| 43 |
|
|
| 44 |
c DATA ALMAX/dinf,dinf,1.,dinf,dinf/ !limits on alpha vector components |
c DATA ALMAX/dinf,dinf,1.,dinf,dinf/ !limits on alpha vector components |
| 45 |
c DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
c DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
| 46 |
DATA ALMAX/dinf,dinf,dinf,dinf,dinf/ !limits on alpha vector components |
DATA ALMAX/dinf,dinf,1.,dinf,dinf/ !limits on alpha vector components |
| 47 |
DATA ALMIN/-dinf,-dinf,-dinf,-dinf,-dinf/ !" |
DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
| 48 |
|
|
| 49 |
DIMENSION DAL(5) !increment of vector alfa |
DIMENSION DAL(5) !increment of vector alfa |
| 50 |
DIMENSION CHI2DD_R(4,4),CHI2D_R(4) !hessiano e gradiente di chi2 |
DIMENSION CHI2DD_R(4,4),CHI2D_R(4) !hessiano e gradiente di chi2 |
| 105 |
* ---------------------------------------------------------- |
* ---------------------------------------------------------- |
| 106 |
* changed in order to evaluate energy-dependent |
* changed in order to evaluate energy-dependent |
| 107 |
* tolerances on all 5 parameters |
* tolerances on all 5 parameters |
| 108 |
FACT=100. !scale factor to define tolerance on alfa |
cPP FACT=1.0e10 !scale factor to define tolerance on alfa |
| 109 |
c deflection error (see PDG) |
c deflection error (see PDG) |
| 110 |
DELETA1 = 0.01/0.3/0.4/0.4451**2*SQRT(720./(6.+4.)) |
DELETA1 = 0.01/0.3/0.4/0.4451**2*SQRT(720./(6.+4.)) |
| 111 |
DELETA2 = 0.016/0.3/0.4/0.4451*SQRT(0.4451/9.36) |
DELETA2 = 0.016/0.3/0.4/0.4451*SQRT(0.4451/9.36) |
| 121 |
* |
* |
| 122 |
ISTEP=0 !num. steps to minimize chi^2 |
ISTEP=0 !num. steps to minimize chi^2 |
| 123 |
JFAIL=0 !error flag |
JFAIL=0 !error flag |
| 124 |
|
CHI2=0 |
| 125 |
|
|
| 126 |
if(TRKDEBUG) print*,'guess: ',al |
if(TRKDEBUG) print*,'guess: ',al |
| 127 |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,1./AL(5) |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,1./AL(5) |
| 141 |
RETURN |
RETURN |
| 142 |
ENDIF |
ENDIF |
| 143 |
|
|
| 144 |
COST=1e-7 |
COST=1e-5 |
| 145 |
DO I=1,5 |
DO I=1,5 |
| 146 |
DO J=1,5 |
DO J=1,5 |
| 147 |
CHI2DD(I,J)=CHI2DD(I,J)*COST |
CHI2DD(I,J)=CHI2DD(I,J)*COST |
| 267 |
