 1, 1, n)- &
                                 rab(3)*v(coset(ax, ay, az), 1, 1, n)
                           END DO
                        END DO
                     END DO
                  END DO

                  ! *** Vertical recurrence step ***

                  ! *** [ap||s]{n} = (Pi - Bi)*[as||s]{n} +          ***
                  ! ***              (Wi - Pi)*[as||s]{n+1} +        ***
                  ! ***              f2*Ni(a)*(   [(a-1i)s||s]{n} +  ***
                  ! ***                        f4*[(a-1i)s||s]{n+1}) ***

                  DO n = 1, nmax-la_max-1
                     DO ax = 0, la_max
                        fx = f2*REAL(ax, dp)
                        DO ay = 0, la_max-ax
                           fy = f2*REAL(ay, dp)
                           az = la_max-ax-ay
                           fz = f2*REAL(az, dp)

                           IF (ax == 0) THEN
                              v(coset(ax, ay, az), 2, 1, n) = &
                                 rbp(1)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(1)*v(coset(ax, ay, az), 1, 1, n+1)
                           ELSE
                              v(coset(ax, ay, az), 2, 1, n) = &
                                 rbp(1)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(1)*v(coset(ax, ay, az), 1, 1, n+1)+ &
                                 fx*(v(coset(ax-1, ay, az), 1, 1, n)+ &
                                     f4*v(coset(ax-1, ay, az), 1, 1, n+1))
                           END IF

                           IF (ay == 0) THEN
                              v(coset(ax, ay, az), 3, 1, n) = &
                                 rbp(2)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(2)*v(coset(ax, ay, az), 1, 1, n+1)
                           ELSE
                              v(coset(ax, ay, az), 3, 1, n) = &
                                 rbp(2)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(2)*v(coset(ax, ay, az), 1, 1, n+1)+ &
                                 fy*(v(coset(ax, ay-1, az), 1, 1, n)+ &
                                     f4*v(coset(ax, ay-1, az), 1, 1, n+1))
                           END IF

                           IF (az == 0) THEN
                              v(coset(ax, ay, az), 4, 1, n) = &
                                 rbp(3)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(3)*v(coset(ax, ay, az), 1, 1, n+1)
                           ELSE
                              v(coset(ax, ay, az), 4, 1, n) = &
                                 rbp(3)*v(coset(ax, ay, az), 1, 1, n)+ &
                                 rpw(3)*v(coset(ax, ay, az), 1, 1, n+1)+ &
                                 fz*(v(coset(ax, ay, az-1), 1, 1, n)+ &
                                     f4*v(coset(ax, ay, az-1), 1, 1, n+1))
                           END IF

                        END DO
                     END DO
                  END DO

                  ! *** Recurrence steps: [ap||s] -> [ab||s] ***

                  DO lb = 2, lb_max

                     ! *** Horizontal recurrence steps ***

                     ! *** [ab||s]{n} = [(a+1i)(b-1i)||s]{n} -    ***
                     ! ***              (Bi - Ai)*[a(b-1i)||s]{n} ***

                     la_start = MAX(0, la_min-1)

                     DO la = la_start, la_max-1
                        DO n = 1, nmax-la-lb
                           DO ax = 0, la
                              DO ay = 0, la-ax
                                 az = la-ax-ay

                                 ! *** Shift of angular momentum component z from a to b ***

                                 v(coset(ax, ay, az), coset(0, 0, lb), 1, n) = &
                                    v(coset(ax, ay, az+1), coset(0, 0, lb-1), 1, n)- &
                                    rab(3)*v(coset(ax, ay, az), coset(0, 0, lb-1), 1, n)

                                 ! *** Shift of angular momentum component y from a to b ***

                                 DO by = 1, lb
                                    bz = lb-by
                                    v(coset(ax, ay, az), coset(0, by, bz), 1, n) = &
                                       v(coset(ax, ay+1, az), coset(0, by-1, bz), 1, n)- &
                                       rab(2)*v(coset(ax, ay, az), coset(0, by-1, bz), 1, n)
                                 END DO

                                 ! *** Shift of angular momentum component x from a to b ***

                                 DO bx = 1, lb
                                    DO by = 0, lb-bx
                                       bz = lb-bx-by
                                       v(coset(ax, ay, az), coset(bx, by, bz), 1, n) = &
                                          v(coset(ax+1, ay, az), coset(bx-1, by, bz), 1, n)- &
                                          rab(1)*v(coset(ax, ay, az), coset(bx-1, by, bz), 1, n)
                                    END DO
                                 END DO

                              END DO
                           END DO
                        END DO
                     END DO

                     ! *** Vertical recurrence step ***

                     ! *** [ab||s]{n} = (Pi - Bi)*[a(b-1i)||s]{n} +          ***
                     ! ***              (Wi - Pi)*[a(b-1i)||s]{n+1} +        ***
                     ! ***              f2*Ni(a)*(   [(a-1i)(b-1i)||s]{n} +  ***
                     ! ***                        f4*[(a-1i)(b-1i)||s]{n+1}) ***
                     ! ***              f2*Ni(b-1i)*(   [a(b-2i)||s]{n} +    ***
                     ! ***                           f4*[a(b-2i)||s]{n+1})   ***

                     DO n = 1, nmax-la_max-lb
                        DO ax = 0, la_max
                           fx = f2*REAL(ax, dp)
                           DO ay = 0, la_max-ax
                              fy = f2*REAL(ay, dp)
                              az = la_max-ax-ay
                              fz = f2*REAL(az, dp)

                              ! *** Shift of angular momentum component z from a to b ***

                              f3 = f2*REAL(lb-1, dp)

