| 1 |
***************************************************************************** |
| 2 |
INTEGER FUNCTION CALOL2CM() |
| 3 |
c |
| 4 |
IMPLICIT NONE |
| 5 |
C |
| 6 |
INCLUDE 'INTEST.TXT' |
| 7 |
C |
| 8 |
REAL PIANO(22), VARFIT(2) |
| 9 |
REAL SHIFT |
| 10 |
REAL TG(2), BAR(2,NPLA) |
| 11 |
REAL DISTX, DISTY, Y(NPLA), YY(NPLA) |
| 12 |
REAL RIG, RMASS |
| 13 |
REAL CHECK, ENER, CX, CY |
| 14 |
REAL EINF, ESUP,ENPLANEX,ENPLANEY,TENPLAX,TENPLAY |
| 15 |
REAL hmemor(9000000) |
| 16 |
c |
| 17 |
INTEGER gtr |
| 18 |
INTEGER j, m, nn, i |
| 19 |
INTEGER IBAR(2,NPLA), NPFIT(2) |
| 20 |
INTEGER Iquest(100), IWPL(2),CHTRACK |
| 21 |
c |
| 22 |
COMMON / TAGLIOEN / EINF, ESUP, ENER(2) |
| 23 |
SAVE / TAGLIOEN / |
| 24 |
C |
| 25 |
COMMON / SHIFT / SHIFT |
| 26 |
SAVE / SHIFT / |
| 27 |
C |
| 28 |
COMMON / ANGOLO / BAR, IBAR |
| 29 |
SAVE / ANGOLO / |
| 30 |
C |
| 31 |
COMMON / WHERE / CX, CY, PIANO |
| 32 |
SAVE / WHERE / |
| 33 |
C |
| 34 |
COMMON / GENERAL / RIG, RMASS |
| 35 |
SAVE / GENERAL / |
| 36 |
C |
| 37 |
COMMON / CH / CHECK |
| 38 |
SAVE / CH / |
| 39 |
C |
| 40 |
COMMON / CALOFIT / VARFIT, NPFIT, IWPL,CHTRACK |
| 41 |
SAVE / CALOFIT / |
| 42 |
C |
| 43 |
COMMON / pawcd / hmemor |
| 44 |
save / pawcd / |
| 45 |
C |
| 46 |
Common / QUESTd / Iquest |
| 47 |
save / questd / |
| 48 |
C |
| 49 |
C Begin ! |
| 50 |
C |
| 51 |
CALOL2CM = 0; |
| 52 |
RMASS = 0.938 |
| 53 |
C |
| 54 |
C Z position of Y planes, Y1 = 0., Y2 = -8.09, Y3 = -18.18, ... |
| 55 |
C |
| 56 |
PIANO(1) = 0. |
| 57 |
DO I = 2, 22 |
| 58 |
IF ( MOD(I,2).EQ.0 ) THEN |
| 59 |
PIANO(I) = PIANO(I-1) - 8.09 |
| 60 |
ELSE |
| 61 |
PIANO(I) = PIANO(I-1) - 10.09 |
| 62 |
ENDIF |
| 63 |
ENDDO |
| 64 |
C |
| 65 |
CALL VZERO(DEXY,2*LENSEV) |
| 66 |
CALL VZERO(BAR,2*NPLA) |
| 67 |
CALL VZERO(IBAR,2*NPLA) |
| 68 |
CALL VZERO(CBAR,2*NPLA) |
| 69 |
CALL VZERO(CIBAR,2*NPLA) |
| 70 |
CALL VZERO(QQ,4) |
| 71 |
CALL VZERO(Y,NPLA) |
| 72 |
CALL VZERO(YY,NPLA) |
| 73 |
VARFIT(1) = 0. |
| 74 |
VARFIT(2) = 0. |
| 75 |
NPFIT(1) = 0. |
| 76 |
NPFIT(2) = 0. |
| 77 |
VARCFIT(1) = 0. |
| 78 |
VARCFIT(2) = 0. |
| 79 |
NPCFIT(1) = 0. |
| 80 |
NPCFIT(2) = 0. |
| 81 |
ELEN = 0. |
| 82 |
SELEN = 0. |
| 83 |
NSTRIP = 0. |
| 84 |
QTOT = 0. |
