| 23 |
c common/dbg/DEBUG |
c common/dbg/DEBUG |
| 24 |
|
|
| 25 |
parameter (dinf=1.d15) !just a huge number... |
parameter (dinf=1.d15) !just a huge number... |
| 26 |
|
parameter (dinfneg=-dinf) ! just a huge negative number... |
| 27 |
c------------------------------------------------------------------------ |
c------------------------------------------------------------------------ |
| 28 |
c variables used in the tracking procedure (mini and its subroutines) |
c variables used in the tracking procedure (mini and its subroutines) |
| 29 |
c |
c |
| 45 |
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 |
| 46 |
c DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
c DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
| 47 |
DATA ALMAX/dinf,dinf,1.,dinf,dinf/ !limits on alpha vector components |
DATA ALMAX/dinf,dinf,1.,dinf,dinf/ !limits on alpha vector components |
| 48 |
DATA ALMIN/-dinf,-dinf,-1.,-dinf,-dinf/ !" |
DATA ALMIN/dinfneg,dinfneg,-1.,dinfneg,dinfneg/ !" |
| 49 |
|
|
| 50 |
c$$$ DIMENSION DAL(5) !increment of vector alfa |
c$$$ DIMENSION DAL(5) !increment of vector alfa |
| 51 |
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 |
| 68 |
|
|
| 69 |
c LOGICAL TRKDEBUG,TRKVERBOSE |
c LOGICAL TRKDEBUG,TRKVERBOSE |
| 70 |
c COMMON/TRKD/TRKDEBUG,TRKVERBOSE |
c COMMON/TRKD/TRKDEBUG,TRKVERBOSE |
| 71 |
LOGICAL TRKDEBUG,TRKVERBOSE,STUDENT |
LOGICAL TRKDEBUG,TRKVERBOSE,STUDENT,FIRSTSTEPS,FIRSTSTUDENT |
| 72 |
COMMON/TRKD/TRKDEBUG,TRKVERBOSE |
COMMON/TRKD/TRKDEBUG,TRKVERBOSE |
| 73 |
|
|
| 74 |
DIMENSION AL0(5) |
DIMENSION AL0(5) |
| 75 |
LOGICAL SUCCESS_NEW,SUCCESS_OLD |
LOGICAL SUCCESS_NEW,SUCCESS_OLD |
| 76 |
|
|
| 77 |
|
c$$$ PRINT*,'==========' ! TEST |
| 78 |
|
c$$$ PRINT*,'START MINI' ! TEST |
| 79 |
|
c$$$ PRINT*,'==========' ! TEST |
| 80 |
|
|
| 81 |
* |
* |
| 82 |
* define kind of minimization (0x=chi2+gaussian or 1x=likelihood+student) |
* define kind of minimization (0x=chi2+gaussian or 1x=likelihood+student) |
| 83 |
* |
* |
| 84 |
STUDENT = .false. |
STUDENT = .false. |
| 85 |
|
FIRSTSTEPS = .true. |
| 86 |
|
FIRSTSTUDENT = .true. |
| 87 |
IF(MOD(INT(TRACKMODE/10),10).EQ.1) STUDENT = .true. |
IF(MOD(INT(TRACKMODE/10),10).EQ.1) STUDENT = .true. |
| 88 |
|
|
| 89 |