                              IF (az == 0) THEN
                                 v(coset(ax, ay, az), coset(0, 0, lb), 1, n) = &
                                    rbp(3)*v(coset(ax, ay, az), coset(0, 0, lb-1), 1, n)+ &
                                    rpw(3)*v(coset(ax, ay, az), coset(0, 0, lb-1), 1, n+1)+ &
                                    f3*(v(coset(ax, ay, az), coset(0, 0, lb-2), 1, n)+ &
                                        f4*v(coset(ax, ay, az), coset(0, 0, lb-2), 1, n+1))
                              ELSE
                                 v(coset(ax, ay, az), coset(0, 0, lb), 1, n) = &
                                    rbp(3)*v(coset(ax, ay, az), coset(0, 0, lb-1), 1, n)+ &
                                    rpw(3)*v(coset(ax, ay, az), coset(0, 0, lb-1), 1, n+1)+ &
                                    fz*(v(coset(ax, ay, az-1), coset(0, 0, lb-1), 1, n)+ &
                                        f4*v(coset(ax, ay, az-1), coset(0, 0, lb-1), 1, n+1))+ &
                                    f3*(v(coset(ax, ay, az), coset(0, 0, lb-2), 1, n)+ &
                                        f4*v(coset(ax, ay, az), coset(0, 0, lb-2), 1, n+1))
                              END IF

                              ! *** Shift of angular momentum component y from a to b ***

                              IF (ay == 0) THEN
                                 bz = lb-1
                                 v(coset(ax, ay, az), coset(0, 1, bz), 1, n) = &
                                    rbp(2)*v(coset(ax, ay, az), coset(0, 0, bz), 1, n)+ &
                                    rpw(2)*v(coset(ax, ay, az), coset(0, 0, bz), 1, n+1)
                                 DO by = 2, lb
                                    bz = lb-by
                                    f3 = f2*REAL(by-1, dp)
                                    v(coset(ax, ay, az), coset(0, by, bz), 1, n) = &
                                       rbp(2)*v(coset(ax, ay, az), coset(0, by-1, bz), 1, n)+ &
                                       rpw(2)*v(coset(ax, ay, az), coset(0, by-1, bz), 1, n+1)+ &
                                       f3*(v(coset(ax, ay, az), coset(0, by-2, bz), 1, n)+ &
                                           f4*v(coset(ax, ay, az), coset(0, by-2, bz), 1, n+1))
                                 END DO
                              ELSE
                                 bz = lb-1
                                 v(coset(ax, ay, az), coset(0, 1, bz), 1, n) = &
                                    rbp(2)*v(coset(ax, ay, az), coset(0, 0, bz), 1, n)+ &
                                    rpw(2)*v(coset(ax, ay, az), coset(0, 0, bz), 1, n+1)+ &
                                    fy*(v(coset(ax, ay-1, az), coset(0, 0, bz), 1, n)+ &
                                        f4*v(coset(ax, ay-1, az), coset(0, 0, bz), 1, n+1))
                                 DO by = 2, lb
                                    bz = lb-by
                                    f3 = f2*REAL(by-1, dp)
                                    v(coset(ax, ay, az), coset(0, by, bz), 1, n) = &
                                       rbp(2)*v(coset(ax, ay, az), coset(0, by-1, bz), 1, n)+ &
                                       rpw(2)*v(coset(ax, ay, az), coset(0, by-1, bz), 1, n+1)+ &
                                       fy*(v(coset(ax, ay-1, az), coset(0, by-1, bz), 1, n)+ &
                                           f4*v(coset(ax, ay-1, az), &
                                                coset(0, by-1, bz), 1, n+1))+ &
                                       f3*(v(coset(ax, ay, az), coset(0, by-2, bz), 1, n)+ &
                                           f4*v(coset(ax, ay, az), coset(0, by-2, bz), 1, n+1))
                                 END DO
                              END IF

                              ! *** Shift of angular momentum component x from a to b ***

                              IF (ax == 0) THEN
                                 DO by = 0, lb-1
                                    bz = lb-1-by
                                    v(coset(ax, ay, az), coset(1, by, bz), 1, n) = &
                                       rbp(1)*v(coset(ax, ay, az), coset(0, by, bz), 1, n)+ &
                                       rpw(1)*v(coset(ax, ay, az), coset(0, by, bz), 1, n+1)
                                 END DO
                                 DO bx = 2, lb
                                    f3 = f2*REAL(bx-1, dp)
                                    DO by = 0, lb-bx
                                       bz = lb-bx-by
                                       v(coset(ax, ay, az), coset(bx, by, bz), 1, n) = &
                                          rbp(1)*v(coset(ax, ay, az), coset(bx-1, by, bz), 1, n)+ &
                                          rpw(1)*v(coset(ax, ay, az), &
                                                   coset(bx-1, by, bz), 1, n+1)+ &
                                          f3*(v(coset(ax, ay, az), coset(bx-2, by, bz), 1, n)+ &
                                              f4*v(coset(ax, ay, az), coset(bx-2, by, bz), 1, n+1))
                                    END DO
                                 END DO
                              ELSE
                                 DO by = 0, lb-1
                                    bz = lb-1-by
                                    v(coset(ax, ay, az), coset(1, by, bz), 1, n) = &
                                       rbp(1)*v(coset(ax, ay, az), coset(0, by, bz), 1, n)+ &
                                       rpw(1)*v(coset(ax, ay, az), coset(0, by, bz), 1, n+1)+ &
                                       fx*(v(coset(ax-1, ay, az), coset(0, by, bz), 1, n)+ &
                                           f4*v(coset(ax-1, ay, az), coset(0, by, bz), 1, n+1))
                                 END DO
                                 DO bx = 2, lb
                                    f3 = f2*REAL(bx-1, dp)
                                    DO by = 0, lb-bx
                                       bz = lb-bx-by
                                       v(coset(ax, ay, az), coset(bx, by, bz), 1, n) = &
                                          rbp(1)*v(coset(ax, ay, az), coset(bx-1, by, bz), 1, n)+ &
                                          rpw(1)*v(coset(ax, ay, az), &
                                                   coset(bx-1, by, bz), 1, n+1)+ &
                                          fx*(v(coset(ax-1, ay, az), &
                                                coset(bx-1, by, bz), 1, n)+ &
                                              f4*v(coset(ax-1, ay, az), &
                                                   coset(bx-1, by, bz), 1, n+1))+ &
                                          f3*(v(coset(ax, ay, az), coset(bx-2, by, bz), 1, n)+ &
                                              f4*v(coset(ax, ay, az), coset(bx-2, by, bz), 1, n+1))
                                    END DO
                                 END DO
                              END IF

