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!******************************************************************************
!
! DPI Library
! Dynamical Plug-In for Mercury 6
! Release 1.0
!
! Copyright (C) 2002-2015 Diego Turrini
!
! This program is free software: you can redistribute it and/or modify
! it under the terms of the GNU General Public License as published by
! the Free Software Foundation, either version 3 of the License, or
! (at your option) any later version.
!
! This program is distributed in the hope that it will be useful,
! but WITHOUT ANY WARRANTY; without even the implied warranty of
! MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
! GNU General Public License for more details.
!
! You should have received a copy of the GNU General Public License
! along with this program. If not, see <http://www.gnu.org/licenses/>.
!
!------------------------------------------------------------------------------
!
! DPI Library
! Dynamical Plug-In for Mercury 6
!
! Release: 1.0
! Author: Diego Turrini
! E-mail: diego.turrini_at_iaps.inaf.it
! Last modified: January 2010
! Modified by: Diego Turrini
!
! Disclaimer: this library is supplied as a plug-in for the Mercury software
! developed by John E. Chamber: specifically, it is designed to
! work with version 6 of Mercury. To facilitate its use in
! conjunction with Mercury, the design of the subroutines was
! kept as similar as possible to that of analogous subroutines
! in Mercury. Mercury is developed by John E. Chambers and can
! be downloaded at the following URL:
! http://www.arm.ac.uk/~jec/home.html (see also the
! Astrophysics Source Code Library, ascl id. 1201.008)
! The DPI library contains some subroutines derived and adapted
! from Mercury 6 and originally developed by John E. Chambers.
! Information on the author and, where appropriate, the name of
! the original subroutines are reported in the headers.
!
! Acknowledgements: the author wishes to thank Patricia Eleanor Verrier
! for her assistance in debugging and restructuring the
! algorithm and the code through comparison with her
! MOIRAI software.
!
! Bibliographic references:
!
! Mercury 6 software:
!
! Chambers J. E., 1999, Monthly Notices of the Royal Astronomical Society,
! vol. 304, pp. 793-799
!
! Symplectic mapping for S-type binary star systems:
!
! Chambers J. E., Quintana E. V., Duncan M. J., Lissauer J. J., 2002, The
! Astrophysical Journal, vol. 123, pp. 2884-2894
!
! MOIRAI software:
!
! Verrier P. E., Evans N. W., 2007, Monthly Notices of the Royal
! Astronomical Society, vol. 382, pp. 1432-1446
!
! DPI library:
!
! Turrini D., Barbieri M., Marzari F., Thebault P., Tricarico P., 2005,
! Memorie della Societa' Astronomica Italiana Supplementi, vol. 6,
! pp. 172-177
!
! Turrini D., Barbieri M., Marzari F., Tricarico P., 2004, Memorie della
! Societa' Astronomica Italiana Supplementi, vol. 5, pp. 127-130
!
! Thebault P., Marzari F., Scholl H., Turrini D., Barbieri M., 2004,
! Astronomy & Astrophysics, vol. 427, pp. 1097-1104
!
!******************************************************************************
!
