Abstract
An orbit correction method is presented for a region where the number of beam position monitors is much less than the number of possible trajectory distortions points (quads). The method was developed for the Coupled Cavities Linac (CCL) part of the Spallation Neutron Source (SNS) linac. The orbit correction is very important in this region to minimize losses and activation, but a traditional orbit correction did not work here. The new method based on a realistic online model was developed. The procedure of a model parameters finding and results are discussed.
Original language | English |
---|---|
Pages | 3056-3058 |
Number of pages | 3 |
State | Published - 2008 |
Event | 11th European Particle Accelerator Conference, EPAC 2008 - Genoa, Italy Duration: Jun 23 2008 → Jun 27 2008 |
Conference
Conference | 11th European Particle Accelerator Conference, EPAC 2008 |
---|---|
Country/Territory | Italy |
City | Genoa |
Period | 06/23/08 → 06/27/08 |