                           END DO
                        END DO
                     END DO

                  END DO

               END IF

            ELSE

               IF (lb_max > 0) THEN

                  ! *** Vertical recurrence steps: [ss||s] -> [sb||s] ***

                  rbp(:) = rap(:)-rab(:)

                  ! *** [sp||s]{n} = (Pi - Bi)*[ss||s]{n} + ***
                  ! ***              (Wi - Pi)*[ss||s]{n+1} ***

                  DO n = 1, nmax-1
                     v(1, 2, 1, n) = rbp(1)*v(1, 1, 1, n)+rpw(1)*v(1, 1, 1, n+1)
                     v(1, 3, 1, n) = rbp(2)*v(1, 1, 1, n)+rpw(2)*v(1, 1, 1, n+1)
                     v(1, 4, 1, n) = rbp(3)*v(1, 1, 1, n)+rpw(3)*v(1, 1, 1, n+1)
                  END DO

                  ! *** [sb||s]{n} = (Pi - Bi)*[s(b-1i)||s]{n} +        ***
                  ! ***              (Wi - Pi)*[s(b-1i)||s]{n+1} +      ***
                  ! ***              f2*Ni(b-1i)*(   [s(b-2i)||s]{n} +  ***
                  ! ***                           f4*[s(b-2i)||s]{n+1}) ***

                  DO lb = 2, lb_max

                     DO n = 1, nmax-lb

                        ! *** Increase the angular momentum component z of b ***

                        v(1, coset(0, 0, lb), 1, n) = &
                           rbp(3)*v(1, coset(0, 0, lb-1), 1, n)+ &
                           rpw(3)*v(1, coset(0, 0, lb-1), 1, n+1)+ &
                           f2*REAL(lb-1, dp)*(v(1, coset(0, 0, lb-2), 1, n)+ &
                                              f4*v(1, coset(0, 0, lb-2), 1, n+1))

                        ! *** Increase the angular momentum component y of b ***

                        bz = lb-1
                        v(1, coset(0, 1, bz), 1, n) = &
                           rbp(2)*v(1, coset(0, 0, bz), 1, n)+ &
                           rpw(2)*v(1, coset(0, 0, bz), 1, n+1)

                        DO by = 2, lb
                           bz = lb-by
                           v(1, coset(0, by, bz), 1, n) = &
                              rbp(2)*v(1, coset(0, by-1, bz), 1, n)+ &
                              rpw(2)*v(1, coset(0, by-1, bz), 1, n+1)+ &
                              f2*REAL(by-1, dp)*(v(1, coset(0, by-2, bz), 1, n)+ &
                                                 f4*v(1, coset(0, by-2, bz), 1, n+1))
                        END DO

                        ! *** Increase the angular momentum component x of b ***

                        DO by = 0, lb-1
                           bz = lb-1-by
                           v(1, coset(1, by, bz), 1, n) = &
                              rbp(1)*v(1, coset(0, by, bz), 1, n)+ &
                              rpw(1)*v(1, coset(0, by, bz), 1, n+1)
                        END DO

                        DO bx = 2, lb
                           f3 = f2*REAL(bx-1, dp)
                           DO by = 0, lb-bx
                              bz = lb-bx-by
                              v(1, coset(bx, by, bz), 1, n) = &
                                 rbp(1)*v(1, coset(bx-1, by, bz), 1, n)+ &
                                 rpw(1)*v(1, coset(bx-1, by, bz), 1, n+1)+ &
                                 f3*(v(1, coset(bx-2, by, bz), 1, n)+ &
                                     f4*v(1, coset(bx-2, by, bz), 1, n+1))
                           END DO
                        END DO

                     END DO

                  END DO

               END IF

            END IF

            ! *** Recurrence steps: [ab||s] -> [ab||c] ***

            IF (lc_max > 0) THEN

               ! *** Vertical recurrence steps: [ss||s] -> [ss||c] ***

               f5 = -zetw/zetp
               f6 = 0.5_dp*zetw
               f7 = 0.5_dp*zetq

               rcw(:) = rcp(:)+rpw(:)

               ! *** [ss||p]{n} = (Wi - Ci)*[ss||s]{n+1}  (i = x,y,z) ***

               DO n = 1, nmax-1
                  v(1, 1, 2, n) = rcw(1)*v(1, 1, 1, n+1)
                  v(1, 1, 3, n) = rcw(2)*v(1, 1, 1, n+1)
                  v(1, 1, 4, n) = rcw(3)*v(1, 1, 1, n+1)
               END DO

               ! *** [ss||c]{n} = (Wi - Ci)*[ss||c-1i]{n+1} + ***
               ! ***              f7*Ni(c-1i)*[ss||c-2i]{n} + ***
               ! ***              f5*[ss||c-2i]{n+1}          ***