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to convert from the initial, inertial coordinates to
! S-type binary coordinates as in Chambers et al. (2002)
! N.B.: the subroutine computes positions and pseudovelocities, not the
! state vectors
! N.B.: the initial coordinates are centered on the initial position of the
! central star yet are not heliocentric
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
subroutine dpi_h2wb(nbig,nbod,m,xh,vh,xb,pvb)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod)
real*8 xh(3,nbod),vh(3,nbod)
real*8 xb(3,nbod),pvb(3,nbod)
! Local variables
integer i,j
real*8 mtot,mden,mvh(3),mxh(3)
! Variables initialization
do i=1,3
mxh(i)=0.d0
mvh(i)=0.d0
end do
do j=1,nbod
do i=1,3
xb(i,j)=0.d0
pvb(i,j)=0.d0
end do
end do
! Computing support variables
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
do i=1,3
mvh(i)=mvh(i)+m(j)*vh(i,j)
mxh(i)=mxh(i)+m(j)*xh(i,j)
end do
end do
end if
mden=mtot
mtot=mtot+m(nbig)
! Computing transformed positions for S type binary systems
! Computing position of central star
do i=1,3
xb(i,1)=(m(1)*xh(i,1)+m(nbig)*xh(i,nbig)+mxh(i))/mtot
end do
! If any, computing positions of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
xb(i,j)=xh(i,j)-xh(i,1)
end do
end do
end if
! Computing position of binary star
do i=1,3
xb(i,nbig)=xh(i,nbig)-(m(1)*xh(i,1)+mxh(i))/mden
end do
! If any, computing positions of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
xb(i,j)=xh(i,j)-xh(i,1)
end do
end do
end if
! Computing transformed pseudo-velocities for S type binary systems
! Computing pseudo-velocity of central star
do i=1,3
pvb(i,1)=(m(1)*vh(i,1)+m(nbig)*vh(i,nbig)+mvh(i))/mtot
end do
! If any, computing pseudo-velocities of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
pvb(i,j)=vh(i,j)-(m(1)*vh(i,1)+mvh(i))/mden
end do
end do
end if
! Computing pseudo-velocity of binary star
do i=1,3
pvb(i,nbig)=vh(i,nbig)-pvb(i,1)
end do
! If any, computing pseudo-velocities of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
pvb(i,j)=vh(i,j)-(m(1)*vh(i,1)+mvh(i))/mden
end do
end do
end if
end subroutine dpi_h2wb
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to convert from the S-type binary coordinates to the initial,
! inertial coordinates as in Chambers et al. (2002)
! N.B.: the subroutine needs positions and pseudovelocities, not the
! state vectors
! N.B.: the initial coordinates are centered on the initial position of the
! central star yet are not heliocentric
! Author: Diego Turrini
! Last modified: January 2010
!******************************************************************************
subroutine dpi_wb2h(nbig,nbod,m,xh,vh,xb,pvb)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod)
real*8 xh(3,nbod),vh(3,nbod)
real*8 xb(3,nbod),pvb(3,nbod)
! Local variables
integer i,j
real*8 mtot,mden,mvb(3),mxb(3)
! Variables initialization
do i=1,3
mxb(i)=0.d0
mvb(i)=0.d0
end do
do j=1,nbod
do i=1,3
xh(i,j)=0.d0
vh(i,j)=0.d0
end do
end do
! Computing support variables
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
do i=1,3
mxb(i)=mxb(i)+m(j)*xb(i,j)
mvb(i)=mvb(i)+m(j)*pvb(i,j)
end do
end do
end if
mden=mtot
mtot=mtot+m(nbig)
! Computing heliocentric positions for S type binary systems
! Computing position of central star
do i=1,3
xh(i,1)=xb(i,1)-(m(nbig)/mtot)*xb(i,nbig)-mxb(i)/mden