| 85 |
NX22 = 0. |
| 86 |
QX22 = 0. |
| 87 |
QMAX = 0. |
| 88 |
GTR = 0 |
| 89 |
CHTRACK = 0 |
| 90 |
C |
| 91 |
DISTX = 0. |
| 92 |
DISTY = 0. |
| 93 |
C |
| 94 |
PLANEMAX(1) = 0 |
| 95 |
PLANEMAX(2) = 0 |
| 96 |
TENPLAX = 0. |
| 97 |
TENPLAY = 0. |
| 98 |
C |
| 99 |
IF (GOOD2.EQ.0.AND.TRIGTY.LT.2) goto 9696 |
| 100 |
C |
| 101 |
C CALCULATE QTOT, NSTRIP, QQ, NX22, QX22, QMAX AND PLANEMAX |
| 102 |
C |
| 103 |
DO I = 1,22 |
| 104 |
ENPLANEY = 0. |
| 105 |
ENPLANEX = 0. |
| 106 |
DO J = 1,96 |
| 107 |
IF ( MOD(I,2).NE.0 ) THEN |
| 108 |
IF ( ESTRIP(2,I,J).GT.EMIN ) THEN |
| 109 |
DEXY(2,I,J) = ESTRIP(2,I,J) |
| 110 |
ENPLANEY = ENPLANEY + DEXY(2,I,J) |
| 111 |
NSTRIP = NSTRIP + 1. |
| 112 |
QTOT = QTOT + DEXY(2,I,J) |
| 113 |
IF (I.LT.11) QQ(1) = QQ(1) + DEXY(2,I,J) |
| 114 |
ENDIF |
| 115 |
IF ( ESTRIP(1,I,J).GT.EMIN ) THEN |
| 116 |
C IF ( ESTRIP(1,I+1,J).GT.EMIN ) THEN |
| 117 |
C |
| 118 |
c print *,' i ',i,' i + 1 ',I+1 |
| 119 |
C DEXY(1,I,J) = ESTRIP(1,I+1,J) |
| 120 |
DEXY(1,I,J) = ESTRIP(1,I,J) |
| 121 |
C |
| 122 |
ENPLANEX = ENPLANEX + DEXY(1,I,J) |
| 123 |
NSTRIP = NSTRIP + 1. |
| 124 |
QTOT = QTOT + DEXY(1,I,J) |
| 125 |
if (i.lt.11) QQ(2) = QQ(2) + DEXY(1,I,J) |
| 126 |
c IF (I.EQ.21) THEN |
| 127 |
c NX22 = NX22 + 1. |
| 128 |
c QX22 = QX22 + DEXY(1,I,J) |
| 129 |
c ENDIF |
| 130 |
ENDIF |
| 131 |
ENDIF |
| 132 |
IF ( MOD(I,2).EQ.0 ) THEN |
| 133 |
IF (ESTRIP(2,I,J).GT.EMIN) THEN |
| 134 |
DEXY(2,I,J) = ESTRIP(2,I,J) |
| 135 |
ENPLANEY = ENPLANEY + DEXY(2,I,J) |
| 136 |
NSTRIP = NSTRIP + 1. |
| 137 |
QTOT = QTOT + DEXY(2,I,J) |
| 138 |
if (i.lt.11) QQ(3) = QQ(3) + DEXY(2,I,J) |
| 139 |
ENDIF |
| 140 |
IF (ESTRIP(1,I,J).GT.EMIN) THEN |
| 141 |
C IF (ESTRIP(1,I-1,J).GT.EMIN) THEN |
| 142 |
C |
| 143 |
c print *,' i ',i,' i - 1 ',I-1 |
| 144 |
C DEXY(1,I,J) = ESTRIP(1,I-1,J) |
| 145 |
DEXY(1,I,J) = ESTRIP(1,I,J) |
| 146 |
C |
| 147 |
ENPLANEX = ENPLANEX + DEXY(1,I,J) |
| 148 |
NSTRIP = NSTRIP + 1. |
| 149 |
QTOT = QTOT + DEXY(1,I,J) |
| 150 |
IF (I.EQ.22) THEN |
| 151 |
NX22 = NX22 + 1. |
| 152 |
QX22 = QX22 + DEXY(1,I,J) |
| 153 |
ENDIF |
| 154 |
IF (I.LT.11) QQ(4) = QQ(4) + DEXY(1,I,J) |
| 155 |
ENDIF |
| 156 |
ENDIF |
| 157 |
C |
| 158 |