IF(IPRINT.EQ.1) THEN |
IF(IPRINT.EQ.1) THEN |
| 102 |
* ---------------------------------------------------------- |
* ---------------------------------------------------------- |
| 103 |
AVRESX = RESXAV |
AVRESX = RESXAV |
| 104 |
AVRESY = RESYAV |
AVRESY = RESYAV |
| 105 |
|
NX = 0 !EM GCC4.7 |
| 106 |
|
NY = 0 !EM GCC4.7 |
| 107 |
DO IP=1,6 |
DO IP=1,6 |
| 108 |
IF( XGOOD(IP).EQ.1 )THEN |
IF( XGOOD(IP).EQ.1 )THEN |
| 109 |
NX=NX+1 |
NX=NX+1!EM GCC4.7 |
| 110 |
AVRESX=AVRESX+RESX(IP) |
AVRESX=AVRESX+RESX(IP) |
| 111 |
ENDIF |
ENDIF |
|
IF(NX.NE.0)AVRESX=AVRESX/NX |
|
| 112 |
IF( YGOOD(IP).EQ.1 )THEN |
IF( YGOOD(IP).EQ.1 )THEN |
| 113 |
NY=NY+1 |
NY=NY+1!EM GCC4.7 |
| 114 |
AVRESY=AVRESY+RESY(IP) |
AVRESY=AVRESY+RESY(IP) |
| 115 |
ENDIF |
ENDIF |
|
IF(NX.NE.0)AVRESY=AVRESY/NY |
|
| 116 |
ENDDO |
ENDDO |
| 117 |
|
IF(NX.NE.0.0)AVRESX=AVRESX/NX |
| 118 |
|
IF(NY.NE.0.0)AVRESY=AVRESY/NY |
| 119 |
|
|
| 120 |
* ---------------------------------------------------------- |
* ---------------------------------------------------------- |
| 121 |
* define ALTOL(5) ---> tolerances on state vector |
* define ALTOL(5) ---> tolerances on state vector |
| 142 |
CHI2=0 |
CHI2=0 |
| 143 |
|
|
| 144 |
if(TRKDEBUG) print*,'guess: ',al |
if(TRKDEBUG) print*,'guess: ',al |
| 145 |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,1./AL(5) |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,AL(5) |
| 146 |
|
|
| 147 |
* |
* |
| 148 |
* ----------------------- |
* ----------------------- |
| 154 |
* **** Chi2+gaussian minimization |
* **** Chi2+gaussian minimization |
| 155 |
* ------------------------------- |
* ------------------------------- |
| 156 |
|
|
| 157 |
IF(.NOT.STUDENT) THEN |
IF((.NOT.STUDENT).OR.FIRSTSTEPS) THEN |
| 158 |
|
|
| 159 |
|
IF(ISTEP.GE.3) FIRSTSTEPS = .false. |
| 160 |
|
|
| 161 |
CALL CHISQ(IFLAG,JFAIL) !chi^2 and its derivatives |
CALL CHISQ(IFLAG,JFAIL) !chi^2 and its derivatives |
| 162 |
IF(JFAIL.NE.0) THEN |
IF(JFAIL.NE.0) THEN |
| 252 |
ENDDO |
ENDDO |
| 253 |
ENDIF |
ENDIF |
| 254 |
|
|
| 255 |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,1./AL(5) |
if(TRKDEBUG) print*,'mini2: step ',istep,chi2,AL(5) |
| 256 |
|
|
| 257 |
c$$$ PRINT*,'DAL ',(DAL(K),K=1,5) |
c$$$ PRINT*,'DAL ',(DAL(K),K=1,5) |