end do
! If any, computing positions of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
xh(i,j)=xb(i,j)+xh(i,1)
end do
end do
end if
! Computing position of binary star
do i=1,3
xh(i,nbig)=xb(i,1)+(mden/mtot)*xb(i,nbig)
end do
! Computing positions of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
xh(i,j)=xb(i,j)+xh(i,1)
end do
end do
end if
! Computing heliocentric velocities for S type binary systems
! Computing velocity of central star
do i=1,3
vh(i,1)=pvb(i,1)-(m(nbig)/mden)*pvb(i,nbig)-mvb(i)/m(1)
end do
! If any, computing velocities of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
vh(i,j)=pvb(i,j)+pvb(i,1)-(m(nbig)/mden)*pvb(i,nbig)
end do
end do
end if
! Computing velocity of binary star
do i=1,3
vh(i,nbig)=pvb(i,1)+pvb(i,nbig)
end do
! If any, computing velocities of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
vh(i,j)=pvb(i,j)+pvb(i,1)-(m(nbig)/mden)*pvb(i,nbig)
end do
end do
end if
end subroutine dpi_wb2h
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to convert S-type velocities for Keplerian propagation back
! to pseudovelocities (based on the subroutines developed by Patricia
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
subroutine dpi_vb2psv_k(nbig,nbod,m,xb,vb,psv)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod)
real*8 xb(3,nbod),vb(3,nbod),psv(3,nbod)
! Local variables
integer i,j
real*8 mtot,mden
! Variables initialization
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
end do
end if
mden=mtot
mtot=mtot+m(nbig)
! Computing pseudo-velocity of central star
do i=1,3
psv(i,1)=vb(i,1)
end do
! If any, computing pseudo-velocities of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
psv(i,j)=vb(i,j)
end do
end do
end if
! Computing pseudo-velocity of binary star
do i=1,3
psv(i,nbig)=vb(i,nbig)/(mtot/mden)
end do
! If any, computing pseudo-velocities of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
psv(i,j)=vb(i,j)
end do
end do
end if
end subroutine dpi_vb2psv_k
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to convert pseudovelocities to S-type velocities for Keplerian
! propagation
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
subroutine dpi_psv2vb_k(nbig,nbod,m,xb,vb,psv)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod)
real*8 xb(3,nbod),vb(3,nbod),psv(3,nbod)
! Local variables
integer i,j
real*8 mtot,mden
! Variables initialization
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
end do
end if
mden=mtot
mtot=mtot+m(nbig)
! Computing transformed velocity of central star
do i=1,3
vb(i,1)=psv(i,1)
end do
! If any, computing transformed velocities of massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
vb(i,j)=psv(i,j)
end do
end do
end if
! Computing transformed velocity of binary star
do i=1,3
vb(i,nbig)=psv(i,nbig)*mtot/mden
end do
! If any, computing transformed velocities of massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
vb(i,j)=psv(i,j)
end do
end do
end if
end subroutine dpi_psv2vb_k
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to compute the H_jump part of the transformed Hamiltonian for
! S-type binary systems
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
subroutine dpi_wbjump(nbig,nbod,dt,m,xb,pvb)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod),dt
real*8 xb(3,nbod),pvb(3,nbod)