               DO lc = 2, lc_max

                  DO n = 1, nmax-lc

                     ! *** Increase the angular momentum component z of c ***

                     v(1, 1, coset(0, 0, lc), n) = &
                        rcw(3)*v(1, 1, coset(0, 0, lc-1), n+1)+ &
                        f7*REAL(lc-1, dp)*(v(1, 1, coset(0, 0, lc-2), n)+ &
                                           f5*v(1, 1, coset(0, 0, lc-2), n+1))

                     ! *** Increase the angular momentum component y of c ***

                     cz = lc-1
                     v(1, 1, coset(0, 1, cz), n) = rcw(2)*v(1, 1, coset(0, 0, cz), n+1)

                     DO cy = 2, lc
                        cz = lc-cy
                        v(1, 1, coset(0, cy, cz), n) = &
                           rcw(2)*v(1, 1, coset(0, cy-1, cz), n+1)+ &
                           f7*REAL(cy-1, dp)*(v(1, 1, coset(0, cy-2, cz), n)+ &
                                              f5*v(1, 1, coset(0, cy-2, cz), n+1))
                     END DO

                     ! *** Increase the angular momentum component x of c ***

                     DO cy = 0, lc-1
                        cz = lc-1-cy
                        v(1, 1, coset(1, cy, cz), n) = rcw(1)*v(1, 1, coset(0, cy, cz), n+1)
                     END DO

                     DO cx = 2, lc
                        DO cy = 0, lc-cx
                           cz = lc-cx-cy
                           v(1, 1, coset(cx, cy, cz), n) = &
                              rcw(1)*v(1, 1, coset(cx-1, cy, cz), n+1)+ &
                              f7*REAL(cx-1, dp)*(v(1, 1, coset(cx-2, cy, cz), n)+ &
                                                 f5*v(1, 1, coset(cx-2, cy, cz), n+1))
                        END DO
                     END DO

                  END DO

               END DO

               ! *** Recurrence steps: [ss||c] -> [ab||c] ***

               DO lc = 1, lc_max

                  DO cx = 0, lc
                     DO cy = 0, lc-cx
                        cz = lc-cx-cy

                        coc = coset(cx, cy, cz)
                        cocx = coset(MAX(0, cx-1), cy, cz)
                        cocy = coset(cx, MAX(0, cy-1), cz)
                        cocz = coset(cx, cy, MAX(0, cz-1))

                        fcx = f6*REAL(cx, dp)
                        fcy = f6*REAL(cy, dp)
                        fcz = f6*REAL(cz, dp)

                        ! *** Recurrence steps: [ss||c] -> [as||c] ***

                        IF (la_max > 0) THEN

                           ! *** Vertical recurrence steps: [ss||c] -> [as||c] ***

                           ! *** [ps||c]{n} = (Pi - Ai)*[ss||c]{n} +                ***
                           ! ***              (Wi - Pi)*[ss||c]{n+1} +              ***
                           ! ***              f6*Ni(c)*[ss||c-1i]{n+1}  (i = x,y,z) ***

                           DO n = 1, nmax-1-lc
                              v(2, 1, coc, n) = rap(1)*v(1, 1, coc, n)+ &
                                                rpw(1)*v(1, 1, coc, n+1)+ &
                                                fcx*v(1, 1, cocx, n+1)
                              v(3, 1, coc, n) = rap(2)*v(1, 1, coc, n)+ &
                                                rpw(2)*v(1, 1, coc, n+1)+ &
                                                fcy*v(1, 1, cocy, n+1)
                              v(4, 1, coc, n) = rap(3)*v(1, 1, coc, n)+ &
                                                rpw(3)*v(1, 1, coc, n+1)+ &
                                                fcz*v(1, 1, cocz, n+1)
                           END DO

                           ! *** [as||c]{n} = (Pi - Ai)*[(a-1i)s||c]{n} +          ***
                           ! ***              (Wi - Pi)*[(a-1i)s||c]{n+1} +        ***
                           ! ***              f2*Ni(a-1i)*(   [(a-2i)s||c]{n} +    ***
                           ! ***                           f4*[(a-2i)s||c]{n+1}) + ***
                           ! ***              f6*Ni(c)*[(a-1i)s||c-1i]{n+1}        ***

                           DO la = 2, la_max

                              DO n = 1, nmax-la-lc

                                 ! *** Increase the angular momentum component z of a ***

                                 v(coset(0, 0, la), 1, coc, n) = &
                                    rap(3)*v(coset(0, 0, la-1), 1, coc, n)+ &
                                    rpw(3)*v(coset(0, 0, la-1), 1, coc, n+1)+ &
                                    f2*REAL(la-1, dp)*(v(coset(0, 0, la-2), 1, coc, n)+ &
                                                       f4*v(coset(0, 0, la-2), 1, coc, n+1))+ &
                                    fcz*v(coset(0, 0, la-1), 1, cocz, n+1)

                                 ! *** Increase the angular momentum component y of a ***

                                 az = la-1
                                 v(coset(0, 1, az), 1, coc, n) = &
                                    rap(2)*v(coset(0, 0, az), 1, coc, n)+ &
                                    rpw(2)*v(coset(0, 0, az), 1, coc, n+1)+ &
                                    fcy*v(coset(0, 0, az), 1, cocy, n+1)

                                 DO ay = 2, la
                                    f3 = f2*REAL(ay-1, dp)
                                    az = la-ay
                                    v(coset(0, ay, az), 1, coc, n) = &
                                       rap(2)*v(coset(0, ay-1, az), 1, coc, n)+ &
                                       rpw(2)*v(coset(0, ay-1, az), 1, coc, n+1)+ &
                                       f3*(v(coset(0, ay-2, az), 1, coc, n)+ &
                                           f4*v(coset(0, ay-2, az), 1, coc, n+1))+ &
                                       fcy*v(coset(0, ay-1, az), 1, cocy, n+1)
                                 END DO