| 258 |
c$$$ PRINT*,'CHI2DOLD ',(CHI2DOLD(K),K=1,5) |
c$$$ PRINT*,'CHI2DOLD ',(CHI2DOLD(K),K=1,5) |
| 264 |
* **** Likelihood+Student minimization |
* **** Likelihood+Student minimization |
| 265 |
* ------------------------------- |
* ------------------------------- |
| 266 |
|
|
| 267 |
IF(STUDENT) THEN |
IF(STUDENT.AND.(.NOT.FIRSTSTEPS)) THEN |
| 268 |
|
|
| 269 |
|
IF(FIRSTSTUDENT) THEN |
| 270 |
|
FIRSTSTUDENT = .false. |
| 271 |
|
ISTEP = 1 |
| 272 |
|
ENDIF |
| 273 |
|
|
| 274 |
CALL CHISQSTT(1,JFAIL) |
CALL CHISQSTT(1,JFAIL) |
| 275 |
DO I=1,5 |
DO I=1,5 |
| 276 |
DAL(I)=0. |
DAL(I)=0. |
| 304 |
FC = CHI2 |
FC = CHI2 |
| 305 |
EC = 0. |
EC = 0. |
| 306 |
|
|
| 307 |
|
ICOUNT = 0 |
| 308 |
100 CONTINUE |
100 CONTINUE |
| 309 |
|
ICOUNT = ICOUNT+1 |
| 310 |
|
|
| 311 |
DO I=1,5 |
DO I=1,5 |
| 312 |
AL0(I)=AL(I) |
AL0(I)=AL(I) |
| 313 |
ENDDO |
ENDDO |
| 351 |
ENDIF |
ENDIF |
| 352 |
c$$$ E = BETA*E |
c$$$ E = BETA*E |
| 353 |
ENDIF |
ENDIF |
| 354 |
|
IF(ICOUNT.GT.20) GOTO 101 |
| 355 |
GOTO 100 |
GOTO 100 |
| 356 |
|
|
| 357 |
101 CONTINUE |
101 CONTINUE |
| 419 |
* --------------------------------------------- |
* --------------------------------------------- |
| 420 |
*------------------------------------------------------------* |
*------------------------------------------------------------* |
| 421 |
c$$$ ALTOL(5) = DSQRT(DELETA1**2+DELETA2**2*AL(5)**2)/FACT |
c$$$ ALTOL(5) = DSQRT(DELETA1**2+DELETA2**2*AL(5)**2)/FACT |
| 422 |
|
IF(FACT.EQ.0)THEN |
| 423 |
|
IFAIL=1 |
| 424 |
|
RETURN |
| 425 |
|
ENDIF |
| 426 |
ALTOL(5) = DSQRT((DELETA1*AVRESX)**2+DELETA2**2*AL(5)**2)/FACT |
ALTOL(5) = DSQRT((DELETA1*AVRESX)**2+DELETA2**2*AL(5)**2)/FACT |
| 427 |
ALTOL(1) = ALTOL(5)/DELETA1 |
ALTOL(1) = ALTOL(5)/DELETA1 |
| 428 |
ALTOL(2) = ALTOL(1) |
ALTOL(2) = ALTOL(1) |
| 559 |
* ------------------------------------ |
* ------------------------------------ |
| 560 |
* Reduced chi^2 |
* Reduced chi^2 |
| 561 |
CHI2 = CHI2/dble(ndof) |
CHI2 = CHI2/dble(ndof) |
|
|
|
| 562 |
c print*,'mini2: chi2 ',chi2 |
c print*,'mini2: chi2 ',chi2 |
| 563 |
|
|
| 564 |
11 CONTINUE |
11 CONTINUE |
| 565 |
|
|
| 566 |
if(TRKDEBUG) print*,'mini2: -ok- ',istep,chi2,1./AL(5) |
if(TRKDEBUG) print*,'mini2: -ok- ',istep,chi2,AL(5) |
