/[PAMELA software]/eventviewer/flight/src/grkuta.for
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Annotation of /eventviewer/flight/src/grkuta.for

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Revision 1.1.1.1 - (hide annotations) (download) (vendor branch)
Mon Mar 20 10:36:48 2006 UTC (18 years, 8 months ago) by mocchiut
Branch: FEventViewer
CVS Tags: v1r02, v1r03, v1r00, start
Changes since 1.1: +0 -0 lines
First flight release (limited capabilities)

1 mocchiut 1.1 **********************************************************************
2     *
3     *
4     * routine per tracciare la particella di uno STEP
5     *
6     SUBROUTINE GRKUTA (CHARGE,STEP,VECT,VOUT)
7     C.
8     C. ******************************************************************
9     C. * *
10     C. * Runge-Kutta method for tracking a particle through a magnetic *
11     C. * field. Uses Nystroem algorithm (See Handbook Nat. Bur. of *
12     C. * Standards, procedure 25.5.20) *
13     C. * *
14     C. * Input parameters *
15     C. * CHARGE Particle charge *
16     C. * STEP Step size *
17     C. * VECT Initial co-ords,direction cosines,momentum *
18     C. * Output parameters *
19     C. * VOUT Output co-ords,direction cosines,momentum *
20     C. * User routine called *
21     C. * CALL GUFLD(X,F) *
22     C. * *
23     C. * ==>Called by : <USER>, GUSWIM *
24     C. * Authors R.Brun, M.Hansroul ********* *
25     C. * V.Perevoztchikov (CUT STEP implementation) *
26     C. * *
27     C. * *
28     C. ******************************************************************
29     C.
30     IMPLICIT DOUBLE PRECISION(A-H,O-Z)
31     *
32     REAL VVV(3),FFF(3)
33     REAL*8 CHARGE, STEP, VECT(*), VOUT(*), F(4)
34     REAL*8 XYZT(3), XYZ(3), X, Y, Z, XT, YT, ZT
35     DIMENSION SECXS(4),SECYS(4),SECZS(4),HXP(3)
36     EQUIVALENCE (X,XYZ(1)),(Y,XYZ(2)),(Z,XYZ(3)),
37     + (XT,XYZT(1)),(YT,XYZT(2)),(ZT,XYZT(3))
38     *
39     PARAMETER (MAXIT = 1992, MAXCUT = 11)
40     PARAMETER (EC=2.9979251D-4,DLT=1D-4,DLT32=DLT/32)
41     PARAMETER (ZERO=0, ONE=1, TWO=2, THREE=3)
42     PARAMETER (THIRD=ONE/THREE, HALF=ONE/TWO)
43     PARAMETER (PISQUA=.986960440109D+01)
44     PARAMETER (IX=1,IY=2,IZ=3,IPX=4,IPY=5,IPZ=6)
45    
46     *.
47     *. ------------------------------------------------------------------
48     *.
49     * This constant is for units CM,GEV/C and KGAUSS
50     *
51     c print *,'GRKUTA+++++ charge ',charge,' step ',step,' vect(3) ',
52     c & vect(3)
53     ITER = 0
54     NCUT = 0
55     DO 10 J=1,7
56     VOUT(J)=VECT(J)
57     c print *,' grkuta j ',j,' vout ',vout(j)
58     c print *,' grkuta j ',j,' vect ',vect(j)