                                 ! *** Increase the angular momentum component x of a ***

                                 DO ay = 0, la-1
                                    az = la-1-ay
                                    v(coset(1, ay, az), 1, coc, n) = &
                                       rap(1)*v(coset(0, ay, az), 1, coc, n)+ &
                                       rpw(1)*v(coset(0, ay, az), 1, coc, n+1)+ &
                                       fcx*v(coset(0, ay, az), 1, cocx, n+1)
                                 END DO

                                 DO ax = 2, la
                                    f3 = f2*REAL(ax-1, dp)
                                    DO ay = 0, la-ax
                                       az = la-ax-ay
                                       v(coset(ax, ay, az), 1, coc, n) = &
                                          rap(1)*v(coset(ax-1, ay, az), 1, coc, n)+ &
                                          rpw(1)*v(coset(ax-1, ay, az), 1, coc, n+1)+ &
                                          f3*(v(coset(ax-2, ay, az), 1, coc, n)+ &
                                              f4*v(coset(ax-2, ay, az), 1, coc, n+1))+ &
                                          fcx*v(coset(ax-1, ay, az), 1, cocx, n+1)
                                    END DO
                                 END DO

                              END DO

                           END DO

                           ! *** Recurrence steps: [as||c] -> [ab||c] ***

                           IF (lb_max > 0) THEN

                              ! *** Horizontal recurrence steps ***

                              ! *** [ap||c]{n} = [(a+1i)s||c]{n} - (Bi - Ai)*[as||c]{n} ***

                              la_start = MAX(0, la_min-1)

                              DO la = la_start, la_max-1
                                 DO n = 1, nmax-la-1-lc
                                    DO ax = 0, la
                                       DO ay = 0, la-ax
                                          az = la-ax-ay
                                          v(coset(ax, ay, az), 2, coc, n) = &
                                             v(coset(ax+1, ay, az), 1, coc, n)- &
                                             rab(1)*v(coset(ax, ay, az), 1, coc, n)
                                          v(coset(ax, ay, az), 3, coc, n) = &
                                             v(coset(ax, ay+1, az), 1, coc, n)- &
                                             rab(2)*v(coset(ax, ay, az), 1, coc, n)
                                          v(coset(ax, ay, az), 4, coc, n) = &
                                             v(coset(ax, ay, az+1), 1, coc, n)- &
                                             rab(3)*v(coset(ax, ay, az), 1, coc, n)
                                       END DO
                                    END DO
                                 END DO
                              END DO

                              ! *** Vertical recurrence step ***

                              ! *** [ap||c]{n} = (Pi - Bi)*[as||c]{n} +            ***
                              ! ***              (Wi - Pi)*[as||c]{n+1} +          ***
                              ! ***              f2*Ni(a)*(   [(a-1i)s||c]{n} +    ***
                              ! ***                        f4*[(a-1i)s||c]{n+1}) + ***
                              ! ***              f6*Ni(c)*[(as||c-1i]{n+1})        ***

                              DO n = 1, nmax-la_max-1-lc
                                 DO ax = 0, la_max
                                    fx = f2*REAL(ax, dp)
                                    DO ay = 0, la_max-ax
                                       fy = f2*REAL(ay, dp)
                                       az = la_max-ax-ay
                                       fz = f2*REAL(az, dp)

                                       IF (ax == 0) THEN
                                          v(coset(ax, ay, az), 2, coc, n) = &
                                             rbp(1)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(1)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fcx*v(coset(ax, ay, az), 1, cocx, n+1)
                                       ELSE
                                          v(coset(ax, ay, az), 2, coc, n) = &
                                             rbp(1)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(1)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fx*(v(coset(ax-1, ay, az), 1, coc, n)+ &
                                                 f4*v(coset(ax-1, ay, az), 1, coc, n+1))+ &
                                             fcx*v(coset(ax, ay, az), 1, cocx, n+1)
                                       END IF

                                       IF (ay == 0) THEN
                                          v(coset(ax, ay, az), 3, coc, n) = &
                                             rbp(2)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(2)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fcy*v(coset(ax, ay, az), 1, cocy, n+1)
                                       ELSE
                                          v(coset(ax, ay, az), 3, coc, n) = &
                                             rbp(2)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(2)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fy*(v(coset(ax, ay-1, az), 1, coc, n)+ &
                                                 f4*v(coset(ax, ay-1, az), 1, coc, n+1))+ &
                                             fcy*v(coset(ax, ay, az), 1, cocy, n+1)
                                       END IF

                                       IF (az == 0) THEN
                                          v(coset(ax, ay, az), 4, coc, n) = &
                                             rbp(3)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(3)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fcz*v(coset(ax, ay, az), 1, cocz, n+1)
                                       ELSE
                                          v(coset(ax, ay, az), 4, coc, n) = &
                                             rbp(3)*v(coset(ax, ay, az), 1, coc, n)+ &
                                             rpw(3)*v(coset(ax, ay, az), 1, coc, n+1)+ &
                                             fz*(v(coset(ax, ay, az-1), 1, coc, n)+ &
                                                 f4*v(coset(ax, ay, az-1), 1, coc, n+1))+ &
                                             fcz*v(coset(ax, ay, az), 1, cocz, n+1)
                                       END IF

                                    END DO
                                 END DO
                              END DO

                              ! *** Recurrence steps: [ap||c] -> [ab||c] ***

                              DO lb = 2, lb_max

                                 ! *** Horizontal recurrence steps ***

                                 ! *** [ab||c]{n} = [(a+1i)(b-1i)||c]{n} -    ***
                                 ! ***              (Bi - Ai)*[a(b-1i)||c]{n} ***

