ZGOUBI USERS' GUIDE - HEP

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242 4 USE OF THE FITTING PROCEDURE4 USE OF THE FITTING PROCEDUREFigure 48: Vary B in all quadrupoles, for fitting of the transfer coefficients 1 7 >and 1 T P at the endof the line. The first and last quadrupoles are coupled so as to present the same value ofB.zgoubi data file.MATCHING A SYMMETRIC QUADRUPOLE TRIPLET’OBJET’ 12501.73 750MeV/c PROTONS5 11 PARTICLES FOR USE OF MATRIX2. 2. 2. 2. 0. .0010. 0. 0. 0. 0. 1.’ESL ’ 2200.’QUADRUPO’ 3 3040. 15. -7.0. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7230. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7235.1 0. 0. 0.’ESL’ 430.’QUADRUPO’ 5 5040. 15. 3.0. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7230. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7235.1 0. 0. 0.’ESL’ 630.’QUADRUPO’ 7 7040. 15. -7.0. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7230. 0.6 .1122 6.2671 -1.4982 3.5882 -2.1209 1.7235.1 0. 0. 0.’ESL’ 8200.’MATRIX’ 91 0’FIT’ VARY B IN QUADS FOR FIT OF R12 AND R34 102 FIRST ORDER TRANSFER COEFFICIENTS3 12 7.12 2. SYMMETRIC TRIPLET => QUADS #1 AND #3 ARE COUPLED5 12 0. 2. PARAMETER #12 OF ELEMENTS #3, 5 AND 7 IS FIELD VALUE21 1 2 8 16.6 1. FIRST CONSTRAINT: R12=16.6, AFTER ELEMENT #8 (LAST DRIF1 3 4 8 -.88 1. SECOND CONSTRAINT: R34=-.88’END’ 11
243Excerpt of zgoubi output : first order transfer matricesprior to and after fitting.*******************************************************************************************TRANSFER MATRIX WITH STARTING CONDITIONS :MATRICE DE TRANSFERT ORDRE 1 ( MKSA )5.43642 17.02625 0.00000 0.00000 0.00000 0.000001.67617 5.43442 0.00000 0.00000 0.00000 0.000000.00000 0.00000 -1.27013 -0.97430 0.00000 0.000000.00000 0.00000 -0.62915 -1.27004 0.00000 0.000000.00000 0.00000 0.00000 0.00000 1.00000 0.000000.00000 0.00000 0.00000 0.00000 0.00000 1.00000*******************************************************************************************STATE OF VARIABLES AFTER MATCHING :VARIABLE ELEMENT 3, PRMTR #12 :COUPLED WITH ELEMENT 7, PRMTR #12STATUS OF VARIABLESLMNT VAR PARAM MINIMUM INITIAL FINAL MAXIMUM STEP3 1 12 -8.384E+00 -6.986E+00 -6.98648097E+00 -5.590E+00 2.424E-165 2 12 2.585E+00 3.230E+00 3.22956371E+00 3.877E+00 1.208E-16STATUS OF CONSTRAINTSTYPE I J LMNT# DESIRED WEIGHT REACHED KI21 1 2 8 1.6600E+01 1.0000E+00 1.6600000E+01 8.2185E-021 3 4 8 -8.8000E-01 1.0000E+00 -8.8000000E-01 9.1781E-01*******************************************************************************************FINAL RUN, WITH NEW VARIABLES :9 MATRIX 9Frame for MATRIX calculation moved by :XC = 0.000 CM , YC = 0.000 CM , A = 0.00000 DEG ( = 0.000000 RD )Path length of particle #1 : 580.0000 mMATRICE DE TRANSFERT ORDRE 1 ( MKSA )5.272531 16.600000 0.000000 0.000000 0.000000 0.0000001.614433 5.272531 0.000000 0.000000 0.000000 0.0000000.000000 0.000000 -1.244124 -0.880000 0.000000 0.0000000.000000 0.000000 -0.622552 -1.244124 0.000000 0.0000000.000000 0.000000 0.000000 0.000000 1.000000 0.0000000.000000 0.000000 0.000000 0.000000 0.000000 1.000000Determinants : DetY-1 = -.0000011112DetZ-1 = -.0000000156R12=0 at -3.1484 metersR34=0 at -0.7073 metersFirst order sympletic conditions (expected values = 0) :-1.1112E-06 -1.5616E-08 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00*******************************************************************************************
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CEA DSM DAPNIA-02-395 (2002)ZGOUBI
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Table of contentsPART A Description
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PART ADescription of software conte
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8¤¥ PARTICUL Particle characteris
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10ELECTROMAGNETIC ELEMENTSDecapoleD
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!!%" && 131 NUMERICAL CALCULATION
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1.2 Integration of the Lorentz Equa
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1.2 Integration of the Lorentz Equa
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4Ž ^ ˜ ¡§ ^"- ^ ˜ ¡ ^¡wTGT
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in fourth order. The coefficients
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4 ´ ´""4§> ´4 >4>1.4 Calculati
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A cylindrically symmetric field can
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Introducing also ¡The derivatives
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30 3 SYNCHROTRON RADIATION¾ÍôVT
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32 3 SYNCHROTRON RADIATIONÉ Éwher
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354 DESCRIPTION OF THE AVAILABLE PR
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4.2 Definition of an Object 37where
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4.2 Definition of an Object 39\Pqî
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4.2 Definition of an Object 41¹q
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4.3 Declaration of options 43\P4.3
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4.3 Declaration of options 45END or
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4.3 Declaration of options 47· £
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4.3 Declaration of options 49{ww{{q
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4.3 Declaration of options 51GASCAT
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4.3 Declaration of options 53·{N$
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4.3 Declaration of options 55PARTIC
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4.3 Declaration of options 57RESET:
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4.3 Declaration of options 59if qî
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4.3 Declaration of options 61P4©@4
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4.3 Declaration of options 63:£¨
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u2 >04.4 Optical Elements and relat
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4.4 Optical Elements and related nu
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4.5 Output Procedures 123¨ ¢ < ¤
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4.5 Output Procedures 1254·444"4HI
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4.5 Output Procedures 127PICKUPS: B
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4.5 Output Procedures 129wSPNPRNL,
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4.5 Output Procedures 131TWISS: Cal
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4.6 Complementary Features 133U@©@
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4.6 Complementary Features 135¢ww@
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Keywords and input data formatting
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146 Keywords and input data formatt
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Page 192 and 193: 192 Keywords and input data formatt
Page 231 and 232: Examples 231oÑwü¦INTRODUCTIONSev
Page 233 and 234: 2331 MONTE CARLO IMAGES IN SPES 2Fi
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Page 237 and 238: 237zgoubi data file.800 MeV/c KAON
Page 239 and 240: 2393 IN-FLIGHT DECAY IN SPES 3Figur
Page 241: 241Excerpt of zgoubi output : histo
Page 245 and 246: 245zgoubi data file (begining and e
Page 247 and 248: 247zgoubi data file.MICROBEAM LINE,
Page 249: 2499 HISTO HISTOGRAHISTOGRAMME DE L
Page 253 and 254: 253INTRODUCTIONThe basic zgoubi FOR
Page 255 and 256: REFERENCES 255References[1] F. Méo
Page 257 and 258: Indexacceleration, 56, 58, 74, 155,
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