ALTOL(3) = DSQRT(ALTOL(1)**2+ALTOL(2)**2)/44.51 |
ALTOL(3) = DSQRT(ALTOL(1)**2+ALTOL(2)**2)/44.51 |
| 268 |
ALTOL(4) = ALTOL(3) |
ALTOL(4) = ALTOL(3) |
| 269 |
|
|
| 270 |
|
c$$$ print*,' -- ',(DAL(I),ALTOL(I),' - ',i=1,5) !>>>> new step! |
| 271 |
|
|
| 272 |
*---- check tolerances: |
*---- check tolerances: |
| 273 |
c$$$ DO I=1,5 |
c$$$ DO I=1,5 |
| 274 |
c$$$ if(TRKVERBOSE)print*,i,' -- ',DAL(I),ALTOL(I) !>>>> new step! |
c$$$ if(TRKVERBOSE)print*,i,' -- ',DAL(I),ALTOL(I) !>>>> new step! |
| 275 |
c$$$ ENDDO |
c$$$ ENDDO |
| 276 |
c$$$ print*,'chi2 -- ',DCHI2 |
c$$$ print*,'chi2 -- ',DCHI2 |
| 277 |
|
|
| 278 |
|
IF(ISTEP.LT.ISTEPMIN) GOTO 10 ! ***PP*** |
| 279 |
DO I=1,5 |
DO I=1,5 |
| 280 |
IF(ABS(DAL(I)).GT.ALTOL(I))GOTO 10 !>>>> new step! |
IF(ABS(DAL(I)).GT.ALTOL(I))GOTO 10 !>>>> new step! |
| 281 |
ENDDO |
ENDDO |
| 366 |
$ print*,'*** WARNING *** in mini n.dof = 0 (set to 1)' |
$ print*,'*** WARNING *** in mini n.dof = 0 (set to 1)' |
| 367 |
endif |
endif |
| 368 |
|
|
|
if(TRKDEBUG) print*,'mini2: -ok- ',istep,chi2,1./AL(5) |
|
|
|
|
| 369 |
* ------------------------------------ |
* ------------------------------------ |
| 370 |
* Reduced chi^2 |
* Reduced chi^2 |
| 371 |
CHI2 = CHI2/dble(ndof) |
CHI2 = CHI2/dble(ndof) |
| 374 |
|
|
| 375 |
11 CONTINUE |
11 CONTINUE |
| 376 |
|
|
| 377 |
|
if(TRKDEBUG) print*,'mini2: -ok- ',istep,chi2,1./AL(5) |
| 378 |
|
|
| 379 |
NSTEP=ISTEP ! ***PP*** |
NSTEP=ISTEP ! ***PP*** |
| 380 |
|
|
| 381 |
|
c$$$ print*,'>>>>> NSTEP = ',NSTEP |
| 382 |
|
|
| 383 |
RETURN |
RETURN |
| 384 |
END |
END |
| 385 |
|
|
| 445 |
* measured position of the cluster. |
* measured position of the cluster. |
| 446 |
* --------------------------------------------------------- |
* --------------------------------------------------------- |
| 447 |
CHI2=0. |
CHI2=0. |
| 448 |
DO I=1,nplanes |
DO I=1,nplanes |
| 449 |
IF(XGOOD(I).EQ.1.AND.YGOOD(I).EQ.0)THEN !X-cl |
IF(XGOOD(I).EQ.1.AND.YGOOD(I).EQ.0)THEN !X-cl |
| 450 |
BETA = (XM_B(I)-XM_A(I))/(YM_B(I)-YM_A(I)) |
BETA = (XM_B(I)-XM_A(I))/(YM_B(I)-YM_A(I)) |
| 451 |
ALFA = XM_A(I) - BETA * YM_A(I) |
ALFA = XM_A(I) - BETA * YM_A(I) |
| 472 |
+ *( XGOOD(I)*(1-YGOOD(I)) ) |
+ *( XGOOD(I)*(1-YGOOD(I)) ) |