                                 la_start = MAX(0, la_min-1)

                                 DO la = la_start, la_max-1
                                    DO n = 1, nmax-la-lb-lc
                                       DO ax = 0, la
                                          DO ay = 0, la-ax
                                             az = la-ax-ay

                                             ! *** Shift of angular momentum component z ***

                                             v(coset(ax, ay, az), coset(0, 0, lb), coc, n) = &
                                                v(coset(ax, ay, az+1), &
                                                  coset(0, 0, lb-1), coc, n)- &
                                                rab(3)*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-1), coc, n)

                                             ! *** Shift of angular momentum component y ***

                                             DO by = 1, lb
                                                bz = lb-by
                                                v(coset(ax, ay, az), coset(0, by, bz), coc, n) = &
                                                   v(coset(ax, ay+1, az), &
                                                     coset(0, by-1, bz), coc, n)- &
                                                   rab(2)*v(coset(ax, ay, az), &
                                                            coset(0, by-1, bz), coc, n)
                                             END DO

                                             ! *** Shift of angular momentum component x ***

                                             DO bx = 1, lb
                                                DO by = 0, lb-bx
                                                   bz = lb-bx-by
                                                   v(coset(ax, ay, az), coset(bx, by, bz), coc, n) = &
                                                      v(coset(ax+1, ay, az), &
                                                        coset(bx-1, by, bz), coc, n)- &
                                                      rab(1)*v(coset(ax, ay, az), &
                                                               coset(bx-1, by, bz), coc, n)
                                                END DO
                                             END DO

                                          END DO
                                       END DO
                                    END DO
                                 END DO

                                 ! *** Vertical recurrence step ***

                                 ! *** [ab||c]{n} = (Pi - Bi)*[a(b-1i)||c]{n} +          ***
                                 ! ***              (Wi - Pi)*[a(b-1i)||c]{n+1} +        ***
                                 ! ***              f2*Ni(a)*(   [(a-1i)(b-1i)||c]{n} +  ***
                                 ! ***                        f4*[(a-1i)(b-1i)||c]{n+1}) ***
                                 ! ***              f2*Ni(b-1i)*(   [a(b-2i)||c]{n} +    ***
                                 ! ***                           f4*[a(b-2i)||c]{n+1}) + ***
                                 ! ***              f6*Ni(c)*[a(b-1i)||c-1i]{n+1})       ***

                                 DO n = 1, nmax-la_max-lb-lc
                                    DO ax = 0, la_max
                                       fx = f2*REAL(ax, dp)
                                       DO ay = 0, la_max-ax
                                          fy = f2*REAL(ay, dp)
                                          az = la_max-ax-ay
                                          fz = f2*REAL(az, dp)

                                          ! *** Shift of angular momentum component z from a to b ***

                                          f3 = f2*REAL(lb-1, dp)

                                          IF (az == 0) THEN
                                             v(coset(ax, ay, az), coset(0, 0, lb), coc, n) = &
                                                rbp(3)*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-1), coc, n)+ &
                                                rpw(3)*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-1), coc, n+1)+ &
                                                f3*(v(coset(ax, ay, az), &
                                                      coset(0, 0, lb-2), coc, n)+ &
                                                    f4*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-2), coc, n+1))+ &
                                                fcz*v(coset(ax, ay, az), &
                                                      coset(0, 0, lb-1), cocz, n+1)
                                          ELSE
                                             v(coset(ax, ay, az), coset(0, 0, lb), coc, n) = &
                                                rbp(3)*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-1), coc, n)+ &
                                                rpw(3)*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-1), coc, n+1)+ &
                                                fz*(v(coset(ax, ay, az-1), &
                                                      coset(0, 0, lb-1), coc, n)+ &
                                                    f4*v(coset(ax, ay, az-1), &
                                                         coset(0, 0, lb-1), coc, n+1))+ &
                                                f3*(v(coset(ax, ay, az), &
                                                      coset(0, 0, lb-2), coc, n)+ &
                                                    f4*v(coset(ax, ay, az), &
                                                         coset(0, 0, lb-2), coc, n+1))+ &
                                                fcz*v(coset(ax, ay, az), &
                                                      coset(0, 0, lb-1), cocz, n+1)
                                          END IF