! Local variables
integer i,j
real*8 pbsum(3)
! Variables initialization
do i=1,3
pbsum(i)=0.d0
end do
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
pbsum(i)=pbsum(i)+pvb(i,j)*m(j)
end do
end do
do i=1,3
pbsum(i)=dt*pbsum(i)/m(1)
end do
! Advancing massive particles
do j=2,nbig-1
do i=1,3
xb(i,j)=xb(i,j)+pbsum(i)
end do
end do
end if
! Advancing massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
xb(i,j)=xb(i,j)+pbsum(i)
end do
end do
end if
end subroutine dpi_wbjump
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to compute the accelerations due to the H_int part of the
! transformed Hamiltonian for S-type binary systems
! Author: Diego Turrini
! Last modified: January 2010
!******************************************************************************
subroutine dpi_wbfor(nbig,nbod,xb,a,m,rcrit)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 xb(3,nbod),m(nbod),a(3,nbod),rcrit(nbod)
! Local variables
integer i,j,l
real*8 mden,mtot,s(3),den1,den2,den3(nbod)
real*8 factor1(3),factor2(3,nbod),rb(nbod)
real*8 drb(3),cenorm,r,r2,r3,rc,rc2,q,q3,q4,q5
real*8 cube,vmod,vsqr
external cube,vmod,vsqr
intrinsic max,sqrt
! Variables initialization
do i=1,3
factor1(i)=0.d0
s(i)=0.d0
end do
do j=1,nbod
rb(j)=0.d0
do i=1,3
a(i,j)=0.d0
factor2(i,j)=0.d0
end do
end do
! Computation of support variables
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
do i=1,3
s(i)=s(i)+m(j)*xb(i,j)
end do
end do
! N.B.: here mtot = mtot-m(nbod) = mden
do i=1,3
s(i)=s(i)/mtot
end do
end if
mden=mtot
mtot=mtot+m(nbig)
do i=1,3
factor1(i)=xb(i,nbig)+s(i)
end do
rb(nbig)=vmod(xb(1,nbig),xb(2,nbig),xb(3,nbig))
den1=cube(rb(nbig))
den2=cube(vmod(factor1(1),factor1(2),factor1(3)))
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
factor2(i,j)=xb(i,nbig)-xb(i,j)+s(i)
end do
rb(j)=vmod(xb(1,j),xb(2,j),xb(3,j))
den3(j)=cube(vmod(factor2(1,j),factor2(2,j),factor2(3,j)))
end do
end if
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
factor2(i,j)=xb(i,nbig)-xb(i,j)+s(i)
end do
rb(j)=vmod(xb(1,j),xb(2,j),xb(3,j))
den3(j)=cube(vmod(factor2(1,j),factor2(2,j),factor2(3,j)))
end do
end if
! Computation of the acceleration of the binary companion
do i=1,3
a(i,nbig)=a(i,nbig)+m(1)*(xb(i,nbig)/den1)
a(i,nbig)=a(i,nbig)-m(1)*factor1(i)/den2
end do
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
a(i,nbig)=a(i,nbig)+m(j)*(xb(i,nbig)/den1)
a(i,nbig)=a(i,nbig)-m(j)*factor2(i,j)/den3(j)
end do
end do
end if
! Computation of the accelerations of the massive particles
if (nbig.gt.2) then
do j=2,nbig-1
do i=1,3
a(i,j)=a(i,j)-(m(1)*m(nbig)/mden)*(factor1(i)/den2)
a(i,j)=a(i,j)+m(nbig)*factor2(i,j)/den3(j)
end do
end do
do j=2,nbig-1
do l=2,nbig-1
do i=1,3
a(i,j)=a(i,j)-(m(nbig)*m(l)/mden)*factor2(i,l)/den3(l)
end do
end do
end do
end if
if (nbig.gt.3) then
do j=2,nbig-1
do l=j+1,nbig-1
drb(1)=xb(1,j)-xb(1,l)
drb(2)=xb(2,j)-xb(2,l)
drb(3)=xb(3,j)-xb(3,l)
r2=vsqr(drb(1),drb(2),drb(3))
r=sqrt(r2)
r3=r*r*r
rc=max(rcrit(j),rcrit(l))
rc2=rc*rc
do i=1,3
if (r2.ge.rc2) then
cenorm=1.d0
else if (r2.le.0.01d0*rc2) then
cenorm=0.d0
else
q=(r-0.1d0*rc)/(0.9d0*rc)
q3=q*q*q
q4=q3*q
q5=q4*q
cenorm=(10.d0*q3-15.d0*q4+6.d0*q5)
end if
a(i,j)=a(i,j)-cenorm*m(l)*drb(i)/r3
a(i,l)=a(i,l)+cenorm*m(j)*drb(i)/r3
end do
end do
end do
end if
! Computation of the accelerations of the massless particles