| 567 |
|
|
| 568 |
NSTEP=ISTEP ! ***PP*** |
NSTEP=ISTEP ! ***PP*** |
| 569 |
|
|
| 1004 |
c$$$ print*,'POSXY (prima) ',vout |
c$$$ print*,'POSXY (prima) ',vout |
| 1005 |
|
|
| 1006 |
DO I=1,nplanes |
DO I=1,nplanes |
| 1007 |
cpp step=vout(3)-zv(i) |
c$$$ ipass = 0 ! TEST |
| 1008 |
step=vout(3)-zm(i) |
c$$$ PRINT *,'TRACKING -> START PLANE: ',I ! TEST |
| 1009 |
|
cPPP step=vout(3)-zm(i) |
| 1010 |
|
cPP step=(zm(i)-vout(3))/VOUT(6) |
| 1011 |
10 DO J=1,7 |
10 DO J=1,7 |
| 1012 |
VECT(J)=VOUT(J) |
VECT(J)=VOUT(J) |
| 1013 |
VECTINI(J)=VOUT(J) |
VECTINI(J)=VOUT(J) |
| 1014 |
ENDDO |
ENDDO |
| 1015 |
|
cPPP step=vect(3)-zm(i) |
| 1016 |
|
IF(VOUT(6).GE.0.) THEN |
| 1017 |
|
IFAIL=1 |
| 1018 |
|
if(TRKVERBOSE) |
| 1019 |
|
$ PRINT *,'posxy (grkuta): WARNING ===> backward track!!' |
| 1020 |
|
RETURN |
| 1021 |
|
ENDIF |
| 1022 |
|
step=(zm(i)-vect(3))/VOUT(6) |
| 1023 |
11 continue |
11 continue |
| 1024 |
CALL GRKUTA(CHARGE,STEP,VECT,VOUT) |
CALL GRKUTA(CHARGE,STEP,VECT,VOUT) |
| 1025 |
|
c$$$ ipass = ipass + 1 ! TEST |
| 1026 |
|
c$$$ PRINT *,'TRACKING -> STEP: ',ipass,' LENGHT: ', STEP ! TEST |
| 1027 |
IF(VOUT(3).GT.VECT(3)) THEN |
IF(VOUT(3).GT.VECT(3)) THEN |
| 1028 |
IFAIL=1 |
IFAIL=1 |
| 1029 |
if(TRKVERBOSE) |
if(TRKVERBOSE) |
| 1065 |
VOUT(7) = VOUT(7) * 0.997 !0.9968 |
VOUT(7) = VOUT(7) * 0.997 !0.9968 |
| 1066 |
* ----------------------------------------------- |
* ----------------------------------------------- |
| 1067 |
ENDIF |
ENDIF |
| 1068 |
|
c$$$ PRINT *,'TRACKING -> END' ! TEST |
| 1069 |
|
|
| 1070 |
ENDDO |
ENDDO |
| 1071 |
|
|
| 1104 |
YM(IP) = -100. !0. |
YM(IP) = -100. !0. |
| 1105 |
XM_A(IP) = -100. !0. |
XM_A(IP) = -100. !0. |
| 1106 |
YM_A(IP) = -100. !0. |
YM_A(IP) = -100. !0. |
| 1107 |
c ZM_A(IP) = 0 |
ZM_A(IP) = fitz(nplanes-ip+1) !init to mech. position |
| 1108 |
XM_B(IP) = -100. !0. |
XM_B(IP) = -100. !0. |
| 1109 |
YM_B(IP) = -100. !0. |
YM_B(IP) = -100. !0. |
| 1110 |
c ZM_B(IP) = 0 |
ZM_B(IP) = fitz(nplanes-ip+1) !init to mech. position |
| 1111 |
RESX(IP) = 1000. !3.d-4 |
RESX(IP) = 1000. !3.d-4 |
| 1112 |
RESY(IP) = 1000. !12.d-4 |
RESY(IP) = 1000. !12.d-4 |
| 1113 |
XGOOD(IP) = 0 |
XGOOD(IP) = 0 |
| 1155 |
S1=0. |
S1=0. |
| 1156 |
DO I=1,nplanes |
DO I=1,nplanes |
