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164 Keywords and input data formattingRepeat £, ‰, ‰777, ‰, ‰>>>ñ@4 qq¥MñqDIPOLESDipole magnet £ -uplet1 2 >b>¿ KBDBDB¡|• ` MbDc 7 ¡ 4 d b ´ b 1 7Öe 1†w{1 2 b 1 2 b > Ö‡ 1†w{1 2 b ¤÷¨ : print field and coordinates along trajectories\ w @¾ q "$ÅI¤;¨q "£ , ŕ , 1 2£ Number of magnets in the -uplet; no dim., I, 2*Etotal angular extent of the dipole; reference radiusdeg, cmtimes the following sequenceACN, PŸ1 2, b ", ¡ 4, Positioning of EFBs : azimuth, 1 2 b 1 2 PŸ1 2; field; deg., cm, kG, 3*E, I,*no dim.ž *Ež q "/number of, and field coefficientsž ž ENTRANCE FIELD BOUNDARY® 4®, Fringe field extent ñ (Exponential type fringe field¥ with7 ¥4 1 1 ® ® 42), sharp edge3'if ×=0 cm, no dim. 2*E ¯‡°±/$3' ² ²CBEBDBL ² M ¥£ ², ² 4 w ² M, shift unused; ² 4EFB shiftto ² M: see above; 0-6, 6* I,7*Eno dim., cm- ² > ¥› ›› ÃS‰, Å , 1 7, ‰, ‰1 > 7ed‰> x 1 7ed > )x, Azimuth of entrance EFB with respect to ACN; 2*deg, 4*cm 6*Ewedge angle of EFB; radii and linearextents of EFB (use whenEXIT FIELD BOUNDARY(See ENTRANCE FIELD BOUNDARY), ñ cm, no dim. 2*E, shift\ w G, G *no dim., cm1, 7*E® 4£ ², ² 4 w ² MÃ ¬, Å , 1 7, 1 > 2*deg, 4*cm 6*ELATERAL FIELD BOUNDARYto be implemented - following data not used, ñ cm, no dim. 2*E®Z4£ ², ² 4 w ² M, shift 0-6, 6*no 1, 7*Edim., cmÃ*¬, Å , 1 7, 1 > , 1 U 2*deg, 5*cm 7*EEnd of repeatKIRD, ResolKIRD=0 : analytical computation of field derivatives, Resolis unusedKIRD 0 : numerical interpolation of field derivatives, sizeof flying mesh XPAS/ResolKIRD=2 or 25 : second degree, 9- or 25-point gridKIRD=4 : fourth degree, 25-point grid\; no dim. I, E
Keywords and input data formatting 165¢·XPAS Integration step cm EKPOS Positioning of the magnet, normally 2. Two options: 1-2 I1|¢ O¥if KPOS = 2Positioning as follows:, , ,Radius and angle of reference, respectively, cm, rad, cm, rad 4*Eat entrance and exit of the magnetif KPOS = 1Automatic positioning of the magnet, by means ofreference relative momentum no dim. E
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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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Page 113 and 114: 4.4 Optical Elements and related nu
Page 123 and 124: 4.5 Output Procedures 123¨ ¢ < ¤
Page 125 and 126: 4.5 Output Procedures 1254·444"4HI
Page 127 and 128: 4.5 Output Procedures 127PICKUPS: B
Page 129 and 130: 4.5 Output Procedures 129wSPNPRNL,
Page 131 and 132: 4.5 Output Procedures 131TWISS: Cal
Page 133 and 134: 4.6 Complementary Features 133U@©@
Page 135: 4.6 Complementary Features 135¢ww@
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214 Keywords and input data formatt
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Examples 231oÑwü¦INTRODUCTIONSev
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2331 MONTE CARLO IMAGES IN SPES 2Fi
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235********************************
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237zgoubi data file.800 MeV/c KAON
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2393 IN-FLIGHT DECAY IN SPES 3Figur
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241Excerpt of zgoubi output : histo
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243Excerpt of zgoubi output : first
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245zgoubi data file (begining and e
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247zgoubi data file.MICROBEAM LINE,
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2499 HISTO HISTOGRAHISTOGRAMME DE L
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253INTRODUCTIONThe basic zgoubi FOR
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REFERENCES 255References[1] F. Méo
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Indexacceleration, 56, 58, 74, 155,
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