if (nbod.gt.nbig) then
do j=nbig+1,nbod
do i=1,3
a(i,j)=a(i,j)-(m(1)*m(nbig)/mden)*(factor1(i)/den2)
a(i,j)=a(i,j)+m(nbig)*factor2(i,j)/den3(j)
end do
end do
end if
if (nbig.gt.2.and.nbod.gt.nbig) then
do j=nbig+1,nbod
do l=2,nbig-1
do i=1,3
a(i,j)=a(i,j)-(m(nbig)*m(l)/mden)*factor2(i,l)/den3(l)
end do
end do
end do
do l=nbig+1,nbod
do j=2,nbig-1
drb(1)=xb(1,l)-xb(1,j)
drb(2)=xb(2,l)-xb(2,j)
drb(3)=xb(3,l)-xb(3,j)
r2=vsqr(drb(1),drb(2),drb(3))
r=sqrt(r2)
r3=r*r*r
rc=max(rcrit(j),rcrit(l))
rc2=rc*rc
do i=1,3
if (r2.ge.rc2) then
cenorm=1.d0
else if (r2.le.0.01d0*rc2) then
cenorm=0.d0
else
q=(r-0.1d0*rc)/(0.9d0*rc)
q3=q*q*q
q4=q3*q
q5=q4*q
cenorm=(10.d0*q3-15.d0*q4+6.d0*q5)
end if
a(i,l)=a(i,l)-cenorm*m(j)*drb(i)/r3
end do
end do
end do
end if
end subroutine dpi_wbfor
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to advance of one time step the N-Body system for S-type
! binary systems
! Author: Diego Turrini
! Last modified: January 2010
!******************************************************************************
subroutine dpi_wbstep(time,tstart,h0,tol,rmax,en,am,jcen,rcen,
& nbod,nbig,m,xh,vh,s,rphys,rcrit,rce,stat,id,ngf,algor,opt,dtflag
& ,ngflag,opflag,colflag,nclo,iclo,jclo,dclo,tclo,ixvclo,jxvclo,
& outfile,mem,lmem)
implicit none
include 'mercury.inc'
! Input/Output variables
integer nbod,nbig,stat(nbod),algor,opt(8),dtflag,ngflag,opflag
integer colflag,lmem(NMESS),nclo,iclo(CMAX),jclo(CMAX)
real*8 time,tstart,h0,tol,rmax,en(3),am(3),jcen(3),rcen
real*8 m(nbod),xh(3,nbod),vh(3,nbod),s(3,nbod),rphys(nbod)
real*8 rce(nbod),rcrit(nbod),ngf(4,nbod),tclo(CMAX),dclo(CMAX)
real*8 ixvclo(6,CMAX),jxvclo(6,CMAX)
character*80 outfile(3),mem(NMESS)
character*8 id(nbod)
! Local variables
integer i,j,iflag,nce,ice(nbod),jce(nbod),ce(nbod)
real*8 a(3,NMAX),x0(3,nbod),v0(3,nbod),hrec,hby2
real*8 xb(3,NMAX),pvb(3,NMAX),vb(3,NMAX)
real*8 mden,mtot,gm(NMAX),mb(NMAX)
external dpi_h2wb,dpi_wb2h,dpi_psv2vb_k,dpi_vb2psv_k
external dpi_wbfor,dpi_wbjump,drift_one,dpi_bhkce
save hrec,gm,mb,xb,pvb,a,mtot,mden
! N.B.: this subroutine internally uses the type S (wide binary)
! coordinate system described in Chambers et al. (2002)
hby2=h0*0.5d0
nclo = 0
colflag = 0
if (dtflag.ne.2) then
if (dtflag.eq.0) hrec=h0
call dpi_h2wb(nbig,nbod,m,xh,vh,xb,pvb)
! Computing accelerations
do j=1,nbod
do i=1,3
a(i,j)=0.d0
end do
end do
if (nbod.gt.2) call dpi_wbfor(nbig,nbod,xb,a,m,rcrit)
gm(1)=0.d0
mb(1)=0.d0
if (nbod.lt.3) then
mden=m(1)
mtot=m(1)+m(2)
gm(2)=mtot
mb(2)=m(nbod)*m(1)/mtot
else
mtot=m(1)
do j=2,nbig-1
mtot=mtot+m(j)
gm(j)=m(1)
mb(j)=m(j)
end do
mden=mtot
mtot=mtot+m(nbig)
gm(nbig)=mtot
mb(nbig)=m(nbig)*mden/mtot
do j=nbig+1,nbod
gm(j)=m(1)
mb(j)=m(j)
end do
end if
dtflag = 2
end if
if (nbod.gt.2) then
! Advancing the Interaction Hamiltonian
do j=2,nbod
do i=1,3
pvb(i,j)=pvb(i,j)+hby2*a(i,j)
end do
end do
! Advancing the Jump Hamiltonian
call dpi_wbjump(nbig,nbod,hby2,m,xb,pvb)
end if
! Computing transformed velocities
call dpi_psv2vb_k(nbig,nbod,m,xb,vb,pvb)
! Save the current coordinates and velocities
call mco_iden(time,jcen,nbod,nbig,h0,m,xb,vb,x0,v0,ngf,ngflag,opt)
! Advancing the Keplerian Hamiltonian
do j=2,nbod
iflag=0
call drift_one(gm(j),xb(1,j),xb(2,j),xb(3,j),vb(1,j),vb(2,j),
& vb(3,j),h0,iflag)
end do
