<?xml version="1.0" encoding="UTF-8"?>
<xml>
  <records>
    <record>
       <contributors>
          <authors>
             <author>Kim, H.</author>
             <author>Hyun, M.O.</author>
             <author>Jang, H.</author>
             <author>Kim, M.S.</author>
             <author>Kim, Y.</author>
          </authors>
       </contributors>
       <titles>
          <title>
             Development of a Tuner Control System for Low-Energy Superconducting Linac at RAON
          </title>
       </titles>
       <publisher>JACoW Publishing</publisher>
       <pub-location>Geneva, Switzerland</pub-location>
		 <isbn>2226-0366</isbn>
		 <isbn>978-3-95450-215-8</isbn>
		 <electronic-resource-num>10.18429/JACoW-LINAC2022-THPOPA18</electronic-resource-num>
		 <language>English</language>
		 <pages>778-780</pages>
       <keywords>
          <keyword>controls</keyword>
          <keyword>cavity</keyword>
          <keyword>LLRF</keyword>
          <keyword>EPICS</keyword>
          <keyword>cryomodule</keyword>
       </keywords>
       <work-type>Contribution to a conference proceedings</work-type>
       <dates>
          <year>2022</year>
          <pub-dates>
             <date>2022-09</date>
          </pub-dates>
       </dates>
       <urls>
          <related-urls>
              <url>https://doi.org/10.18429/JACoW-LINAC2022-THPOPA18</url>
              <url>https://jacow.org/linac2022/papers/thpopa18.pdf</url>
          </related-urls>
       </urls>
       <abstract>
          We propose a tuner control system for low-energy superconducting linac at RAON. The frequency error of the superconducting cavities must be smaller than a few of Hz to operate in beam acceleration mode. To minimize the freuqency error as much as possible, the error is calculated in the low-level RF(LLRF), and the proposed tuner control system changes the superconducting cavity frequency by using a mechanical tuner and a motor attached to the cavity directly. This control system deals with not only the initial frequency error of the cavity but also the frequency drift of the cavity induced by external disturbance such as the slow fluctuation helium pressure automatically. In addition, an automatic proportional gain calibration technique is also proposed. In this paper, the detailed operation and techniques will be described.
       </abstract>
    </record>
  </records>
</xml>