| 473 |
+ +((XV(I)-XM(I))**2+(YV(I)-YM(I))**2)/RESY(i)**2 |
+ +((XV(I)-XM(I))**2+(YV(I)-YM(I))**2)/RESY(i)**2 |
| 474 |
+ *( (1-XGOOD(I))*YGOOD(I) ) |
+ *( (1-XGOOD(I))*YGOOD(I) ) |
| 475 |
|
c$$$ print*,(XV(I)-XM(I))**2/RESX(i)**2 *( XGOOD(I)*YGOOD(I) ) |
| 476 |
|
c$$$ print*,(YV(I)-YM(I))**2/RESY(i)**2 *( YGOOD(I)*XGOOD(I) ) |
| 477 |
|
c$$$ print*,((XV(I)-XM(I))**2+(YV(I)-YM(I))**2)/RESX(i)**2 |
| 478 |
|
c$$$ + *( XGOOD(I)*(1-YGOOD(I)) ) |
| 479 |
|
c$$$ print*,((XV(I)-XM(I))**2+(YV(I)-YM(I))**2)/RESY(i)**2 |
| 480 |
|
c$$$ + *( (1-XGOOD(I))*YGOOD(I) ) |
| 481 |
|
c$$$ print*,XV(I),XM(I),XGOOD(I) |
| 482 |
|
c$$$ print*,YV(I),YM(I),YGOOD(I) |
| 483 |
ENDDO |
ENDDO |
| 484 |
c print*,'CHISQ ',chi2 |
c$$$ print*,'CHISQ ',chi2 |
| 485 |
* ------------------------------------------------ |
* ------------------------------------------------ |
| 486 |
* |
* |
| 487 |
* calculation of derivatives (dX/dAL_fa and dY/dAL_fa) |
* calculation of derivatives (dX/dAL_fa and dY/dAL_fa) |
| 640 |
c |
c |
| 641 |
DIMENSION AL_P(5) |
DIMENSION AL_P(5) |
| 642 |
* |
* |
| 643 |
DO I=1,nplanes |
cpp DO I=1,nplanes |
| 644 |
ZV(I)=ZM(I) ! |
cpp ZV(I)=ZM(I) ! |
| 645 |
ENDDO |
cpp ENDDO |
| 646 |
* |
* |
| 647 |
* set parameters for GRKUTA |
* set parameters for GRKUTA |
| 648 |
* |
* |
| 657 |
IF(AL_P(5).NE.0.) VOUT(7)=DABS(1./AL_P(5)) |
IF(AL_P(5).NE.0.) VOUT(7)=DABS(1./AL_P(5)) |
| 658 |
IF(AL_P(5).EQ.0.) VOUT(7)=1.E8 |
IF(AL_P(5).EQ.0.) VOUT(7)=1.E8 |
| 659 |
|
|
| 660 |
c$$$ print*,'POSXY ',vout |
c$$$ print*,'POSXY (prima) ',vout |
| 661 |
|
|
| 662 |
DO I=1,nplanes |
DO I=1,nplanes |
| 663 |
step=vout(3)-zv(i) |
cpp step=vout(3)-zv(i) |
| 664 |
|
step=vout(3)-zm(i) |
| 665 |
10 DO J=1,7 |
10 DO J=1,7 |
| 666 |
VECT(J)=VOUT(J) |
VECT(J)=VOUT(J) |
| 667 |
VECTINI(J)=VOUT(J) |
VECTINI(J)=VOUT(J) |
| 693 |
GOTO 11 |
GOTO 11 |
| 694 |
ENDIF |
ENDIF |
| 695 |
|
|
| 696 |
|
|
| 697 |
* ----------------------------------------------- |
* ----------------------------------------------- |
| 698 |
* evaluate track coordinates |
* evaluate track coordinates |
| 699 |
100 XV(I)=VOUT(1) |
100 XV(I)=VOUT(1) |
| 703 |
AYV(I)=DATAN(VOUT(5)/VOUT(6))*180./ACOS(-1.) |
