Author: Böge, M.
Paper Title Page
THPC061 Comparison of Linear Optics Correction Means at the SLS 3032
 
  • M. Aiba, M. Böge, J.T.M. Chrin, N. Milas, T. Schilcher, A. Streun
    PSI, Villigen, Switzerland
 
  The ex­per­i­men­tal de­ter­mi­na­tion of lin­ear op­tics is a fun­da­men­tal pre­req­ui­site to achiev­ing a high per­for­mance stor­age ring. In order to fur­ther en­hance SLS per­for­mance and to sim­u­la­ta­neous­ly re­veal the lim­i­ta­tions of the var­i­ous tech­niques, we per­form a sys­tem­at­ic study of lin­ear op­tics op­ti­miza­tion using var­i­ous in­de­pen­dent meth­ods. These in­clude an anal­y­sis of the orbit re­ponse (LOCO), turn-by-turn data, and the re­sponse of the tune, whose cor­rec­tion is ac­com­plished using the stan­dard SLS pro­ce­dure of vary­ing the quadrupole strengths. A com­par­i­son of re­sults from these pro­ce­dures, which use fully in­de­pen­dent ob­serv­ables, pro­vides us with a valu­able cross-check. For ex­am­ple, the be­ta­tron phase ad­vances be­tween BPMs, which is in­de­pen­dent of BPM cal­i­bra­tion, con­firms the op­tics cor­rec­tion as de­ter­mined from LOCO. The lin­ear op­tics are hence bet­ter op­ti­mized, and these pro­ce­dures, LOCO in par­tic­u­lar, fur­ther serve to ex­pose any pre­vi­ous­ly hid­den mis-cal­i­bra­tion of pa­ram­e­ters e.g. from BPMs and cor­rec­tor mag­nets. Sys­tem­at­ic er­rors from turn-by-turn data could also be vast­ly re­duced by a bet­ter syn­chro­niza­tion of the BPM trig­gers with the elec­tron beam.  
 
THPC062 SLS Vertical Emittance Tuning 3035
 
  • M. Böge, M. Aiba, N. Milas, A. Streun
    PSI, Villigen, Switzerland
  • S.M. Liuzzo
    INFN/LNF, Frascati (Roma), Italy
 
  To es­tab­lish ul­tra-small ver­ti­cal emit­tances (<1pm­rad @2.86GeV) is one im­por­tant aim of fu­ture lin­ear col­lid­er damp­ing ring op­ti­miza­tion stud­ies* at the SLS. By uti­liz­ing var­i­ous cor­rec­tion tech­niques the SLS is al­ready close to this goal with emit­tances of <2pm.​rad @2.4GeV under the con­straint of main­tain­ing user op­er­a­tion con­di­tions. One of the lim­it­ing con­tri­bu­tions is the re­main­ing spu­ri­ous ver­ti­cal dis­per­sion etay of ~1.4mm which can be re­duced by care­ful re-align­ment and the ap­pli­ca­tion of dis­per­sion-free steer­ing tech­niques. The lat­ter re­quire orbit ma­nip­u­la­tions which are only par­tial­ly com­pat­i­ble with the user op­er­a­tion mode. A first ap­pli­ca­tion of dis­per­sion-free steer­ing tech­niques demon­strates that etay can be re­duced to <1mm at the ex­pense of large orbit ex­cur­sions which re­quire a si­mul­ta­ne­ous be­ta­tron-cou­pling cor­rec­tion by means of skew quadrupoles in order to ben­e­fit in terms of a fur­ther re­duc­tion of ver­ti­cal emit­tance. There­fore pos­si­ble gird­er and mag­net mis­align­ments are an­a­lyzed in sim­u­la­tion which al­lows to lo­cal­ize the sources of etay and to elim­i­nate them by re-align­ment. Fol­low­ing this path the goal to achieve emit­tances close to 1pm­rad is with­in reach.
* In January 2011 the EU-project TIARA (Test Infrastructure and Accelerator Research Area) started with contributions from the SLS as part of the SVET (SLS Vertical Emittance Tuning) work package WP6.