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***************************************************************************** |
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INTEGER FUNCTION CALOL2CM() |
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c |
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IMPLICIT NONE |
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C |
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INCLUDE 'INTEST.TXT' |
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C |
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REAL PIANO(NPLAV), VARFIT(2) |
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REAL SHIFT |
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REAL TG(2), BAR(2,NPLAV) |
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REAL DISTX, DISTY, Y(NPLAV), YY(NPLAV) |
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REAL RIG, RMASS |
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REAL CHECK, ENER, CX, CY |
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REAL EINF, ESUP,ENPLANEX,ENPLANEY,TENPLAX,TENPLAY |
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REAL hmemor(9000000) |
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c |
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INTEGER gtr |
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INTEGER j, m, nn, i |
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INTEGER IBAR(2,NPLAV), NPFIT(2) |
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INTEGER Iquest(100), IWPL(2),CHTRACK |
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c |
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COMMON / TAGLIOEN / EINF, ESUP, ENER(2) |
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SAVE / TAGLIOEN / |
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C |
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COMMON / SHIFT / SHIFT |
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SAVE / SHIFT / |
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C |
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COMMON / ANGOLO / BAR, IBAR |
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SAVE / ANGOLO / |
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C |
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COMMON / WHERE / CX, CY, PIANO |
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SAVE / WHERE / |
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C |
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COMMON / GENERAL / RIG, RMASS |
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SAVE / GENERAL / |
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C |
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COMMON / CH / CHECK |
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SAVE / CH / |
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C |
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COMMON / CALOFIT / VARFIT, NPFIT, IWPL,CHTRACK |
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SAVE / CALOFIT / |
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C |
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COMMON / pawcd / hmemor |
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save / pawcd / |
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C |
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Common / QUESTd / Iquest |
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save / questd / |
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C |
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C Begin ! |
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C |
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CALOL2CM = 0; |
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RMASS = 0.938 |
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C |
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C Z position of Y planes, Y1 = 0., Y2 = -8.09, Y3 = -18.18, ... |
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C |
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c print *,'NPLA IS ',NPLA |
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PIANO(1) = 0. |
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DO I = 2, NPLA |
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IF ( MOD(I,2).EQ.0 ) THEN |
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PIANO(I) = PIANO(I-1) - 8.09 |
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ELSE |
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PIANO(I) = PIANO(I-1) - 10.09 |
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ENDIF |
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ENDDO |
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C |
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CALL VZERO(DEXY,2*LENSEV) |
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CALL VZERO(BAR,2*NPLAV) |
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CALL VZERO(IBAR,2*NPLAV) |
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CALL VZERO(CBAR,2*NPLAV) |
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CALL VZERO(CIBAR,2*NPLAV) |
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CALL VZERO(QQ,4) |
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CALL VZERO(Y,NPLAV) |
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CALL VZERO(YY,NPLAV) |
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VARFIT(1) = 0. |
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VARFIT(2) = 0. |
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NPFIT(1) = 0 |
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NPFIT(2) = 0 |
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VARCFIT(1) = 0. |
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VARCFIT(2) = 0. |
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NPCFIT(1) = 0 |
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NPCFIT(2) = 0 |
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ELEN = 0. |
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SELEN = 0. |
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NSTRIP = 0. |
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QTOT = 0. |
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NX22 = 0. |
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QX22 = 0. |
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QMAX = 0. |
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GTR = 0 |
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CHTRACK = 0 |
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C |
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DISTX = 0. |
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DISTY = 0. |
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C |
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PLANEMAX(1) = 0 |
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PLANEMAX(2) = 0 |
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TENPLAX = 0. |
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TENPLAY = 0. |
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C |
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IF (GOOD2.EQ.0.AND.TRIGTY.LT.2) goto 9696 |
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C |
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C CALCULATE QTOT, NSTRIP, QQ, NX22, QX22, QMAX AND PLANEMAX |
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C |
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DO I = 1,NPLA |
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ENPLANEY = 0. |
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ENPLANEX = 0. |
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DO J = 1,96 |
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c if ( ESTRIP(1,I,J).gt.0) |
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c & print *,' I ',I,' J ',J,' ES1 ',ESTRIP(1,I,J) |
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c if ( ESTRIP(2,I,J).gt.0) |
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c & print *,' I ',I,' J ',J,' ES2 ',ESTRIP(2,I,J) |
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IF ( MOD(I,2).NE.0 ) THEN |
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IF ( ESTRIP(2,I,J).GT.EMIN ) THEN |
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DEXY(2,I,J) = ESTRIP(2,I,J) |
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ENPLANEY = ENPLANEY + DEXY(2,I,J) |
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NSTRIP = NSTRIP + 1. |
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QTOT = QTOT + DEXY(2,I,J) |
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IF (I.LT.11) QQ(1) = QQ(1) + DEXY(2,I,J) |
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ENDIF |
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IF ( ESTRIP(1,I,J).GT.EMIN ) THEN |
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C IF ( ESTRIP(1,I+1,J).GT.EMIN ) THEN |
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C |
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c print *,' i ',i,' i + 1 ',I+1 |
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C DEXY(1,I,J) = ESTRIP(1,I+1,J) |
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DEXY(1,I,J) = ESTRIP(1,I,J) |
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C |
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ENPLANEX = ENPLANEX + DEXY(1,I,J) |
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NSTRIP = NSTRIP + 1. |
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QTOT = QTOT + DEXY(1,I,J) |
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if (i.lt.11) QQ(2) = QQ(2) + DEXY(1,I,J) |
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c IF (I.EQ.21) THEN |