AYV(I)=DATAN(VOUT(5)/VOUT(6))*180./ACOS(-1.) |
| 704 |
* ----------------------------------------------- |
* ----------------------------------------------- |
| 705 |
|
|
| 706 |
|
IF(TRACKMODE.EQ.1) THEN |
| 707 |
|
* ----------------------------------------------- |
| 708 |
|
* change of energy by bremsstrahlung for electrons |
| 709 |
|
VOUT(7) = VOUT(7) * 0.997 !0.9968 |
| 710 |
|
* ----------------------------------------------- |
| 711 |
|
ENDIF |
| 712 |
|
|
| 713 |
ENDDO |
ENDDO |
| 714 |
|
|
| 715 |
|
c$$$ print*,'POSXY (dopo) ',vout |
| 716 |
|
|
| 717 |
|
|
| 718 |
RETURN |
RETURN |
| 719 |
END |
END |
| 720 |
|
|
| 755 |
RESY(IP) = 1000. !12.d-4 |
RESY(IP) = 1000. !12.d-4 |
| 756 |
XGOOD(IP) = 0 |
XGOOD(IP) = 0 |
| 757 |
YGOOD(IP) = 0 |
YGOOD(IP) = 0 |
| 758 |
|
DEDXTRK_X(IP) = 0 |
| 759 |
|
DEDXTRK_Y(IP) = 0 |
| 760 |
|
AXV(IP) = 0 |
| 761 |
|
AYV(IP) = 0 |
| 762 |
|
XV(IP) = -100 |
| 763 |
|
YV(IP) = -100 |
| 764 |
enddo |
enddo |
| 765 |
|
|
| 766 |
return |
return |
| 833 |
ENDDO |
ENDDO |
| 834 |
IFLAG=0 !no debug mode |
IFLAG=0 !no debug mode |
| 835 |
CALL TRICIRCLE(NP,XP,ZP,AP,RP,CHI,XC,ZC,RADIUS,IFLAG) |
CALL TRICIRCLE(NP,XP,ZP,AP,RP,CHI,XC,ZC,RADIUS,IFLAG) |
| 836 |
c print*,' circle: ',XC,ZC,RADIUS,' --- ',CHI,IFLAG |
|
| 837 |
|
c$$$ print*,' circle: ',XC,ZC,RADIUS,' --- ',CHI,IFLAG |
| 838 |
|
c$$$ print*,' XP ',(xp(i),i=1,np) |
| 839 |
|
c$$$ print*,' ZP ',(zp(i),i=1,np) |
| 840 |
|
c$$$ print*,' AP ',(ap(i),i=1,np) |
| 841 |
|
c$$$ print*,' XP ',(rp(i),i=1,np) |
| 842 |
|
|
| 843 |
IF(IFLAG.NE.0)GOTO 10 !straigth fit |
IF(IFLAG.NE.0)GOTO 10 !straigth fit |
| 844 |
if(CHI.gt.100)GOTO 10 !straigth fit |
c if(CHI.gt.100)GOTO 10 !straigth fit |
| 845 |
ARG = RADIUS**2-(ZINI-ZC)**2 |
ARG = RADIUS**2-(ZINI-ZC)**2 |
| 846 |
IF(ARG.LT.0)GOTO 10 !straigth fit |
IF(ARG.LT.0)GOTO 10 !straigth fit |
| 847 |
DC = SQRT(ARG) |
DC = SQRT(ARG) |
| 851 |
DEF=100./(RADIUS*0.3*0.43) |
DEF=100./(RADIUS*0.3*0.43) |
| 852 |
IF(XC.GT.0)DEF=-DEF |
IF(XC.GT.0)DEF=-DEF |
| 853 |
|
|
| 854 |
|
|
| 855 |
|
|
| 856 |
IF(ABS(X0).GT.30)THEN |
IF(ABS(X0).GT.30)THEN |
| 857 |
PRINT*,'STRANGE GUESS: XC,ZC,R ',XC,ZC,RADIUS |
c$$$ PRINT*,'STRANGE GUESS: XC,ZC,R ',XC,ZC,RADIUS |
| 858 |