                                          ! *** Shift of angular momentum component y from a to b ***

                                          IF (ay == 0) THEN
                                             bz = lb-1
                                             v(coset(ax, ay, az), coset(0, 1, bz), coc, n) = &
                                                rbp(2)*v(coset(ax, ay, az), &
                                                         coset(0, 0, bz), coc, n)+ &
                                                rpw(2)*v(coset(ax, ay, az), &
                                                         coset(0, 0, bz), coc, n+1)+ &
                                                fcy*v(coset(ax, ay, az), &
                                                      coset(0, 0, bz), cocy, n+1)
                                             DO by = 2, lb
                                                bz = lb-by
                                                f3 = f2*REAL(by-1, dp)
                                                v(coset(ax, ay, az), coset(0, by, bz), coc, n) = &
                                                   rbp(2)*v(coset(ax, ay, az), &
                                                            coset(0, by-1, bz), coc, n)+ &
                                                   rpw(2)*v(coset(ax, ay, az), &
                                                            coset(0, by-1, bz), coc, n+1)+ &
                                                   f3*(v(coset(ax, ay, az), &
                                                         coset(0, by-2, bz), coc, n)+ &
                                                       f4*v(coset(ax, ay, az), &
                                                            coset(0, by-2, bz), coc, n+1))+ &
                                                   fcy*v(coset(ax, ay, az), &
                                                         coset(0, by-1, bz), cocy, n+1)
                                             END DO
                                          ELSE
                                             bz = lb-1
                                             v(coset(ax, ay, az), coset(0, 1, bz), coc, n) = &
                                                rbp(2)*v(coset(ax, ay, az), &
                                                         coset(0, 0, bz), coc, n)+ &
                                                rpw(2)*v(coset(ax, ay, az), &
                                                         coset(0, 0, bz), coc, n+1)+ &
                                                fy*(v(coset(ax, ay-1, az), &
                                                      coset(0, 0, bz), coc, n)+ &
                                                    f4*v(coset(ax, ay-1, az), &
                                                         coset(0, 0, bz), coc, n+1))+ &
                                                fcy*v(coset(ax, ay, az), &
                                                      coset(0, 0, bz), cocy, n+1)
                                             DO by = 2, lb
                                                bz = lb-by
                                                f3 = f2*REAL(by-1, dp)
                                                v(coset(ax, ay, az), coset(0, by, bz), coc, n) = &
                                                   rbp(2)*v(coset(ax, ay, az), &
                                                            coset(0, by-1, bz), coc, n)+ &
                                                   rpw(2)*v(coset(ax, ay, az), &
                                                            coset(0, by-1, bz), coc, n+1)+ &
                                                   fy*(v(coset(ax, ay-1, az), &
                                                         coset(0, by-1, bz), coc, n)+ &
                                                       f4*v(coset(ax, ay-1, az), &
                                                            coset(0, by-1, bz), coc, n+1))+ &
                                                   f3*(v(coset(ax, ay, az), &
                                                         coset(0, by-2, bz), coc, n)+ &
                                                       f4*v(coset(ax, ay, az), &
                                                            coset(0, by-2, bz), coc, n+1))+ &
                                                   fcy*v(coset(ax, ay, az), &
                                                         coset(0, by-1, bz), cocy, n+1)
                                             END DO
                                          END IF

                                          ! *** Shift of angular momentum component x from a to b ***

                                          IF (ax == 0) THEN
                                             DO by = 0, lb-1
                                                bz = lb-1-by
                                                v(coset(ax, ay, az), coset(1, by, bz), coc, n) = &
                                                   rbp(1)*v(coset(ax, ay, az), &
                                                            coset(0, by, bz), coc, n)+ &
                                                   rpw(1)*v(coset(ax, ay, az), &
                                                            coset(0, by, bz), coc, n+1)+ &
                                                   fcx*v(coset(ax, ay, az), &
                                                         coset(0, by, bz), cocx, n+1)
                                             END DO
                                             DO bx = 2, lb
                                                f3 = f2*REAL(bx-1, dp)
                                                DO by = 0, lb-bx
                                                   bz = lb-bx-by
                                                   v(coset(ax, ay, az), coset(bx, by, bz), coc, n) = &
                                                      rbp(1)*v(coset(ax, ay, az), &
                                                               coset(bx-1, by, bz), coc, n)+ &
                                                      rpw(1)*v(coset(ax, ay, az), &
                                                               coset(bx-1, by, bz), coc, n+1)+ &
                                                      f3*(v(coset(ax, ay, az), &
                                                            coset(bx-2, by, bz), coc, n)+ &
                                                          f4*v(coset(ax, ay, az), &
                                                               coset(bx-2, by, bz), coc, n+1))+ &
                                                      fcx*v(coset(ax, ay, az), &
                                                            coset(bx-1, by, bz), cocx, n+1)
                                                END DO
                                             END DO
                                          ELSE
                                             DO by = 0, lb-1
                                                bz = lb-1-by
                                                v(coset(ax, ay, az), coset(1, by, bz), coc, n) = &
                                                   rbp(1)*v(coset(ax, ay, az), &
                                                            coset(0, by, bz), coc, n)+ &
                                                   rpw(1)*v(coset(ax, ay, az), &
                                                            coset(0, by, bz), coc, n+1)+ &
                                                   fx*(v(coset(ax-1, ay, az), &
                                                         coset(0, by, bz), coc, n)+ &
                                                       f4*v(coset(ax-1, ay, az), &
                                                            coset(0, by, bz), coc, n+1))+ &
                                                   fcx*v(coset(ax, ay, az), &
                                                         coset(0, by, bz), cocx, n+1)
                                             END DO
                                             DO bx = 2, lb
                                                f3 = f2*REAL(bx-1, dp)
                                                DO by = 0, lb-bx
                                                   bz = lb-bx-by
                                                   v(coset(ax, ay, az), coset(bx, by, bz), coc, n) = &
                                                      rbp(1)*v(coset(ax, ay, az), &
                                                               coset(bx-1, by, bz), coc, n)+ &
                                                      rpw(1)*v(coset(ax, ay, az), &
                                                               coset(bx-1, by, bz), coc, n+1)+ &
                                                      fx*(v(coset(ax-1, ay, az), &
                                                            coset(bx-1, by, bz), coc, n)+ &
                                                          f4*v(coset(ax-1, ay, az), &
                                                               coset(bx-1, by, bz), coc, n+1))+ &
                                                      f3*(v(coset(ax, ay, az), &
                                                            coset(bx-2, by, bz), coc, n)+ &
                                                          f4*v(coset(ax, ay, az), &
                                                               coset(bx-2, by, bz), coc, n+1))+ &
                                                      fcx*v(coset(ax, ay, az), &
                                                            coset(bx-1, by, bz), cocx, n+1)
                                                END DO
                                             END DO
                                          END IF

                                       END DO
                                    END DO
                                 END DO

                              END DO
                           END IF

                        ELSE

                           IF (lb_max > 0) THEN

                              ! *** Vertical recurrence steps: [ss||c] -> [sb||c] ***

                              ! *** [sp||c]{n} = (Pi - Bi)*[ss||c]{n} +    ***
                              ! ***              (Wi - Pi)*[ss||c]{n+1} +  ***
                              ! ***              f6*Ni(c)**[ss||c-1i]{n+1} ***