! Check whether any object separations were < R_CRIT whilst advancing H_K
call dpi_snif(h0,2,nbod,nbig,x0,v0,xb,vb,rcrit,ce,nce,ice,jce)
! If objects had close encounters, advance H_K using Bulirsch-Stoer instead
if (nce.gt.0) then
do j=2,nbod
if (ce(j).ne.0) then
do i=1,3
xb(i,j) = x0(i,j)
vb(i,j) = v0(i,j)
end do
end if
end do
call dpi_bhkce(time,tstart,h0,hrec,tol,rmax,en(3),jcen,rcen,
& nbod,nbig,m,xb,vb,s,rphys,rcrit,rce,stat,id,ngf,
& algor,opt,ngflag,colflag,ce,nce,ice,jce,nclo,iclo,
& jclo,dclo,tclo,ixvclo,jxvclo,outfile,mem,lmem)
end if
! Computing transformed pseudovelocities
call dpi_vb2psv_k(nbig,nbod,m,xb,vb,pvb)
if (nbod.gt.2) then
! Advancing the Jump Hamiltonian
call dpi_wbjump(nbig,nbod,hby2,m,xb,pvb)
! Computing accelerations
call dpi_wbfor(nbig,nbod,xb,a,m,rcrit)
! Advancing the Interaction Hamiltonian
do j=2,nbod
do i=1,3
pvb(i,j)=pvb(i,j)+hby2*a(i,j)
end do
end do
end if
! Updating inertial (input) coordinates
call dpi_wb2h(nbig,nbod,m,xh,vh,xb,pvb)
end subroutine dpi_wbstep
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine to computate of energy and angular momentum in the transformed
! coordinate system for S-type binary systems
! Author: Diego Turrini
! Last modified: June 2009
!******************************************************************************
subroutine dpi_en(nbod,nbig,m,xh,vh,energy,angmom)
implicit none
! Input/Output variables
integer nbod,nbig
real*8 m(nbod)
real*8 xh(3,nbod),vh(3,nbod)
real*8 energy,angmom
! Local variables
integer i,j,l
real*8 xb(3,nbod),pvb(3,nbod)
real*8 mden,mtot,rp,drp(3),amom(3)
real*8 r(nbod),p2(nbod),pbsum(3),sp(3)
real*8 Hkep,Hint,Hjump
real*8 vmod,vsqr
external vmod,vsqr
! Computing S type variables
call dpi_h2wb(nbig,nbod,m,xh,vh,xb,pvb)
! Variables initialization
Hkep=0.d0
Hint=0.d0
Hjump=0.d0
mtot=m(1)
if (nbig.gt.2) then
do j=2,nbig-1
mtot=mtot+m(j)
end do
end if
mden=mtot
mtot=mtot+m(nbig)
! Computing Keplerian energy
r(1)=0.d0
p2(1)=0.d0!vsqr(pvb(1,1),pvb(2,1),pvb(3,1))
do j=2,nbig
r(j)=vmod(xb(1,j),xb(2,j),xb(3,j))
p2(j)=vsqr(pvb(1,j),pvb(2,j),pvb(3,j))
end do
if (nbig.gt.2) then
do j=2,nbig-1
Hkep=Hkep+0.5d0*m(j)*p2(j)
Hkep=Hkep-m(j)*m(1)/r(j)
end do
end if
Hkep=Hkep+m(nbig)*mtot*p2(nbig)/(2.0d0*mden)
Hkep=Hkep-m(nbig)*mden/r(nbig)
if (nbig.gt.2) then
! Computation of support variables
do i=1,3
sp(i)=0.d0
end do
do j=2,nbig-1
do i=1,3
sp(i)=sp(i)+m(j)*xb(i,j)
end do
end do
do i=1,3
sp(i)=sp(i)/mden
end do
! Computation of the Interaction part of the Hamiltonian
Hint=Hint+m(nbig)*m(1)/r(nbig)
do j=2,nbig-1
Hint=Hint+m(nbig)*m(j)/r(nbig)
end do
Hint=Hint-m(nbig)*m(1)/vmod((xb(1,nbig)+sp(1)),
& (xb(2,nbig)+sp(2)),(xb(3,nbig)+sp(3)))
do j=2,nbig-1
Hint=Hint-m(nbig)*m(j)/vmod((xb(1,nbig)-xb(1,j)+sp(1)),
& (xb(2,nbig)-xb(2,j)+sp(2)),(xb(3,nbig)-xb(3,j)+sp(3)))
end do
if (nbig.gt.3) then
do j=2,nbig-1
do l=j+1,nbig-1
drp(1)=xb(1,j)-xb(1,l)
drp(2)=xb(2,j)-xb(2,l)
drp(3)=xb(3,j)-xb(3,l)
rp=vmod(drp(1),drp(2),drp(3))
Hint=Hint-(m(j)*m(l)/rp)
end do
end do
end if
! Computation of the Jump part of the Hamiltonian
do i=1,3
pbsum(i)=0.d0
end do
do j=2,nbig-1
do i=1,3
pbsum(i)=pbsum(i)+pvb(i,j)*m(j)
end do
end do
Hjump=vsqr(pbsum(1),pbsum(2),pbsum(3))/(2.d0*m(1))
end if
! Computing total energy (including contribution from central star)
energy=Hkep+Hint+Hjump!+(0.5d0*mtot*p2(1))
! Computing angular momentum
