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118 4 DESCRIPTION OF THE AVAILABLE PROCEDURES˜@˜@ Ã O þÿ)@¾¾> Ž O ¿ >4 1@¡)U¾¾¦UNIPOT: Unipotential cylindrical electrostatic lensThe lens is cylindrically symmetric about § the -axis.The length of the first (resp. second, third) § q electrode §is 4 (resp.The ˜ q potentials ˜ are and . The inner radius is 1is [27]§ , ). The distance between the electrodes O is .(Fig. 38). The model for the electrostatic potential along the axisO ¿¤£¥¤ é ÃÄn&`é Ã> wÄ w Ž >@ w1 4Äm ˜ q> Ž¿ >Ä w Ž >& é ÃÄ›&`é Ã> ¿( distance from the center of the central electrode; = 1,318; cosh = hyperbolic cosine), from which the field¢ Ä and its derivatives are deduced following the procedure described in section 1.5.2. Ã §#"kS"eUse PARTICUL prior to UNIPOT, for the definition of particle mass and charge.1 41 4ÿ ¢¡The total length of the lens § q isterminates at exit of the third one. §@ §U O ; stepwise integration starts at entrance of the first electrode andFigure 38: Three-electrode cylindrical unipotential lens.
4.4 Optical Elements and related numerical procedures 119VENUS: Simulation of a rectangular dipole magnet4VENUS is dedicated to a ‘rough’ simulation of Saturne Laboratory’s VENUS dipole. The fieldmagnet, with ¡ 4longitudinal extent and o å¨ transverse extent ; outside these limits, ¡ §„¨is constant inside the(Fig. 39).C\Figure 39: Scheme of VENUS rectangular dipole.
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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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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@
Page 139 and 140: Keywords and input data formatting
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Page 146 and 147: 146 Keywords and input data formatt
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168 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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