| 1157 |
IF(YGOOD(I).EQ.1)THEN |
IF(YGOOD(I).EQ.1)THEN |
| 1158 |
YY = YM(I) |
YY = REAL(YM(I))!EM GCC4.7 |
| 1159 |
IF(XGOOD(I).EQ.0)THEN |
IF(XGOOD(I).EQ.0)THEN |
| 1160 |
YY = (YM_A(I) + YM_B(I))/2 |
YY = REAL((YM_A(I) + YM_B(I))/2.)!EM GCC4.7 |
| 1161 |
ENDIF |
ENDIF |
| 1162 |
SZZ=SZZ+ZM(I)*ZM(I) |
SZZ=SZZ+REAL(ZM(I)*ZM(I))!EM GCC4.7 |
| 1163 |
SZY=SZY+ZM(I)*YY |
SZY=SZY+REAL(ZM(I)*YY)!EM GCC4.7 |
| 1164 |
SSY=SSY+YY |
SSY=SSY+YY |
| 1165 |
SZ=SZ+ZM(I) |
SZ=SZ+REAL(ZM(I))!EM GCC4.7 |
| 1166 |
S1=S1+1. |
S1=S1+1. |
| 1167 |
ENDIF |
ENDIF |
| 1168 |
ENDDO |
ENDDO |
| 1169 |
DET=SZZ*S1-SZ*SZ |
DET=SZZ*S1-SZ*SZ |
| 1170 |
AY=(SZY*S1-SZ*SSY)/DET |
AY=(SZY*S1-SZ*SSY)/DET |
| 1171 |
BY=(SZZ*SSY-SZY*SZ)/DET |
BY=(SZZ*SSY-SZY*SZ)/DET |
| 1172 |
Y0 = AY*ZINI+BY |
Y0 = REAL(AY*ZINI+BY)!EM GCC4.7 |
| 1173 |
* ---------------------------------------- |
* ---------------------------------------- |
| 1174 |
* X view |
* X view |
| 1175 |
* ---------------------------------------- |
* ---------------------------------------- |
| 1179 |
NP=0 |
NP=0 |
| 1180 |
DO I=1,nplanes |
DO I=1,nplanes |
| 1181 |
IF(XGOOD(I).EQ.1)THEN |
IF(XGOOD(I).EQ.1)THEN |
| 1182 |
XX = XM(I) |
XX = REAL(XM(I))!EM GCC4.7 |
| 1183 |
IF(YGOOD(I).EQ.0)THEN |
IF(YGOOD(I).EQ.0)THEN |
| 1184 |
XX = (XM_A(I) + XM_B(I))/2 |
XX = REAL((XM_A(I) + XM_B(I))/2.)!EM GCC4.7 |
| 1185 |
ENDIF |
ENDIF |
| 1186 |
NP=NP+1 |
NP=NP+1 |
| 1187 |
XP(NP)=XX |
XP(NP)=XX |
| 1188 |
ZP(NP)=ZM(I) |
ZP(NP)=REAL(ZM(I))!EM GCC4.7 |
| 1189 |
ENDIF |
ENDIF |
| 1190 |
ENDDO |
ENDDO |
| 1191 |
IFLAG=0 !no debug mode |
IFLAG=0 !no debug mode |
| 1199 |
|
|
| 1200 |
IF(IFLAG.NE.0)GOTO 10 !straigth fit |
IF(IFLAG.NE.0)GOTO 10 !straigth fit |
| 1201 |
c if(CHI.gt.100)GOTO 10 !straigth fit |
c if(CHI.gt.100)GOTO 10 !straigth fit |
| 1202 |
ARG = RADIUS**2-(ZINI-ZC)**2 |
ARG = REAL(RADIUS**2-(ZINI-ZC)**2)!EM GCC4.7 |
| 1203 |
IF(ARG.LT.0)GOTO 10 !straigth fit |
IF(ARG.LT.0)GOTO 10 !straigth fit |
| 1204 |
DC = SQRT(ARG) |
DC = SQRT(ARG) |
| 1205 |
IF(XC.GT.0)DC=-DC |
IF(XC.GT.0)DC=-DC |
| 1206 |
X0=XC+DC |
X0=XC+DC |
| 1207 |
AX = -(ZINI-ZC)/DC |
AX = REAL(-(ZINI-ZC)/DC)!EM GCC4.7 |
| 1208 |
DEF=100./(RADIUS*0.3*0.43) |
DEF=100./(RADIUS*0.3*0.43) |
| 1209 |
IF(XC.GT.0)DEF=-DEF |