amom(1)=mtot*(xb(2,1)*pvb(3,1)-xb(3,1)*pvb(2,1))
amom(2)=mtot*(xb(3,1)*pvb(1,1)-xb(1,1)*pvb(3,1))
amom(3)=mtot*(xb(1,1)*pvb(2,1)-xb(2,1)*pvb(1,1))
do j=2,nbig
amom(1)=amom(1)+m(j)*(xb(2,j)*pvb(3,j)-xb(3,j)*pvb(2,j))
amom(2)=amom(2)+m(j)*(xb(3,j)*pvb(1,j)-xb(1,j)*pvb(3,j))
amom(3)=amom(3)+m(j)*(xb(1,j)*pvb(2,j)-xb(2,j)*pvb(1,j))
end do
angmom=vmod(amom(1),amom(2),amom(3))
end subroutine dpi_en
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Function to computate the squared modulus of a vector (i.e. its dot
! product against itself)
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
function vsqr(x,y,z)
implicit none
! Input/Output variables
real*8 vsqr,x,y,z
! Computing scalar product
vsqr=(x*x+y*y+z*z)
end function vsqr
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Function to computate of the modulus of a vector (i.e. its root square
! dot product)
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
function vmod(x,y,z)
implicit none
! Input/Output variables
real*8 vmod,x,y,z
intrinsic sqrt
! Computing vectorial module
vmod=sqrt(x*x+y*y+z*z)
end function vmod
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Function to compute the cubic power of a scalar variable
! Author: Diego Turrini
! Last modified: May 2009
!******************************************************************************
function cube(x)
implicit none
! Input/Output variables
real*8 cube,x
! Computing cube of scalar x
cube=x*x*x
end function cube
!******************************************************************************
! Dynamical Plug-In for Mercury 6
! Subroutine for the numerical integration of the Keplerian part of the
! Hamiltonian for S-type binary stars systems during close encounters
! (derived from MDT_HKCE subroutine of Mercury 6.2)
! Adapted by: Diego Turrini
! Last modified: July 2009
!******************************************************************************
!
! Author: John E. Chambers (subroutine MDT_HKCE in Mercury 6.2)
!
! Integrates NBOD bodies (of which NBIG are Big) for one timestep H under
! the Hamiltonian H_K, including close-encounter terms.
!
!******************************************************************************
subroutine dpi_bhkce(time,tstart,h0,hrec,tol,rmax,elost,jcen,
% rcen,nbod,nbig,m,x,v,s,rphy,rcrit,rce,stat,id,ngf,algor,opt,
% ngflag,colflag,ce,nce,ice,jce,nclo,iclo,jclo,dclo,tclo,ixvclo,
% jxvclo,outfile,mem,lmem)
implicit none
include 'mercury.inc'
! Input/Output
integer nbod,nbig,nce,ice(nce),jce(nce),stat(nbod),ngflag,ce(nbod)
integer algor,opt(8),colflag,lmem(NMESS),nclo,iclo(CMAX)
integer jclo(CMAX)
real*8 time,tstart,h0,hrec,tol,rmax,elost,jcen(3),rcen
real*8 m(nbod),x(3,nbod),v(3,nbod),s(3,nbod)
real*8 rce(nbod),rphy(nbod),rcrit(nbod),ngf(4,nbod)
real*8 tclo(CMAX),dclo(CMAX),ixvclo(6,CMAX),jxvclo(6,CMAX)
character*80 outfile(3),mem(NMESS)
character*8 id(nbod)
! Local
integer iback(NMAX),indexs(NMAX),ibs(NMAX),jbs(NMAX),nclo_old
integer i,j,k,nbs,nbsbig,statbs(NMAX)
integer nhit,ihit(CMAX),jhit(CMAX),chit(CMAX),nowflag,dtflag
real*8 tlocal,hlocal,hdid,tmp0
real*8 mbs(NMAX),xbs(3,NMAX),vbs(3,NMAX),sbs(3,NMAX)
real*8 rcritbs(NMAX),rcebs(NMAX),rphybs(NMAX)
real*8 ngfbs(4,NMAX),x0(3,NMAX),v0(3,NMAX)
real*8 thit(CMAX),dhit(CMAX),thit1,temp
character*8 idbs(NMAX)
! N.B.: Don't set nclo to zero!!
