projxyzt fixed. now ywrk is left unchanged
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118
src/gray.f
118
src/gray.f
@ -5712,11 +5712,9 @@ c gg=F(u)/u with F(u) as in Cohen paper
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dimension xtiv(nrmax),ytiv(nrmax),zwjv(nrmax),w(nrmax)
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dimension pvett(3),pvettn(3),dery0(3),dery0n(3)
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dimension deltax(3,jmx,kmx),avn(3,jmx,kmx),avmod(jmx,kmx)
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dimension deltaxdotn0(jmx,kmx),avndotn0(jmx,kmx)
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dimension aalpha(jmx,kmx),aplane(3,jmx,kmx)
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dimension avn(3,jmx,kmx)
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dimension aplane(3,jmx,kmx),asip(jmx,kmx)
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dimension gri(3,jmx,kmx)
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dimension aincr(3,jmx,kmx),asip(jmx,kmx)
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c parameter(nxmax=2*jmx-1)
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parameter(nxmax=2*kmx)
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@ -5768,51 +5766,33 @@ c initialize grid dimension for spline interpolation
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kktx=nrayth
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if(j.eq.1) kktx=1
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do k=1,kktx
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do ll=1,3
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aplane(ll,j,k)=ywrk(ll,j,k)
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enddo
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asip(j,k)=(dble(j-1)*rwmax/dble(nrayr-1))**2
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enddo
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enddo
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else
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if(iplane.eq.2) then
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endif
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if(iplane.eq.2) then
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c prjection parallel to vg on the plane perpendicular to n0 passing through x11
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do j=2,nrayr
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do k=1,nrayth
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avmod(j,k)=sqrt(ypwrk(1,j,k)*ypwrk(1,j,k)+
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. ypwrk(2,j,k)*ypwrk(2,j,k)+ypwrk(3,j,k)*ypwrk(3,j,k))
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do ii=1,3
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deltax(ii,j,k)=ywrk(ii,1,1)-ywrk(ii,j,k)
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avn(ii,j,k)=ypwrk(ii,j,k)/avmod(j,k)
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enddo
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deltaxdotn0(j,k)=deltax(1,j,k)*ywrk(4,1,1)+
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. deltax(2,j,k)*ywrk(5,1,1)+
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. deltax(3,j,k)*ywrk(6,1,1)
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avndotn0(j,k)=avn(1,j,k)*ywrk(4,1,1)+
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. avn(2,j,k)*ywrk(5,1,1)+
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. avn(3,j,k)*ywrk(6,1,1)
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aalpha(j,k)=deltaxdotn0(j,k)/avndotn0(j,k)
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do ll=1,3
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aplane(ll,j,k)=ywrk(ll,j,k)+aalpha(j,k)*avn(ll,j,k)
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enddo
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enddo
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enddo
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c ortogonal projection on the plane perpendicular to n0 passing through x11
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else
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do j=2,nrayr
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do k=1,nrayth
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do ii=1,3
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deltax(ii,j,k)=ywrk(ii,1,1)-ywrk(ii,j,k)
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enddo
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deltaxdotn0(j,k)=deltax(1,j,k)*ywrk(4,1,1)+
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. deltax(2,j,k)*ywrk(5,1,1)+
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. deltax(3,j,k)*ywrk(6,1,1)
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an02=ywrk(4,1,1)*ywrk(4,1,1)+ywrk(5,1,1)*ywrk(5,1,1)+
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. ywrk(6,1,1)*ywrk(6,1,1)
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aalpha(j,k)=deltaxdotn0(j,k)/an02
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do ll=1,3
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aplane(ll,j,k)=ywrk(ll,j,k)+aalpha(j,k)*ywrk(ll+3,1,1)
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enddo
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enddo
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enddo
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end if
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do j=2,nrayr
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do k=1,nrayth
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avmod=sqrt(ypwrk(1,j,k)**2+ypwrk(2,j,k)**2+ypwrk(3,j,k)**2)
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do ii=1,3
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avn(ii,j,k)=ypwrk(ii,j,k)/avmod
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enddo
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deltaxdotn0=(ywrk(1,1,1)-ywrk(1,j,k))*ywrk(4,1,1)+
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. (ywrk(2,1,1)-ywrk(2,j,k))*ywrk(5,1,1)+
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. (ywrk(3,1,1)-ywrk(3,j,k))*ywrk(6,1,1)
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avndotn0=avn(1,j,k)*ywrk(4,1,1)+
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. avn(2,j,k)*ywrk(5,1,1)+
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. avn(3,j,k)*ywrk(6,1,1)
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aalpha=deltaxdotn0/avndotn0
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do ll=1,3