IF(XC.GT.0)DEF=-DEF |
| 1210 |
|
|
| 1230 |
S1=0. |
S1=0. |
| 1231 |
DO I=1,nplanes |
DO I=1,nplanes |
| 1232 |
IF(XGOOD(I).EQ.1)THEN |
IF(XGOOD(I).EQ.1)THEN |
| 1233 |
XX = XM(I) |
XX = REAL(XM(I))!EM GCC4.7 |
| 1234 |
IF(YGOOD(I).EQ.0)THEN |
IF(YGOOD(I).EQ.0)THEN |
| 1235 |
XX = (XM_A(I) + XM_B(I))/2 |
XX = REAL((XM_A(I) + XM_B(I))/2.)!EM GCC4.7 |
| 1236 |
ENDIF |
ENDIF |
| 1237 |
SZZ=SZZ+ZM(I)*ZM(I) |
SZZ=SZZ+REAL(ZM(I)*ZM(I))!EM GCC4.7 |
| 1238 |
SZX=SZX+ZM(I)*XX |
SZX=SZX+REAL(ZM(I)*XX)!EM GCC4.7 |
| 1239 |
SSX=SSX+XX |
SSX=SSX+XX |
| 1240 |
SZ=SZ+ZM(I) |
SZ=SZ+REAL(ZM(I))!EM GCC4.7 |
| 1241 |
S1=S1+1. |
S1=S1+1. |
| 1242 |
ENDIF |
ENDIF |
| 1243 |
ENDDO |
ENDDO |
| 1245 |
AX=(SZX*S1-SZ*SSX)/DET |
AX=(SZX*S1-SZ*SSX)/DET |
| 1246 |
BX=(SZZ*SSX-SZX*SZ)/DET |
BX=(SZZ*SSX-SZX*SZ)/DET |
| 1247 |
DEF = 0 |
DEF = 0 |
| 1248 |
X0 = AX*ZINI+BX |
X0 = REAL(AX*ZINI+BX)!EM GCC4.7 |
| 1249 |
|
|
| 1250 |
20 CONTINUE |
20 CONTINUE |
| 1251 |
* ---------------------------------------- |
* ---------------------------------------- |
| 1256 |
AL(2) = Y0 |
AL(2) = Y0 |
| 1257 |
tath = sqrt(AY**2+AX**2) |
tath = sqrt(AY**2+AX**2) |
| 1258 |
AL(3) = tath/sqrt(1+tath**2) |
AL(3) = tath/sqrt(1+tath**2) |
|
c$$$ IF(AX.NE.0)THEN |
|
|
c$$$ AL(4)= atan(AY/AX) |
|
|
c$$$ ELSE |
|
|
c$$$ AL(4) = acos(-1.)/2 |
|
|
c$$$ IF(AY.LT.0)AL(4) = AL(4)+acos(-1.) |
|
|
c$$$ ENDIF |
|
|
c$$$ IF(AX.LT.0)AL(4)= acos(-1.)+ AL(4) |
|
|
c$$$ AL(4) = -acos(-1.) + AL(4) !from incidence direction to tracking ref.sys. |
|
|
|
|
|
c$$$ AL(4) = 0. |
|
|
c$$$ IF(AX.NE.0.AND.AY.NE.0)THEN |
|
|
c$$$ AL(4)= atan(AY/AX) |
|
|
c$$$ ELSEIF(AY.EQ.0)THEN |
|
|
c$$$ AL(4) = 0. |
|
|
c$$$ IF(AX.LT.0)AL(4) = AL(4)+acos(-1.) |
|
|
c$$$ ELSEIF(AX.EQ.0)THEN |
|
|
c$$$ AL(4) = acos(-1.)/2 |
|
|
c$$$ IF(AY.LT.0)AL(4) = AL(4)+acos(-1.) |
|
|
c$$$ ENDIF |
|
|
c$$$ IF(AX.LT.0)AL(4)= acos(-1.)+ AL(4) |
|
|
c$$$ AL(4) = -acos(-1.) + AL(4) !from incidence direction to tracking ref.sys. |
|
|
|
|
|
c$$$ AL(4)=0. |
|
|
c$$$ IF( AX.NE.0.OR.AY.NE.0. ) THEN |
|
|
c$$$ AL(4) = ASIN(AY/SQRT(AX**2+AY**2)) |
|
|
c$$$ IF(AX.LT.0.) AL(4) = ACOS(-1.0)-AL(4) |
|
|
c$$$ ENDIF |
|
| 1259 |
|
|
| 1260 |
AL(4)=0. |
AL(4)=0. |
| 1261 |
IF( AX.NE.0.OR.AY.NE.0. ) THEN |
IF( AX.NE.0.OR.AY.NE.0. ) THEN |