nbs = 1
nbsbig = 0
mbs(1) = m(1)
do k=1,3
sbs(k,1) = s(k,1)
end do
! P-type binary algorithm still to be implemented, stop integration
if (algor.eq.11) then
! if (algor.eq.11) mbs(1) = m(1) + m(2)
write(6,*) "P-type binary algorithm still to be implemented"
write(6,*) "Stopping integration"
stop
end if
! S-type binary algorithm does not allow collisions with binary companion
if ((algor.eq.12).and.(ce(nbig).ne.0)) stop
! Put data for close-encounter bodies into local arrays for use with BS routine
do j = 2, nbod
if (ce(j).ne.0) then
nbs = nbs + 1
if (j.le.nbig) nbsbig = nbs
mbs(nbs) = m(j)
do k=1,3
xbs(k,nbs) = x(k,j)
vbs(k,nbs) = v(k,j)
sbs(k,nbs) = s(k,j)
end do
rcebs(nbs) = rce(j)
rphybs(nbs) = rphy(j)
statbs(nbs) = stat(j)
rcritbs(nbs) = rcrit(j)
idbs(nbs) = id(j)
indexs(nbs) = j
iback(j) = nbs
end if
end do
do k = 1, nce
ibs(k) = iback(ice(k))
jbs(k) = iback(jce(k))
end do
tlocal = 0.d0
hlocal = sign(hrec,h0)
! Begin the Bulirsch-Stoer integration
50 continue
tmp0 = abs(h0) - abs(tlocal)
hrec = hlocal
if (abs(hlocal).gt.tmp0) hlocal = sign (tmp0, h0)
! Save old coordinates and integrate
call mco_iden (time,jcen,nbs,0,h0,mbs,xbs,vbs,x0,v0,ngf,ngflag,
% opt)
call dpi_bs2 (time,hlocal,hdid,tol,jcen,nbs,nbsbig,mbs,xbs,vbs,
% sbs,rphybs,rcritbs,ngfbs,statbs,dtflag,ngflag,opt,nce,
% ibs,jbs)
tlocal = tlocal + hdid
! Check for close-encounter minima
nclo_old = nclo
temp = time + tlocal
call mce_stat (temp,hdid,rcen,nbs,nbsbig,mbs,x0,v0,xbs,vbs,
% rcebs,rphybs,nclo,iclo,jclo,dclo,tclo,ixvclo,jxvclo,nhit,ihit,
% jhit,chit,dhit,thit,thit1,nowflag,statbs,outfile(3),mem,lmem)
! If collisions occurred, resolve the collision and return a flag
if (nhit.gt.0.and.opt(2).ne.0) then
do k = 1, nhit
if (chit(k).eq.1) then
i = ihit(k)
j = jhit(k)
call dpi_coll (thit(k),tstart,elost,jcen,i,j,nbs,nbsbig,
% mbs,xbs,vbs,sbs,rphybs,statbs,idbs,opt,mem,lmem,
% outfile(3))
colflag = colflag + 1
end if
end do
end if
! If necessary, continue integrating objects undergoing close encounters
if ((tlocal - h0)*h0.lt.0) goto 50
! Return data for the close-encounter objects to global arrays
do k = 2, nbs
j = indexs(k)
m(j) = mbs(k)
x(1,j) = xbs(1,k)
x(2,j) = xbs(2,k)
x(3,j) = xbs(3,k)
v(1,j) = vbs(1,k)
v(2,j) = vbs(2,k)
v(3,j) = vbs(3,k)
s(1,j) = sbs(1,k)
s(2,j) = sbs(2,k)
s(3,j) = sbs(3,k)
stat(j) = statbs(k)