59     10 CONTINUE
60     PINV = EC * CHARGE / VECT(7)
61     TL = 0.
62     H = STEP
63     *
64     *
65     20 REST = STEP-TL
66     IF (DABS(H).GT.DABS(REST)) H = REST
67     DO I=1,3
68     VVV(I)=SNGL(VOUT(I))
69     c print *,'grkuta i ',i,' vvv ',vvv(i)
70     ENDDO
71     c print *,'grkuta pinv ',pinv,' h ',h,' rest ',rest
72    
73     CALL GUFLD(VVV,FFF)
74     DO I=1,3
75     F(I)=DBLE(FFF(I))
76     c print *,'grkuta i ',i,' f ',f(i)
77     ENDDO
78     *
79     * Start of integration
80     *
81     X = VOUT(1)
82     Y = VOUT(2)
83     Z = VOUT(3)
84     A = VOUT(4)
85     B = VOUT(5)
86     C = VOUT(6)
87     c print *,' QUI A ',A,' B ',B,' C ',C
88     c print *,' QUI x ',x,' y ',y,' z ',z
89     *
90     H2 = HALF * H
91     H4 = HALF * H2
92     PH = PINV * H
93     PH2 = HALF * PH
94     SECXS(1) = (B * F(3) - C * F(2)) * PH2
95     SECYS(1) = (C * F(1) - A * F(3)) * PH2
96     SECZS(1) = (A * F(2) - B * F(1)) * PH2
97     ANG2 = (SECXS(1)**2 + SECYS(1)**2 + SECZS(1)**2)
98     IF (ANG2.GT.PISQUA) GO TO 40
99     DXT = H2 * A + H4 * SECXS(1)
100     DYT = H2 * B + H4 * SECYS(1)
101     DZT = H2 * C + H4 * SECZS(1)
102     XT = X + DXT
103     YT = Y + DYT
104     ZT = Z + DZT
105     *
106     * Second intermediate point
107     *
108     EST = DABS(DXT)+DABS(DYT)+DABS(DZT)
109     IF (EST.GT.H) GO TO 30
110    
111     DO I=1,3
112     VVV(I)=SNGL(XYZT(I))
113     ENDDO
114     CALL GUFLD(VVV,FFF)
115     DO I=1,3
116     F(I)=DBLE(FFF(I))
117     c print *,'2grkuta i ',i,' f ',f(i)
118     ENDDO
119     C CALL GUFLD(XYZT,F)
120     AT = A + SECXS(1)
121     BT = B + SECYS(1)
122     CT = C + SECZS(1)
123     *
124     SECXS(2) = (BT * F(3) - CT * F(2)) * PH2
125     SECYS(2) = (CT * F(1) - AT * F(3)) * PH2
126     SECZS(2) = (AT * F(2) - BT * F(1)) * PH2
127     c print *,'1 at ',xt,' bt ',yt,' ct ',zt
128     AT = A + SECXS(2)
129     BT = B + SECYS(2)
130     CT = C + SECZS(2)
131     c print *,'2 at ',xt,' bt ',yt,' ct ',zt
132     SECXS(3) = (BT * F(3) - CT * F(2)) * PH2
133     SECYS(3) = (CT * F(1) - AT * F(3)) * PH2
134     SECZS(3) = (AT * F(2) - BT * F(1)) * PH2
135     DXT = H * (A + SECXS(3))
136     DYT = H * (B + SECYS(3))
137     DZT = H * (C + SECZS(3))
138     XT = X + DXT
139     YT = Y + DYT
140     ZT = Z + DZT
141     c print *,' xt ',xt,' yt ',yt,' zt ',zt
142     c print *,' dxt ',xt,' dyt ',yt,' dzt ',zt
143     c print *,' at ',xt,' bt ',yt,' ct ',zt
144     AT = A + TWO*SECXS(3)
145     BT = B + TWO*SECYS(3)
146     CT = C + TWO*SECZS(3)
147     *
148     EST = ABS(DXT)+ABS(DYT)+ABS(DZT)
149     IF (EST.GT.2.*ABS(H)) GO TO 30
150    
151     DO I=1,3
152     VVV(I)=SNGL(XYZT(I))
153     c print *,'3grkuta i ',i,' vvv ',vvv(i)
154     c print *,'3grkuta i ',i,' xyzt ',xyzt(i)
155     ENDDO
156     CALL GUFLD(VVV,FFF)
157     DO I=1,3
158     F(I)=DBLE(FFF(I))
159     c print *,'3grkuta i ',i,' f ',f(i)
160     c print *,'3grkuta i ',i,' fff ',fff(i)
161     ENDDO
162     C CALL GUFLD(XYZT,F)
163     *
164     Z = Z + (C + (SECZS(1) + SECZS(2) + SECZS(3)) * THIRD) * H
165     Y = Y + (B + (SECYS(1) + SECYS(2) + SECYS(3)) * THIRD) * H
166     X = X + (A + (SECXS(1) + SECXS(2) + SECXS(3)) * THIRD) * H
167     *
168     SECXS(4) = (BT*F(3) - CT*F(2))* PH2
169     c print *,'secxs4 bt ',bt,' ct ',ct,' ph2 ',ph2
170     SECYS(4) = (CT*F(1) - AT*F(3))* PH2
171     SECZS(4) = (AT*F(2) - BT*F(1))* PH2
172     A = A+(SECXS(1)+SECXS(4)+TWO * (SECXS(2)+SECXS(3))) * THIRD
173     c print *,'=> a ',a,' secxs 1 ',SECXS(1),' 4 ',SECXS(4),' 2 ',
174     c & SECXS(2),' 3 ',SECXS(3),' third ',third
175     B = B+(SECYS(1)+SECYS(4)+TWO * (SECYS(2)+SECYS(3))) * THIRD
176     C = C+(SECZS(1)+SECZS(4)+TWO * (SECZS(2)+SECZS(3))) * THIRD
177     *
178     EST = ABS(SECXS(1)+SECXS(4) - (SECXS(2)+SECXS(3)))