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c NX22 = NX22 + 1. |
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c QX22 = QX22 + DEXY(1,I,J) |
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c ENDIF |
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ENDIF |
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ENDIF |
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IF ( MOD(I,2).EQ.0 ) THEN |
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IF (ESTRIP(2,I,J).GT.EMIN) THEN |
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DEXY(2,I,J) = ESTRIP(2,I,J) |
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ENPLANEY = ENPLANEY + DEXY(2,I,J) |
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NSTRIP = NSTRIP + 1. |
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QTOT = QTOT + DEXY(2,I,J) |
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if (i.lt.11) QQ(3) = QQ(3) + DEXY(2,I,J) |
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ENDIF |
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IF (ESTRIP(1,I,J).GT.EMIN) THEN |
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C IF (ESTRIP(1,I-1,J).GT.EMIN) THEN |
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C |
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c print *,' i ',i,' i - 1 ',I-1 |
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C DEXY(1,I,J) = ESTRIP(1,I-1,J) |
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DEXY(1,I,J) = ESTRIP(1,I,J) |
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C |
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ENPLANEX = ENPLANEX + DEXY(1,I,J) |
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NSTRIP = NSTRIP + 1. |
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QTOT = QTOT + DEXY(1,I,J) |
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IF (I.EQ.NPLA) THEN |
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NX22 = NX22 + 1. |
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QX22 = QX22 + DEXY(1,I,J) |
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ENDIF |
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IF (I.LT.11) QQ(4) = QQ(4) + DEXY(1,I,J) |
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ENDIF |
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ENDIF |
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C |
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IF (DEXY(1,I,J).GT.QMAX) QMAX = DEXY(1,I,J) |
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IF (DEXY(2,I,J).GT.QMAX) QMAX = DEXY(2,I,J) |
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C |
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ENDDO |
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IF (ENPLANEX.GT.TENPLAX) THEN |
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PLANEMAX(1) = I |
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TENPLAX = ENPLANEX |
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ENDIF |
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IF (ENPLANEY.GT.TENPLAY) THEN |
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PLANEMAX(2) = I |
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TENPLAY = ENPLANEY |
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ENDIF |
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ENDDO |
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C |
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C FIT THE TRACK INSIDE THE CALORIMETER |
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C |
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if (GOOD2.EQ.1.OR.TRIGTY.GE.2) then |
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c print *,' CALL CLUSTER ' |
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CALL CLUSTER |
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c print *,' CALL DIRECTION ' |
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CALL DIRECTION(TG) |
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NPCFIT(1) = NPFIT(1) |
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NPCFIT(2) = NPFIT(2) |
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C |
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DO M = 1,2 |
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C |
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IF (NPCFIT(M).GE.2) THEN |
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VARCFIT(M) = VARFIT(M) |
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IF (M.EQ.1) THEN |
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IMPX = (CX - XALIG)/10. |
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TANX = TG(1) |
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ELSE |
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IMPY =( CY - YALIG)/10. |
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TANY = TG(2) |
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ENDIF |
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C |
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DO I = 1,NPLA |
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C NN = 1 |
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NN = 0 |
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C IF (M.EQ.2) NN = 1 |
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IF (MOD(I,2).EQ.NN) THEN |
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IF (REVERSE.EQ.0) THEN |
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SHIFT = -0.5 |
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ELSE |
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SHIFT = +0.5 |
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ENDIF |
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ELSE |
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IF (REVERSE.EQ.0) THEN |
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SHIFT = +0.5 |
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ELSE |
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SHIFT = -0.5 |
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ENDIF |
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ENDIF |
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C |
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IF (M.EQ.1) THEN |
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DISTX = PIANO(I) - 5.81 |
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c print *,'C X PLANE I= ',I,' Z = ',DISTX+ZALIG |
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Y(I) = DISTX * TG(1) + CX |
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BAR(M,I) = Y(I) |
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CBAR(M,I) = (Y(I) - XALIG)/10. |
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C |
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ELSE |
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DISTY = PIANO(I) |
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c print *,'C Y PLANE I= ',I,' Z = ',DISTY+ZALIG |
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YY(I) = DISTY * TG(2) + CY |
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BAR(M,I) = YY(I) |
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CBAR(M,I) = (-YALIG + YY(I))/10. |
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C |
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ENDIF |
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CALL LASTRISCIA(BAR(M,I),IBAR(M,I)) |
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CIBAR(M,I) = IBAR(M,I) |
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IF (ibar(m,i).EQ.-1) THEN |
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CHTRACK = CHTRACK + 1 |
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ELSE |
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IWPL(M) = IWPL(M) + 1 |
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ENDIF |
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ENDDO |
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ENDIF |
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C |
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ENDDO |
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ELSE |
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GOTO 9696 |
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ENDIF |
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C |
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C CALCULATE ELEN AND SELEN |
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C |
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c ELEN = 40.82 * QTOT * 1.06 * 1E-4 |
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C ELEN = 260. * QTOT |
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ELEN = QTOT / 260. |
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IF (ELEN.GT.0.) THEN |
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SELEN = ELEN * (0.01183 + 0.121 / SQRT(ELEN)) |
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ELSE |
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SELEN = 0. |
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ENDIF |
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C |
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9696 CONTINUE |
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C |
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c 45 continue |
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|
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c 50 continue |
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|
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return |
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END |
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|
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