IF (DEXY(1,I,J).GT.QMAX) QMAX = DEXY(1,I,J) |
| 159 |
IF (DEXY(2,I,J).GT.QMAX) QMAX = DEXY(2,I,J) |
| 160 |
C |
| 161 |
ENDDO |
| 162 |
IF (ENPLANEX.GT.TENPLAX) THEN |
| 163 |
PLANEMAX(1) = I |
| 164 |
TENPLAX = ENPLANEX |
| 165 |
ENDIF |
| 166 |
IF (ENPLANEY.GT.TENPLAY) THEN |
| 167 |
PLANEMAX(2) = I |
| 168 |
TENPLAY = ENPLANEY |
| 169 |
ENDIF |
| 170 |
ENDDO |
| 171 |
C |
| 172 |
C FIT THE TRACK INSIDE THE CALORIMETER |
| 173 |
C |
| 174 |
if (GOOD2.EQ.1.OR.TRIGTY.GE.2) then |
| 175 |
CALL CLUSTER |
| 176 |
CALL DIRECTION(TG) |
| 177 |
NPCFIT(1) = NPFIT(1) |
| 178 |
NPCFIT(2) = NPFIT(2) |
| 179 |
C |
| 180 |
DO M = 1,2 |
| 181 |
C |
| 182 |
IF (NPCFIT(M).GE.2) THEN |
| 183 |
VARCFIT(M) = VARFIT(M) |
| 184 |
IF (M.EQ.1) THEN |
| 185 |
IMPX = (CX - XALIG)/10. |
| 186 |
TANX = TG(1) |
| 187 |
ELSE |
| 188 |
IMPY =( CY - YALIG)/10. |
| 189 |
TANY = TG(2) |
| 190 |
ENDIF |
| 191 |
C |
| 192 |
DO I = 1,NPLA |
| 193 |
NN = 1 |
| 194 |
C NN = 0 |
| 195 |
C IF (M.EQ.2) NN = 1 |
| 196 |
IF (MOD(I,2).EQ.NN) THEN |
| 197 |
SHIFT = +0.5 |
| 198 |
ELSE |
| 199 |
SHIFT = -0.5 |
| 200 |
ENDIF |
| 201 |
C |
| 202 |
IF (M.EQ.1) THEN |
| 203 |
DISTX = PIANO(I) - 5.81 |
| 204 |
Y(I) = DISTX * TG(1) + CX |
| 205 |
BAR(M,I) = Y(I) |
| 206 |
CBAR(M,I) = (Y(I) - XALIG)/10. |
| 207 |
C |
| 208 |
ELSE |
| 209 |
DISTY = PIANO(I) |
| 210 |
YY(I) = DISTY * TG(2) + CY |
| 211 |
BAR(M,I) = YY(I) |
| 212 |
CBAR(M,I) = (-YALIG + YY(I))/10. |
| 213 |
C |
| 214 |
ENDIF |
| 215 |
CALL LASTRISCIA(BAR(M,I),IBAR(M,I)) |
| 216 |
CIBAR(M,I) = IBAR(M,I) |
| 217 |
IF (ibar(m,i).EQ.-1) THEN |
| 218 |
CHTRACK = CHTRACK + 1 |
| 219 |
ELSE |
| 220 |
IWPL(M) = IWPL(M) + 1 |
| 221 |
ENDIF |
| 222 |
ENDDO |
| 223 |
ENDIF |
| 224 |
C |
| 225 |
ENDDO |
| 226 |
ELSE |
| 227 |
GOTO 9696 |
| 228 |
ENDIF |
| 229 |
C |
| 230 |
C CALCULATE ELEN AND SELEN |
| 231 |
C |
| 232 |
ELEN = 40.82 * QTOT * 1.06 * 1E-4 |
| 233 |
IF (ELEN.GT.0.) THEN |
| 234 |
SELEN = ELEN * (0.01183 + 0.121 / SQRT(ELEN)) |
| 235 |
ELSE |
| 236 |
SELEN = 0. |
| 237 |
ENDIF |
| 238 |
C |
| 239 |
9696 CONTINUE |
| 240 |
C |
| 241 |
45 continue |
| 242 |
|
| 243 |
50 continue |
| 244 |
|
| 245 |
return |
| 246 |
END |
| 247 |
|
| 248 |
|
Parent Directory
| 
Revision Log