                              DO n = 1, nmax-1-lc
                                 v(1, 2, coc, n) = rbp(1)*v(1, 1, coc, n)+ &
                                                   rpw(1)*v(1, 1, coc, n+1)+ &
                                                   fcx*v(1, 1, cocx, n+1)
                                 v(1, 3, coc, n) = rbp(2)*v(1, 1, coc, n)+ &
                                                   rpw(2)*v(1, 1, coc, n+1)+ &
                                                   fcy*v(1, 1, cocy, n+1)
                                 v(1, 4, coc, n) = rbp(3)*v(1, 1, coc, n)+ &
                                                   rpw(3)*v(1, 1, coc, n+1)+ &
                                                   fcz*v(1, 1, cocz, n+1)
                              END DO

                              ! *** [sb||c]{n} = (Pi - Bi)*[s(b-1i)||c]{n} +          ***
                              ! ***              (Wi - Pi)*[s(b-1i)||c]{n+1} +        ***
                              ! ***              f2*Ni(b-1i)*(   [s(b-2i)||c]{n} +    ***
                              ! ***                           f4*[s(b-2i)||c]{n+1}) + ***
                              ! ***              f6*Ni(c)**[s(b-1i)||c-1i]{n+1}       ***

                              DO lb = 2, lb_max

                                 DO n = 1, nmax-lb-lc

                                    ! *** Increase the angular momentum component z of b ***

                                    v(1, coset(0, 0, lb), coc, n) = &
                                       rbp(3)*v(1, coset(0, 0, lb-1), coc, n)+ &
                                       rpw(3)*v(1, coset(0, 0, lb-1), coc, n+1)+ &
                                       f2*REAL(lb-1, dp)*(v(1, coset(0, 0, lb-2), coc, n)+ &
                                                          f4*v(1, coset(0, 0, lb-2), coc, n+1))+ &
                                       fcz*v(1, coset(0, 0, lb-1), cocz, n+1)

                                    ! *** Increase the angular momentum component y of b ***

                                    bz = lb-1
                                    v(1, coset(0, 1, bz), coc, n) = &
                                       rbp(2)*v(1, coset(0, 0, bz), coc, n)+ &
                                       rpw(2)*v(1, coset(0, 0, bz), coc, n+1)+ &
                                       fcy*v(1, coset(0, 0, bz), cocy, n+1)

                                    DO by = 2, lb
                                       f3 = f2*REAL(by-1, dp)
                                       bz = lb-by
                                       v(1, coset(0, by, bz), coc, n) = &
                                          rbp(2)*v(1, coset(0, by-1, bz), coc, n)+ &
                                          rpw(2)*v(1, coset(0, by-1, bz), coc, n+1)+ &
                                          f3*(v(1, coset(0, by-2, bz), coc, n)+ &
                                              f4*v(1, coset(0, by-2, bz), coc, n+1))+ &
                                          fcy*v(1, coset(0, by-1, bz), cocy, n+1)
                                    END DO

                                    ! *** Increase the angular momentum component x of b ***

                                    DO by = 0, lb-1
                                       bz = lb-1-by
                                       v(1, coset(1, by, bz), coc, n) = &
                                          rbp(1)*v(1, coset(0, by, bz), coc, n)+ &
                                          rpw(1)*v(1, coset(0, by, bz), coc, n+1)+ &
                                          fcx*v(1, coset(0, by, bz), cocx, n+1)
                                    END DO

                                    DO bx = 2, lb
                                       f3 = f2*REAL(bx-1, dp)
                                       DO by = 0, lb-bx
                                          bz = lb-bx-by
                                          v(1, coset(bx, by, bz), coc, n) = &
                                             rbp(1)*v(1, coset(bx-1, by, bz), coc, n)+ &
                                             rpw(1)*v(1, coset(bx-1, by, bz), coc, n+1)+ &
                                             f3*(v(1, coset(bx-2, by, bz), coc, n)+ &
                                                 f4*v(1, coset(bx-2, by, bz), coc, n+1))+ &
                                             fcx*v(1, coset(bx-1, by, bz), cocx, n+1)
                                       END DO
                                    END DO

                                 END DO

                              END DO

                           END IF

                        END IF

                     END DO
                  END DO

               END DO

            END IF

            ! *** Add the contribution of the current pair ***
            ! *** of primitive Gaussian-type functions     ***

            DO k = ncoset(lc_min-1)+1, ncoset(lc_max)
               kk = k-ncoset(lc_min-1)
               DO j = ncoset(lb_min-1)+1, ncoset(lb_max)
                  DO i = ncoset(la_min-1)+1, ncoset(la_max-maxder_local)
                     vabc(na+i, nb+j) = vabc(na+i, nb+j)+gccc(kk)*v(i, j, k, 1)
                     int_abc(na+i, nb+j, kk) = v(i, j, k, 1)
                  END DO
               END DO
            END DO

            IF (PRESENT(maxder)) THEN
               DO k = ncoset(lc_min-1)+1, ncoset(lc_max)
                  kk = k-ncoset(lc_min-1)
                  DO j = 1, ncoset(lb_max)
                     DO i = 1, ncoset(la_max)
                        vabc_plus(nap+i, nb+j) = vabc_plus(nap+i, nb+j)+gccc(kk)*v(i, j, k, 1)
                     END DO
                  END DO
               END DO
            END IF

            nb = nb+ncoset(lb_max)

         END DO

         na = na+ncoset(la_max-maxder_local)
         nap = nap+ncoset(la_max)

      END DO

   END SUBROUTINE coulomb3

END MODULE ai_coulomb