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aplane(ll,j,k)=ywrk(ll,j,k)+aalpha*avn(ll,j,k)
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enddo
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enddo
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enddo
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do ll=1,3
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aplane(ll,1,1)=ywrk(ll,1,1)
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enddo
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@ -5820,21 +5800,36 @@ c ortogonal projection on the plane perpendicular to n0 passing through x11
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kktx=nrayth
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if(j.eq.1) kktx=1
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do k=1,kktx
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do ii=1,3
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aincr(ii,j,k)=aplane(ii,j,k)-ywrk(ii,j,k)
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ywrk(ii,j,k)=aplane(ii,j,k)
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enddo
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asip(j,k)=(dble(j-1)*rwmax/dble(nrayr-1))**2
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enddo
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enddo
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c Si evaluation on the projection plane(Taylor, first order)
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enddo
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endif
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if(iplane.eq.3) then
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c ortogonal projection on the plane perpendicular to n0 passing through x11
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do j=2,nrayr
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do k=1,nrayth
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deltaxdotn0=(ywrk(1,1,1)-ywrk(1,j,k))*ywrk(4,1,1)+
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. (ywrk(2,1,1)-ywrk(2,j,k))*ywrk(5,1,1)+
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. (ywrk(3,1,1)-ywrk(3,j,k))*ywrk(6,1,1)
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an02=ywrk(4,1,1)**2+ywrk(5,1,1)**2+ywrk(6,1,1)**2
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aalpha=deltaxdotn0/an02
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do ll=1,3
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aplane(ll,j,k)=ywrk(ll,j,k)+aalpha*ywrk(ll+3,1,1)
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enddo
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enddo
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enddo
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do ll=1,3
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aplane(ll,1,1)=ywrk(ll,1,1)
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enddo
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c Si evaluation on the projection plane(Taylor, first order)
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do j=1,nrayr
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kktx=nrayth
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if(j.eq.1) kktx=1
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do k=1,kktx
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asip(j,k)=(dble(j-1)*rwmax/dble(nrayr-1))**2+
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. gri(1,j,k)*aincr(1,j,k)+
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. gri(2,j,k)*aincr(2,j,k)+
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. gri(3,j,k)*aincr(3,j,k)
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. gri(1,j,k)*(aplane(1,j,k)-ywrk(1,j,k))+
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. gri(2,j,k)*(aplane(2,j,k)-ywrk(2,j,k))+
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. gri(3,j,k)*(aplane(3,j,k)-ywrk(3,j,k))
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enddo
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enddo
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endif
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@ -5846,9 +5841,9 @@ c
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zwj=asip(j,k)+
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. 0.5*(tauv(j,k,istep)-tauv(1,1,istep))
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c
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dx=ywrk(1,j,k)-ywrk(1,1,1)
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dy=ywrk(2,j,k)-ywrk(2,1,1)
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dz=ywrk(3,j,k)-ywrk(3,1,1)
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dx=aplane(1,j,k)-aplane(1,1,1)
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dy=aplane(2,j,k)-aplane(2,1,1)
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dz=aplane(3,j,k)-aplane(3,1,1)
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c
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dirx=ywrk(4,j,k)
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diry=ywrk(5,j,k)
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@ -5857,14 +5852,13 @@ c
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if (j>1) then
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k2=mod(k+kktx/4-1,kktx)+1
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dx2=ywrk(1,j,k2)-ywrk(1,1,1)
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dy2=ywrk(2,j,k2)-ywrk(2,1,1)
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dz2=ywrk(3,j,k2)-ywrk(3,1,1)
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dx2=aplane(1,j,k2)-aplane(1,1,1)
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dy2=aplane(2,j,k2)-aplane(2,1,1)
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dz2=aplane(3,j,k2)-aplane(3,1,1)
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pvett(1)=dy*dz2-dy2*dz
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pvett(2)=dz*dx2-dz2*dx
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pvett(3)=dx*dy2-dx2*dy
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pvettmod=sqrt(pvett(1)*pvett(1)+
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. pvett(2)*pvett(2)+pvett(3)*pvett(3))
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pvettmod=sqrt(pvett(1)**2+pvett(2)**2+pvett(3)**2)
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do ll=1,3
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pvettn(ll)=pvett(ll)/pvettmod
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dery0n(ll)=dery0(ll)/dery0mod
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