$ ,' - CHI ',CHI,' - X0,AX,DEF ',X0,AX,DEF |
c$$$ $ ,' - CHI ',CHI,' - X0,AX,DEF ',X0,AX,DEF |
| 859 |
GOTO 10 !straigth fit |
GOTO 10 !straigth fit |
| 860 |
ENDIF |
ENDIF |
| 861 |
GOTO 20 !guess is ok |
GOTO 20 !guess is ok |
| 899 |
AL(2) = Y0 |
AL(2) = Y0 |
| 900 |
tath = sqrt(AY**2+AX**2) |
tath = sqrt(AY**2+AX**2) |
| 901 |
AL(3) = tath/sqrt(1+tath**2) |
AL(3) = tath/sqrt(1+tath**2) |
| 902 |
IF(AX.NE.0)THEN |
c$$$ IF(AX.NE.0)THEN |
| 903 |
AL(4)= atan(AY/AX) |
c$$$ AL(4)= atan(AY/AX) |
| 904 |
ELSE |
c$$$ ELSE |
| 905 |
AL(4) = acos(-1.)/2 |
c$$$ AL(4) = acos(-1.)/2 |
| 906 |
IF(AY.LT.0)AL(4) = AL(4)+acos(-1.) |
c$$$ IF(AY.LT.0)AL(4) = AL(4)+acos(-1.) |
| 907 |
|
c$$$ ENDIF |
| 908 |
|
c$$$ IF(AX.LT.0)AL(4)= acos(-1.)+ AL(4) |
| 909 |
|
c$$$ AL(4) = -acos(-1.) + AL(4) !from incidence direction to tracking ref.sys. |
| 910 |
|
|
| 911 |
|
c$$$ AL(4) = 0. |
| 912 |
|
c$$$ IF(AX.NE.0.AND.AY.NE.0)THEN |
| 913 |
|
c$$$ AL(4)= atan(AY/AX) |
| 914 |
|
c$$$ ELSEIF(AY.EQ.0)THEN |
| 915 |
|
c$$$ AL(4) = 0. |
| 916 |
|
c$$$ IF(AX.LT.0)AL(4) = AL(4)+acos(-1.) |
| 917 |
|
c$$$ ELSEIF(AX.EQ.0)THEN |
| 918 |
|
c$$$ AL(4) = acos(-1.)/2 |
| 919 |
|
c$$$ IF(AY.LT.0)AL(4) = AL(4)+acos(-1.) |
| 920 |
|
c$$$ ENDIF |
| 921 |
|
c$$$ IF(AX.LT.0)AL(4)= acos(-1.)+ AL(4) |
| 922 |
|
c$$$ AL(4) = -acos(-1.) + AL(4) !from incidence direction to tracking ref.sys. |
| 923 |
|
|
| 924 |
|
c$$$ AL(4)=0. |
| 925 |
|
c$$$ IF( AX.NE.0.OR.AY.NE.0. ) THEN |
| 926 |
|
c$$$ AL(4) = ASIN(AY/SQRT(AX**2+AY**2)) |
| 927 |
|
c$$$ IF(AX.LT.0.) AL(4) = ACOS(-1.0)-AL(4) |
| 928 |
|
c$$$ ENDIF |
| 929 |
|
|
| 930 |
|
AL(4)=0. |
| 931 |
|
IF( AX.NE.0.OR.AY.NE.0. ) THEN |
| 932 |
|
AL(4) = ASIN(AY/SQRT(AX**2+AY**2)) |
| 933 |
|
IF(AX.LT.0.AND.AY.GE.0) AL(4) = ACOS(-1.0)-AL(4) |
| 934 |
|
IF(AX.LT.0.AND.AY.LT.0) AL(4) = -ACOS(-1.0)-AL(4) |
| 935 |
ENDIF |
ENDIF |
| 936 |
IF(AX.LT.0)AL(4)= acos(-1.)+ AL(4) |
IF(AY.GT.0.) AL(4) = AL(4)-ACOS(-1.0) |
| 937 |
AL(4) = -acos(-1.) + AL(4) !from incidence direction to tracking rs |
IF(AY.LE.0.) AL(4) = AL(4)+ACOS(-1.0) |
| 938 |
|
|
| 939 |
AL(5) = DEF |
AL(5) = DEF |
| 940 |
|
|
| 941 |
c print*,' guess: ',(al(i),i=1,5) |
c print*,' guess: ',(al(i),i=1,5) |