179     ++ ABS(SECYS(1)+SECYS(4) - (SECYS(2)+SECYS(3)))
180     ++ ABS(SECZS(1)+SECZS(4) - (SECZS(2)+SECZS(3)))
181     *
182     IF (EST.GT.DLT .AND. ABS(H).GT.1.E-4) GO TO 30
183     ITER = ITER + 1
184     NCUT = 0
185     * If too many iterations, go to HELIX
186     IF (ITER.GT.MAXIT) GO TO 40
187     *
188     TL = TL + H
189     IF (EST.LT.(DLT32)) THEN
190     H = H*TWO
191     ENDIF
192     CBA = ONE/ SQRT(A*A + B*B + C*C)
193     VOUT(1) = X
194     VOUT(2) = Y
195     VOUT(3) = Z
196     VOUT(4) = CBA*A
197     VOUT(5) = CBA*B
198     VOUT(6) = CBA*C
199     REST = STEP - TL
200     IF (STEP.LT.0.) REST = -REST
201     IF (REST .GT. 1.E-5*DABS(STEP)) GO TO 20
202     *
203     c print *,' x ',x,' y ',y,' z ',z,' cba ',cba,
204     c & ' a ',a,' b ',b,' c ',c,' step ',step,
205     c & ' tl ',tl,' rest ',rest,' est ',est,
206     c & ' h ',h,' two ',two,' one ',one
207     GO TO 999
208     *
209     ** CUT STEP
210     30 NCUT = NCUT + 1
211     * If too many cuts , go to HELIX
212     IF (NCUT.GT.MAXCUT) GO TO 40
213     H = H*HALF
214     GO TO 20
215     *
216     ** ANGLE TOO BIG, USE HELIX
217     40 F1 = F(1)
218     F2 = F(2)
219     F3 = F(3)
220     F4 = DSQRT(F1**2+F2**2+F3**2)
221     RHO = -F4*PINV
222     TET = RHO * STEP
223     IF(TET.NE.0.) THEN
224     HNORM = ONE/F4
225     F1 = F1*HNORM
226     F2 = F2*HNORM
227     F3 = F3*HNORM
228     *
229     HXP(1) = F2*VECT(IPZ) - F3*VECT(IPY)
230     HXP(2) = F3*VECT(IPX) - F1*VECT(IPZ)
231     HXP(3) = F1*VECT(IPY) - F2*VECT(IPX)
232    
233     HP = F1*VECT(IPX) + F2*VECT(IPY) + F3*VECT(IPZ)
234     *
235     RHO1 = ONE/RHO
236     SINT = DSIN(TET)
237     COST = TWO*DSIN(HALF*TET)**2
238     *
239     G1 = SINT*RHO1
240     G2 = COST*RHO1
241     G3 = (TET-SINT) * HP*RHO1
242     G4 = -COST
243     G5 = SINT
244     G6 = COST * HP
245    
246     VOUT(IX) = VECT(IX) + (G1*VECT(IPX) + G2*HXP(1) + G3*F1)
247     VOUT(IY) = VECT(IY) + (G1*VECT(IPY) + G2*HXP(2) + G3*F2)
248     VOUT(IZ) = VECT(IZ) + (G1*VECT(IPZ) + G2*HXP(3) + G3*F3)
249     c print *,' iz ',iz,' vect ',vect(iz),' g1 ',g1,' ipz ',ipz,
250     c & ' vect ',vect(ipz),' g2 ',g2,' hxp ',hxp(3),' g3 ',g3,
251     c & ' f3 ',f3
252    
253     VOUT(IPX) = VECT(IPX) + (G4*VECT(IPX) + G5*HXP(1) + G6*F1)
254     VOUT(IPY) = VECT(IPY) + (G4*VECT(IPY) + G5*HXP(2) + G6*F2)
255     VOUT(IPZ) = VECT(IPZ) + (G4*VECT(IPZ) + G5*HXP(3) + G6*F3)
256     *
257     ELSE
258     VOUT(IX) = VECT(IX) + STEP*VECT(IPX)
259     VOUT(IY) = VECT(IY) + STEP*VECT(IPY)
260     VOUT(IZ) = VECT(IZ) + STEP*VECT(IPZ)
261     c print *,' iz ',iz,' vect ',vect(iz),' step ',step,' ipz ',ipz,
262     c & ' vect ',vect(ipz)
263     *
264     ENDIF
265     *
266     999 END
267     *
268     *
269    
270    
271    
272     **********************************************************************
273     *
274     * gives the value of the magnetic field in the tracking point
275     *
276     **********************************************************************
277    
278     subroutine gufld(v,f) !coordinates in cm, B field in kGauss
279    
280     real v(3),f(3) !coordinates in cm, B field in kGauss, error in kGauss
281    
282     real*8 vv(3),ff(3) !inter_B.f works in double precision
283    
284    
285     do i=1,3
286     vv(i)=v(i)/100. !inter_B.f works in meters
287     c print *,'IN gufld i ',i,' v ',v(i)
288     enddo
289     c inter_B: coordinates in m, B field in Tesla
290     call inter_B(vv(1),vv(2),vv(3),ff)
291     do i=1,3 !change back the field in kGauss
292     f(i)=ff(i)*10.
293     enddo
294     c do i=1,3
295     c print *,'OUT gufld i ',i,' v ',v(i)
296     c enddo
297     return
298     end
299    

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